Replace Python numerical kernels with native C execution

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# 仿真后端
`app.simulation` 是 SystemSimulationApp 的仿真子包,用于承接模型定义、系统装配、数值求解和结果导出。
当前采用 Python 编排、C 数值执行。输入 XML 经校验后,Python 根据模型参数和连接生成系统专用 C;GCC 编译成 EXE,EXE 内执行初始化、物性、流量、机械、RK45/CVODE BDF、事件和采样。求解循环不调用 Python。
目标不是逐行翻译源模型,而是建立可运行、可测试、可导出,并能与 OpenModelica 或 AMESim baseline 对比的 Python 仿真框架。
## 目录
当前包含两条模型线:`Testmodel` 已有可运行的 ODE 近似和 OpenModelica 对比能力;`test_mql` 已形成 132 状态气动机械总闭包,正在按 AMESim baseline 做数值校准。
- `components/`:模型参数、端口、显示和结果声明。
- `core/`、`registry.py`、`systems/network.py`:模型合同与网络结构校验。
- `native_codegen/`:C 生成、构建、进程运行和 CLI。
- `config.py`、`sampling.py`、`results.py`:公共配置、进度、采样网格校验与结果类型。
- `performance.py`、`warmup.py`:编排计时和启动工具链检查。
- `reporting/amesim_results.py`:外部 Amesim 结果读取。
- 仓库根目录 `native/`:C 组件公式和求解器。
## 当前目录
旧 Python 积分器、数值组件方法和固定算例专用求解器已经退役。旧 `/api/reactflow/simulate-testmodel`、`/api/reactflow/simulate-test-mql` 返回 410;使用 `/api/system-xml/simulate` 或流式接口。
- `core/`: 元件基类、端口、状态、介质、方程和元数据协议。
- `solvers/`: ODE、压力流量代数方程和 stream 求解。
- `components/experimental/`: 用于验证元件开发规范的临时组件库。
- `components/experimental/storage/`: 气瓶和贮箱等储能元件。
- `components/experimental/flow/`: 对外注册的阻性管道和孔板等流动元件。
- `components/experimental/junctions/`: 三通等连接节点。
- `components/amesim/`: AMESim 气动、信号和机械组件原语。
- `systems/`: 通用仿真网络与 XML 驱动系统装配。
- `examples/testmodel/`: 固定 TestModel、专用闭合逻辑和基线运行入口。
- `examples/test_mql/`: AMESim `test_mql` 的系统装配、校准原语、诊断和运行入口。
- `reporting/`: CSV、SVG、运行报告、Modelica 对比结果、AMESim 结果读取和诊断报告导出。
- `registry.py`: 从已启用库清单受控发现、校验和实例化组件。
- `paths.py`: 项目、运行产物、基准和 Modelica 参考结果路径。
稳定基准存放在 `tests/baselines/simulation/`,实际运行产物默认写入被 Git 忽略的
`app/data/simulation-runs/`。新增或修改元件时,先阅读 `components/example.md`。
需要把运行产物写到仓库外时,可以设置 `SIMULATIONAPP_DATA_DIR` 环境变量。
FastAPI 的 `GET /api/components/catalog` 会把注册表转换成前端组件目录。ReactFlow
启动时自动读取该接口;接口暂时不可用时使用内置的同结构兜底定义。
临时组件库的声明入口是 `components/experimental/library.py`,AMESim 第一版
公开临时库入口是 `components/amesim/library.py`。公开模型必须在
模型类中声明 `MODEL_TYPE / MODEL_VERSION / PORTS / PARAMETERS /
RESULT_VARIABLES / DISPLAY / create()`,再把类路径加入库清单。完整规范参见
[`组件模型建模规范 v1`](../../docs/standard/component-model-authoring-spec-v1.md)和
[`组件库分类、发现与读取规范 v1`](../../docs/standard/component-library-spec-v1.md)。
当前关键文件:
- `core/medium.py`: 气体介质协议 `GasMedium` 与通用理想气体实现 `IdealGasMedium`
- `components/amesim/media/`: AMESim 零端口介质物性定义元件;具体类型确定介质,`property_model` 下拉参数选择计算方法,当前提供空气理想气体和氦气 Peng-Robinson
- `components/amesim/gases.py`: AMESim `gi` 介质物性实例注册表;`gi=0` 固定为空气(理想气体,内置默认),`gi=1..99` 引用画布中的显式介质定义
- `core/peng_robinson.py`: `test_mql` 与公开氦气介质共用的 Peng-Robinson 状态方程
- `performance.py`: 默认关闭、按单次仿真隔离的阶段与物性性能埋点
- `benchmark_performance.py`: System XML 主求解路径的可重复命令行基准工具
- `systems/network.py`: `SimulationNetwork`,负责组件注册、连接拓扑和状态向量拼装
- `solvers/solver.py`: `integrate_ode()`,优先走 `SciPy solve_ivp`,缺依赖时回退到内置 RK4,并支持 `t_start == t_stop` 的零时长返回
- `examples/testmodel/dynamic_pipe.py`: TestModel 专用单阻容管道近似,入口压降 + 出口直连内容腔
- `components/experimental/junctions/tee.py`: 三通的最小 stream 混合 helper
- `examples/testmodel/system.py`: `Testmodel` 的系统装配壳与外部运行入口
- `examples/testmodel/closure.py`: `Testmodel` 当前专用的闭合、初始化投影、分支求解与端口回写
- `examples/test_mql/system.py`: `test_mql` 系统装配、132 状态总闭包和关键输出映射
- `examples/test_mql/closure.py`: `test_mql` 气动网络 closure、snapshot、流量计算和端口写回
- `examples/test_mql/primitives/`: 固定算例专用的 Peng-Robinson 氦气、管路和机械校准原语
- `examples/test_mql/structural_network.py`: 固定算例专用的结构网络;不替代带端口契约校验的通用网络
- `reporting/testmodel_outputs.py`: `Testmodel` 的 CSV/SVG/对比摘要导出
- `reporting/amesim_results.py`: AMESim 结果读取入口
- `examples/test_mql/run_full_state_comparison.py`: `test_mql` 短时域 AMESim comparison 和诊断入口
- `examples/test_mql/run.py`: `test_mql` 结构运行与程序化执行入口
- `tests/`: 当前组件契约、XML、通用系统、AMESim 迁移和结果导出测试
## 可选性能诊断
`SIMULATIONAPP_PROFILE` 支持 `off`(默认)、`standard` 和 `audit`。`standard`
只统计低频的大阶段;`audit` 才展开 RHS、代数闭合、stream 和物性调用,开销也
明显更高。最终优化收益必须在 `off` 下复测。
Peng–Robinson 氦气的高开销物性默认使用一次仿真内独立的精确 LRU 缓存;不同
仿真任务不会共享条目,仿真结束后自动释放。可在启动进程前设置
`SIMULATIONAPP_PROPERTY_CACHE=off` 做数值和性能 A/B,正常运行保持默认 `on`。
缓存只复用完全相同的输入,不做四舍五入或容差匹配。
FastAPI worker 默认在 lifespan 启动阶段预热 SciPy 积分、非线性求解、稀疏
Jacobian 和 System XML XSD,完成后才开始接收请求。它不会运行业务模型,也不
写入文件;如需诊断冷启动,可设置 `SIMULATIONAPP_WARMUP=off`。每个 worker 都会
独立暖机一次。
```powershell
.venv-win\Scripts\python.exe -m app.simulation.benchmark_performance `
--mode audit --warmups 1 --runs 3 `
--factory "helium_step=tests.test_amesim_pnvo001_signal_xml:high_pressure_helium_step_project" `
--output app/data/performance-evaluations/helium-step.json
```
缓存关闭对照可在同一命令中增加 `--disable-property-cache`。缓存容量、命中、
未命中和驱逐数会在 audit 响应的
`diagnostics.performance.propertyCache` 中返回。
基准原始 JSON 默认放到已忽略的 `app/data/` 下。指标字段、实测结果和使用边界见
[`仿真性能评估 2026-08-15`](../../docs/other/仿真性能评估-2026-08-15.md)。
## 当前阶段进度
这一阶段原先有 4 件重点工作,现在的状态如下:
1. `mytee1` 的 stream/焓传播语义:已完成当前阶段收紧
现在如果只有一条支路发生倒流,下游来流焓统一按 `tank.h` 处理,不再临时借另一条支路的焓来凑。
2. 下游初始化/约束处理:已完成当前阶段收口
之前是“直接改对象状态再开始积分”,现在已经收成显式的 `consistent_initial_state_vector()` 初始化入口。当前这一步会在不改下游总质量、总内能的前提下,把几段直接相连的体积拉回同一个连接压力。
3. 自动校验:已完成当前阶段首版
已经补了标准库 `unittest` 回归测试,先把初始化投影是否守恒、是否污染原始状态,以及 4 个主变量的提交基线锁住。
4. 更严格介质模型:已完成当前阶段首版
已经从固定 `cp/cv` 的理想气体近似,推进到随温度变化的空气近似,并接上了内能反解和初始化求根。
如果只看结果,可以把这一阶段理解成:
- 连接器语义:首轮收紧已完成
- 初始化入口:首轮收口已完成
- 基线验证:首轮保护已完成
- 介质精化:首轮近似已完成
## 当前阶段收口
上一轮 `N0-N3` 已全部完成首版,当前可以简单理解为:
1. `N0`:系统层里最明显的流向/焓判断已经继续下沉到组件 helper。
2. `N1`:模型参数和运行参数已经收口到配置对象。
3. `N2`:运行接口已经分成“准备请求”和“执行请求”两层。
4. `N3`:结果导出和命令行报告格式化已经统一收口到 `reporting/`。
这一轮结束后,项目已经不缺“能不能跑”的能力,下一步更重要的是把后续开发最容易卡住的地方先处理掉。
## 本次推送更新
本次推送已经把上一轮建议里的 `M2-M5` 推进到下面这个状态:
1. `M2`:已完成当前阶段首版
- 已把 `Testmodel` 的专用闭合、初始化投影、分支入口流量求解、下游支路出口流量闭合、端口状态回写,从 `examples/testmodel/system.py` 拆到 `examples/testmodel/closure.py`
- `TestModelSystem` 现在主要承担组件装配、网络注册和对闭合器的委托,不再继续堆积系统级手写细节
2. `M3`:已完成当前阶段首版
- 已给两条支路入口流量固定点求解、下游公共压力投影补了显式诊断
- 诊断内容至少包含 `converged / iterations / residual`
- 已支持严格模式;内部求解不收敛时可以直接抛错,而不是静默返回最后一个近似值
- `run_testmodel()` 的结构化结果和 `testmodel_run_report.txt` 已能带出最后一次内部闭合求解诊断
3. `M4`:已完成当前阶段首版
- 自动测试已不再只盯最终主变量结果
- 现在已经覆盖:
- 改支路参数后,初始支路入口流量是否按预期变化
- 更偏激配置下,初始化和内部闭合是否仍然收敛
- 有无 Modelica 参考两种运行路径下,程序接口与产物行为是否一致
4. `M5`:已启动
- 当前已经明确选择优先走“更容易扩展”的方向,而不是先追求更贴近 Modelica
- 已完成第一步:把闭合器内部原来大量写死的 `upper/lower` 双支路逻辑,收成可复用的 `BranchClosureComponents / BranchClosureState` 结构
- 当前已继续推进到 `G1-G5` 的首轮兼容层改造:`snapshot` 已提供通用分支集合,系统层结果生成已拆成“通用键生成 + 旧键别名派生”两层,报告层已开始优先消费通用分支键,旧导出列名仍通过兼容映射保留,兼容测试已显式保护分支顺序和旧导出语义
## 下一阶段接手建议
如果继续往前推进,建议按下面顺序做,而不是再零散补功能:
1. `G1`:已完成当前阶段首轮兼容接入
- `TestModelSnapshot` 已新增 `branches` 集合
- 每个分支当前至少带 `name / pipe / inlet_flow / outlet_flow / inlet_h / inlet_flow_diagnostics`
- `pipe_upper / pipe_lower / branch_inlet_flows / branch_outlet_flows` 目前仍保留为兼容属性,供旧调用方继续使用
2. `G2`:已完成当前阶段首轮内部迁移
- `evaluate_solution()` 已改成从 `snapshot.branches` 读取数据,再通过显式分支名映射写回当前旧列名
- `rhs()` 里的分支导数计算已改成通过通用 helper 按分支循环生成,再按当前状态向量顺序拼回
- 当前外部导出列名仍保持兼容:
- `mypipe.p`
- `mypipe1.p`
- `branch_upper.in/out`
- `branch_lower.in/out`
3. `G3`:已完成当前阶段首轮兼容测试
- 当前测试已经显式保护:
- `branches` 顺序是否稳定
- `snapshot` 新字段和兼容字段是否一致
- 旧导出列名是否仍映射到正确分支语义
- 参数变化后 `upper/lower` 的名字和顺序是否不会被打乱
4. `G4`:已完成当前阶段首轮兼容拆层
- `evaluate_solution()` 现在会同时产出:
- 通用分支键:`branch.<branch_name>.p/in/out`
- 旧兼容键:`mypipe.p`、`mypipe1.p`、`branch_upper.*`、`branch_lower.*`
- 报告层当前已开始优先读取通用分支键,旧键只作为兼容后备
- 当前已经把“内部统一表达”和“旧接口兼容导出”拆成两层,但还没有把所有报告/导出逻辑都迁干净
5. `G5`:已完成当前阶段首轮兼容收口
- `evaluate_solution()` 当前会先生成通用分支键,再统一派生旧兼容键
- 报告层当前已支持“通用键优先、旧键兼容后备”
- 当前已经把系统层和 reporting 层的主要旧专名读取入口收口到少量 helper 上,后续继续迁移不会再到处散改
6. `P1`:下一阶段建议从这里接手
当前更合适的下一步,不是继续深挖内核通用化,而是切回结果导向主线:
- 定义一份稳定的外部输入参数 schema
- 明确这些结构化参数如何映射到 `TestModelConfig / TestModelRunConfig`
- 建立“结构化参数 -> 仿真执行 -> 结果产物/摘要”的稳定接口
这样可以直接服务后续文档解析、网页入口和报告生成,而不是继续在 `Testmodel` 内部做边际收益越来越低的抽象整理
7. `P2`:在 `P1` 完成后,再推进文档解析或报告生成链路
更现实的顺序应是:
- 先把结构化输入跑通
- 再把结果摘要/产物组织成更接近最终产品的输出包
- 最后再接 Word 解析或页面入口
如果后续继续推进,这个 README 也要一起更新,不要长期保留已经失效的路线描述。
## 当前实现了什么
当前代码已经实现:
1. `m`、`U` 作为动态元件主状态,`p`、`T`、`rho`、`u`、`h` 作为派生量。
2. `Cylinder`、`Tank`、`Pipe` 的刚性绝热容腔近似。
3. `Orifice` 的压差开方流量关系。
4. `Tee` 的简化混合焓处理。
5. `Testmodel` 的系统级拓扑映射和一版可运行的 `rhs(t, x)`。
6. 基于 `solve_ivp` 的积分入口,以及 SciPy 不可用时的 RK4 回退。
7. 温度相关空气近似介质,包括 `cp(T)`、`h(T)`、`u(T)` 以及 `u -> T` 反解。
8. 显式一致初值入口 `consistent_initial_state_vector()`,以及可迭代初始化器 `initialize_consistent_state()`。
9. Python 主变量结果导出:
`mytank.p`、`mytank.T`、`mycylinder.p`、`mycylinder.T`
10. 贮箱温度曲线导出:
`testmodel_tank_temperature.csv`
`testmodel_tank_temperature.svg`
11. 基于 `ModelicaModels/Simulation/Testmodel_res.csv` 的逐时刻对比与误差摘要导出。
12. 基于 `unittest` 的自动回归测试,当前已覆盖初始化守恒、主变量基线、运行接口、内部闭合诊断、通用分支兼容层、通用结果键与旧键别名一致性,以及部分中间闭合过程行为。
13. 面向 System XML v3 的拓扑驱动仿真 MVP:压力-流量非线性闭合、stream 焓传播、动态状态自动拼装和端口结果序列。
当前没有实现:
- 通用 DAE 初始化器
- `Modelica.Media.Air.SimpleAir` 的严格复刻
- 一般高指数 DAE、事件和严格 Modelica `inStream/actualStream` 求解器
## 当前怎么运行
最小运行方式:
```bash
python -m app.simulation.examples.testmodel.run
```
如果要改模型参数或运行参数,建议直接改配置对象,而不是改源码里的默认值。例如:
```python
from app.simulation.examples.testmodel.run import (
TestModelRunConfig,
TestModelSamplingConfig,
run_testmodel,
)
from app.simulation.examples.testmodel.system import (
BranchConfig,
CylinderConfig,
OrificeConfig,
PipeConfig,
TankConfig,
TestModelConfig,
)
from app.simulation.solvers.solver import SolveIVPConfig
run_config = TestModelRunConfig(
model=TestModelConfig(
cylinder=CylinderConfig(p0=30e6),
upper_branch=BranchConfig(
orifice=OrificeConfig(K=8e-6),
pipe=PipeConfig(length=6.0, diameter=0.03),
),
tank=TankConfig(volume=0.12),
),
solver=SolveIVPConfig(t_start=0.0, t_stop=10.0, method="BDF"),
sampling=TestModelSamplingConfig(step=0.05),
)
result = run_testmodel(run_config=run_config)
```
如果调用方想先确认“这次运行最后到底会用哪些路径、哪些采样点”,可以先准备请求,再执行:
```python
from app.simulation.examples.testmodel.run import (
prepare_testmodel_run,
run_prepared_testmodel,
TestModelRunConfig,
)
prepared = prepare_testmodel_run(run_config=TestModelRunConfig())
print(prepared.output_dir)
print(prepared.t_eval)
result = run_prepared_testmodel(prepared)
print(result.artifacts.primary_csv_path)
print(result.used_modelica_reference)
```
当前脚本会:
1. 构建 `TestModelSystem`
2. 打印原始初值向量与约束一致后的初值向量
3. 运行 `0 s -> 20 s` 的仿真,默认采样间隔 `0.1 s`
4. 将结果写入 `app/data/simulation-runs/` 下本次运行专属的时间戳目录
5. 若存在 `ModelicaModels/Simulation/Testmodel_res.csv`,自动生成 Python 与 OpenModelica 对比结果
当前脚本默认不会把运行结果直接写到提交基线目录,而是会在
`app/data/simulation-runs/` 下创建一个带时间戳的子目录,例如:
- `app/data/simulation-runs/testmodel_20260512_103000_123456/`
该目录里通常会包含:
- `testmodel_primary_series.csv`
- `testmodel_tank_temperature.csv`
- `testmodel_tank_temperature.svg`
- `testmodel_run_report.txt`
- `testmodel_modelica_comparison.csv`
- `testmodel_modelica_comparison_summary.txt`
## 基线结果
当前基线对比摘要来自:
[`testmodel_modelica_comparison_summary.txt`](../../tests/data/testmodel/testmodel_modelica_comparison_summary.txt)
当前四个主变量的最大误差为:
- `mytank.p`: `max_abs_error = 134.960858 Pa`, `max_rel_error = 0.006798%`
- `mytank.T`: `max_abs_error = 0.035507 K`, `max_rel_error = 0.009016%`
- `mycylinder.p`: `max_abs_error = 1391.986349 Pa`, `max_rel_error = 0.009447%`
- `mycylinder.T`: `max_abs_error = 0.009069 K`, `max_rel_error = 0.003870%`
这说明在当前基线工况下,Python 版主变量已经能较好贴近 OpenModelica 结果。
## AMESim test_mql 当前进度
`test_mql` 从 `AmesimModels/test_mql.ame` 迁移,并与旧 `testmodel` 保持独立。
固定算例实现统一位于 `examples/test_mql/`,结果读取和比较能力位于
`reporting/`;公开拖拽组件由 `components/amesim/library.py` 单独登记。
当前已形成 112 个气动状态和 20 个机械状态的总闭包、AMESim 原生结果读取、
`Data_Path` 输出校验及短时域 comparison。这里不再复制易过期的数值进度;
最新对比结果、运行命令、限制和下一步校准路径以
[`AmesimModels/test_mql/README.md`](../../AmesimModels/test_mql/README.md)
为唯一说明。当前仍不能宣称 Python 时域仿真与 AMESim 全局一致。
## Testmodel 当前架构判断
如果按“组件正确 -> 网络闭合 -> 积分可跑 -> 结果对齐 -> 去近似”来看,当前大致处于:
- 组件级:已完成首版
- 系统闭合:已完成首版
- 积分入口:已完成首版
- 基线结果对齐:已具备初步能力
- 去近似:仍在进行中
所以当前最准确的说法不是“已完成移植”,而是:
`Testmodel` 已有一版可运行、可导出、可对比的 Python 近似实现。
## Testmodel 已知限制
当前最主要的限制可以直接理解成下面几条:
- 介质模型已从常 `cp/cv` 推进到温度相关空气近似,但仍不是 `Modelica.Media.Air.SimpleAir` 的严格复刻。
- 系统整体仍是 ODE 化近似,不是原始 Modelica DAE 的直接复现。
- `mytee1 -> mytank` 这一段虽然已经去掉早期的“虚拟出口导通系数”,改成了基于压力一致性的下游能量闭合,但本质上仍是工程近似。
- 通用 XML 求解链路已经支持按实际流向传播和三通混合 stream 焓,但仍是正则化 MVP,不是严格的 Modelica `inStream/actualStream` 框架。
- 当前一致初值仍是 ODE 入口处的约束投影,不等同于真正的 DAE 初始化求解。
- 当前自动校验主要锁的是 Python 提交基线,还不是稳定的 Modelica 阈值回归。
- 当前闭合器、系统层和 reporting 层虽然已经开始做“双支路结构化”,但对外结果序列、报告字段和部分导出命名仍然保留 `Testmodel` 专名兼容层,还没有完全转成通用表达。
- 当前内核已经足够支撑下一阶段“结构化参数 -> 仿真执行 -> 产物输出”的链路开发,但还没有现成的 Word 参数解析入口和正式报告生成链路。
所以,当前版本适合:
- 架构验证
- 组件接口验证
- 基线工况对比
- 结果导出与误差定位
但当前版本还不适合:
- 直接宣称与 OpenModelica 严格等价
- 作为最终工程结论的唯一依据
- 直接扩展到更复杂拓扑而不补通用连接器语义
## Testmodel 文件级现状
按代码现状逐项看:
- `core/base.py`: 正常
只提供最小抽象层,没有明显冗余。
- `core/ports.py`: 正常
`PortState` 目前只保留 `p`、`m_flow`、`h_outflow` 三个必要字段。
- `core/state.py`: 正常
`VolumeState` 只负责 `[m, U]` 状态打包。
- `systems/network.py`: 正常
负责状态向量拼装和连接摘要,不参与物理求解。
- `solvers/solver.py`: 正常
已支持 SciPy、RK4 回退和零时长仿真。
- `components/experimental/**/*.py`: 正常
都是当前一版近似模型,没有发现与 README 明显冲突的“未记录能力”。
- `examples/testmodel/system.py`: 是当前最重要的技术债集中区
这里承载了下游流向切换、焓混合、压力投影等近似逻辑,后续演进应主要落在这里。
- `examples/testmodel/run.py`: 正常
已不是“最小打印脚本”,而是当前结果导出和对比入口。
- `tests/baselines/simulation/`: 是当前稳定基线,不应该随着日常运行频繁改动。
- `app/data/simulation-runs/`: 是默认运行产物目录,不是手写源代码,也不应该提交。
## Testmodel 当前主技术债
目前最主要的技术债,可以直接理解成下面 4 件事:
1. 当前初始化虽然已经引入迭代诊断,但本质上仍是 ODE 入口近似,不是真正的 DAE 初始化器。
2. `examples/testmodel/system.py` 还是承载了太多系统级闭合和初始化逻辑,只是主要端口的手写 stream 方向判断已经搬到组件 helper 里了,装配参数本身已经基本收口到配置对象。
3. 自动校验现在主要锁的是 Python 这一版自己的基线,还不是稳定的 Modelica 阈值回归。
4. 当前空气物性已经完成首轮基线校准,但还不是 `SimpleAir` 的严格复刻。以后如果换工况,或者拿到更多 Modelica 原始结果,参数大概率还要继续调。
运行、支持范围与依赖见 [C 后端说明](../../native/README.md)。模型开发规则见 [组件规范](../../docs/standard/component-model-authoring-spec-v1.md)。历史性能、Amesim 差异和旧公式说明位于 `docs/other/` 及 Git 历史,不能作为当前运行入口。
+37
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@@ -0,0 +1,37 @@
"""One execution boundary shared by XML API and native validation tools."""
from __future__ import annotations
import os
from app.simulation.config import SolveIVPConfig
DEFAULT_NUMERIC_ENGINE = "native"
def numeric_engine_name(backend: str | None = None) -> str:
configured = backend or os.environ.get("SIMULATION_NUMERIC_ENGINE", "")
selected = configured.strip().lower() or DEFAULT_NUMERIC_ENGINE
if selected == "native-c":
return "native"
if selected == "native":
return selected
if selected == "python":
raise ValueError("The Python numerical backend has been removed. Use SIMULATION_NUMERIC_ENGINE=native.")
raise ValueError(f"Unknown simulation engine: {selected}.")
def simulation_config(simulation) -> SolveIVPConfig:
# Preserve the existing XML execution accuracy. The XML
# protocol's future tolerance fields are a separate compatibility change.
return SolveIVPConfig(t_start=simulation.t_start, t_stop=simulation.t_stop,
method=simulation.method, rtol=1e-6, max_step=simulation.max_step)
def simulate_network(network, simulation, *, progress_callback=None,
cancel_check=None, activity_tracker=None, backend=None):
numeric_engine_name(backend)
config = simulation_config(simulation)
from app.simulation.native_codegen.runner import simulate_native
return simulate_native(network, config, sample_step=simulation.sample_step, progress_callback=progress_callback,
cancel_check=cancel_check, activity_tracker=activity_tracker)
-244
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@@ -1,244 +0,0 @@
from __future__ import annotations
import argparse
import hashlib
import importlib
import json
import os
import platform
import statistics
import sys
from datetime import UTC, datetime
from math import ceil
from pathlib import Path
from time import perf_counter_ns, process_time_ns
from typing import Any
def _named_value(value: str, *, option: str) -> tuple[str, str]:
name, separator, target = value.partition("=")
if not separator or not name.strip() or not target.strip():
raise ValueError(
f"{option} must use NAME=VALUE syntax, received {value!r}."
)
return name.strip(), target.strip()
def _percentile(values: list[float], percentile: float) -> float:
ordered = sorted(values)
index = max(0, min(len(ordered) - 1, ceil(percentile * len(ordered)) - 1))
return ordered[index]
def _duration_summary(values: list[float]) -> dict[str, object]:
return {
"samplesMs": values,
"minimumMs": min(values),
"medianMs": statistics.median(values),
"p95Ms": _percentile(values, 0.95),
"maximumMs": max(values),
}
def _load_factory_xml(specification: str) -> bytes:
module_name, separator, member_name = specification.partition(":")
if not separator or not module_name or not member_name:
raise ValueError(
"Factory specifications must use module.path:callable syntax."
)
factory = getattr(importlib.import_module(module_name), member_name)
value = factory()
if isinstance(value, bytes):
return value
if isinstance(value, str):
return value.encode("utf-8")
from app.main import build_reactflow_system_xml
return build_reactflow_system_xml(value)
def _serialize_result_event(result: dict[str, object]) -> bytes:
"""Render the final NDJSON payload shape used by the streaming endpoint."""
status = str(result.get("status", "completed"))
event = {
"event": "result",
"progress": 100 if status == "completed" else 0,
"phase": status,
"message": "仿真完成" if status == "completed" else "仿真任务结束",
"simulatedTime": result.get("simulatedUntil"),
"totalTime": result.get("requestedStopTime"),
"result": result,
}
return (
json.dumps(event, ensure_ascii=False, separators=(",", ":")) + "\n"
).encode("utf-8")
def _run_case(
name: str,
xml_bytes: bytes,
*,
warmups: int,
runs: int,
cancellable_path: bool,
allow_failures: bool,
) -> dict[str, object]:
from app.main import run_system_xml_simulation
cancel_check = (lambda: False) if cancellable_path else None
for _ in range(warmups):
result = run_system_xml_simulation(xml_bytes, cancel_check=cancel_check)
if not bool(result.get("success")) and not allow_failures:
raise RuntimeError(f"Warmup for {name!r} failed: {result.get('message')}")
wall_samples_ms: list[float] = []
cpu_samples_ms: list[float] = []
serialization_samples_ms: list[float] = []
serialized_sizes: list[int] = []
profiles: list[dict[str, object]] = []
final_result: dict[str, object] | None = None
for _ in range(runs):
wall_start = perf_counter_ns()
cpu_start = process_time_ns()
result = run_system_xml_simulation(xml_bytes, cancel_check=cancel_check)
cpu_samples_ms.append((process_time_ns() - cpu_start) / 1_000_000.0)
wall_samples_ms.append((perf_counter_ns() - wall_start) / 1_000_000.0)
if not bool(result.get("success")) and not allow_failures:
raise RuntimeError(f"Benchmark for {name!r} failed: {result.get('message')}")
diagnostics = result.get("diagnostics")
if isinstance(diagnostics, dict):
performance = diagnostics.get("performance")
if isinstance(performance, dict):
profiles.append(performance)
serialization_start = perf_counter_ns()
serialized_event = _serialize_result_event(result)
serialization_samples_ms.append(
(perf_counter_ns() - serialization_start) / 1_000_000.0
)
serialized_sizes.append(len(serialized_event))
final_result = result
assert final_result is not None
return {
"name": name,
"success": bool(final_result.get("success")),
"message": final_result.get("message"),
"inputBytes": len(xml_bytes),
"inputSha256": hashlib.sha256(xml_bytes).hexdigest(),
"status": final_result.get("status"),
"simulatedUntil": final_result.get("simulatedUntil"),
"requestedStopTime": final_result.get("requestedStopTime"),
"wall": _duration_summary(wall_samples_ms),
"cpu": _duration_summary(cpu_samples_ms),
"resultSerialization": _duration_summary(serialization_samples_ms),
"resultEventBytes": serialized_sizes,
"performanceRuns": profiles,
}
def _parse_arguments(argv: list[str] | None = None) -> argparse.Namespace:
parser = argparse.ArgumentParser(
description="Benchmark the real System XML simulation path with optional profiling."
)
parser.add_argument(
"--mode",
choices=("off", "standard", "audit"),
default="audit",
help="Instrumentation depth selected before importing the simulation modules.",
)
parser.add_argument("--warmups", type=int, default=1)
parser.add_argument("--runs", type=int, default=5)
parser.add_argument(
"--xml",
action="append",
default=[],
metavar="NAME=PATH",
help="Add an XML file benchmark case.",
)
parser.add_argument(
"--factory",
action="append",
default=[],
metavar="NAME=MODULE:CALLABLE",
help="Add a zero-argument factory returning XML or ReactFlowProjectPayload.",
)
parser.add_argument(
"--direct-path",
action="store_true",
help="Do not pass a cancel callback; use the one-shot SciPy path when eligible.",
)
parser.add_argument(
"--disable-property-cache",
action="store_true",
help="Disable the run-local exact property cache for an A/B comparison.",
)
parser.add_argument(
"--allow-failures",
action="store_true",
help="Record failed simulation runs instead of aborting the benchmark.",
)
parser.add_argument("--output", type=Path)
arguments = parser.parse_args(argv)
if arguments.warmups < 0:
parser.error("--warmups must not be negative.")
if arguments.runs <= 0:
parser.error("--runs must be positive.")
if not arguments.xml and not arguments.factory:
parser.error("At least one --xml or --factory case is required.")
return arguments
def main(argv: list[str] | None = None) -> int:
arguments = _parse_arguments(argv)
os.environ["SIMULATIONAPP_PROFILE"] = arguments.mode
os.environ["SIMULATIONAPP_PROPERTY_CACHE"] = (
"off" if arguments.disable_property_cache else "on"
)
cases: list[tuple[str, bytes]] = []
for raw_case in arguments.xml:
name, raw_path = _named_value(raw_case, option="--xml")
cases.append((name, Path(raw_path).read_bytes()))
for raw_case in arguments.factory:
name, specification = _named_value(raw_case, option="--factory")
cases.append((name, _load_factory_xml(specification)))
report: dict[str, Any] = {
"generatedAt": datetime.now(UTC).isoformat(),
"profileMode": arguments.mode,
"cancellableSolverPath": not arguments.direct_path,
"propertyCacheEnabled": not arguments.disable_property_cache,
"allowFailures": bool(arguments.allow_failures),
"warmups": arguments.warmups,
"runs": arguments.runs,
"runtime": {
"python": sys.version,
"platform": platform.platform(),
"processor": platform.processor(),
},
"cases": [
_run_case(
name,
xml_bytes,
warmups=arguments.warmups,
runs=arguments.runs,
cancellable_path=not arguments.direct_path,
allow_failures=arguments.allow_failures,
)
for name, xml_bytes in cases
],
}
text = json.dumps(report, ensure_ascii=False, indent=2)
if arguments.output is not None:
arguments.output.parent.mkdir(parents=True, exist_ok=True)
arguments.output.write_text(text + "\n", encoding="utf-8")
print(f"Performance report written to {arguments.output.resolve()}")
else:
print(text)
return 0
if __name__ == "__main__":
raise SystemExit(main())
File diff suppressed because it is too large. Load diff
@@ -1,14 +1,11 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping
from app.simulation.core.base import AlgebraicComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.medium import IdealGasMedium
from app.simulation.core.ports import PortDefinition
class AmesimPnpl01(AlgebraicComponent):
"""AMESim PNPL01 zero pneumatic flow source.
@@ -16,53 +13,19 @@ class AmesimPnpl01(AlgebraicComponent):
solver: it does not prescribe pressure, and only constrains its port mass
flow to zero.
"""
MODEL_TYPE = "amesim_pnpl01"
MODEL_VERSION = "0.1.0"
PRESSURE_FLOW_DEPENDS_ON_STREAM = False
PORTS = (PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),)
MODEL_TYPE = 'amesim_pnpl01'
MODEL_VERSION = '0.1.0'
PORTS = (PortDefinition.pneumatic('port_1', nominal_role='bidirectional'),)
PARAMETERS = ()
RESULT_VARIABLES = ()
DISPLAY = ComponentDisplaySpec(
label="PNPL01 零气动流边界",
library_id="amesim",
category_id="boundary",
symbol="amesim_pnpl01",
ports=(PortDisplaySpec("port_1", "left", order=10),),
order=10,
)
DISPLAY = ComponentDisplaySpec(label='PNPL01 零气动流边界', library_id='amesim', category_id='boundary', symbol='amesim_pnpl01', ports=(PortDisplaySpec('port_1', 'left', order=10),), order=10)
def __init__(self, name: str) -> None:
super().__init__(name=name)
self.set_parameter_values({})
self.port_1 = self.register_declared_port("port_1")
self.port_1 = self.register_declared_port('port_1')
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> AmesimPnpl01:
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> AmesimPnpl01:
return cls(name=name)
def pressure_flow_equation_values(self) -> tuple[float, ...]:
return (self.port_1.m_flow,)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
return (
EquationResidual(
id=f"{self.name}:zero_mass_flow",
owner="component",
owner_id=self.name,
relation="constitutive",
variables=(f"{self.name}.port_1.m_flow",),
role="flow",
value=self.port_1.m_flow,
),
)
def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
if "port_1" in connected_h:
self.port_1.h_outflow = connected_h["port_1"]
EQUATIONS = ({'id': '__MODEL__:zero_mass_flow', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'constitutive', 'variables': ['__MODEL__.port_1.m_flow'], 'role': 'flow'},)
File diff suppressed because it is too large. Load diff
File diff suppressed because it is too large. Load diff
@@ -1,31 +1,10 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping
from app.simulation.core.base import AlgebraicComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.medium import IdealGasMedium
from app.simulation.core.ports import PortDefinition, PortState
_REFERENCE_OUTFLOW_REGULARIZATION_RATIO = 0.05
def _regularized_inverse_outflow(flow: float, transition_flow: float) -> float:
"""Return a C1 inverse that tends to zero as a negative flow vanishes."""
if flow >= 0.0:
return 0.0
transition_flow = max(float(transition_flow), 1.0e-12)
if -flow >= transition_flow:
return 1.0 / flow
return (
flow
* (2.0 * transition_flow * transition_flow - flow * flow)
/ transition_flow**4
)
from app.simulation.core.ports import PortDefinition
class _AmesimPneumaticNode(AlgebraicComponent):
"""Shared implementation for AMESim pneumatic junction submodels.
@@ -35,9 +14,7 @@ class _AmesimPneumaticNode(AlgebraicComponent):
an outlet, its enthalpy is the residual that closes the junction energy
balance, matching the AMESim dh2 causality.
"""
PRESSURE_FLOW_DEPENDS_ON_STREAM = False
REFERENCE_PORT = "port_2"
REFERENCE_PORT = 'port_2'
def __init__(self, name: str) -> None:
super().__init__(name=name)
@@ -46,194 +23,30 @@ class _AmesimPneumaticNode(AlgebraicComponent):
for definition in self.PORTS:
setattr(self, definition.name, self.register_declared_port(definition.name))
def pressure_flow_equation_values(self) -> tuple[float, ...]:
reference = self.get_port(self.REFERENCE_PORT)
return tuple(
self.get_port(definition.name).p - reference.p
for definition in self.PORTS
if definition.name != self.REFERENCE_PORT
) + (
sum(
self.get_port(definition.name).m_flow
for definition in self.PORTS
),
)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
reference = self.get_port(self.REFERENCE_PORT)
residuals: list[EquationResidual] = []
for definition in self.PORTS:
if definition.name == self.REFERENCE_PORT:
continue
port = self.get_port(definition.name)
residuals.append(
EquationResidual(
id=f"{self.name}:{definition.name}_pressure_reference",
owner="component",
owner_id=self.name,
relation="equal",
variables=(
f"{self.name}.{definition.name}.p",
f"{self.name}.{self.REFERENCE_PORT}.p",
),
role="effort",
value=port.p - reference.p,
)
)
residuals.append(
EquationResidual(
id=f"{self.name}:mass_flow_balance",
owner="component",
owner_id=self.name,
relation="sumToZero",
variables=tuple(
f"{self.name}.{definition.name}.m_flow"
for definition in self.PORTS
),
role="flow",
value=sum(self.get_port(definition.name).m_flow for definition in self.PORTS),
)
)
return tuple(residuals)
def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
self.temperature_reference_h = connected_h.get(
self.REFERENCE_PORT,
sum(connected_h.values()) / len(connected_h) if connected_h else 0.0,
)
incoming = [
(port.m_flow, connected_h[name])
for name, port in self.ports.items()
if port.m_flow > 1e-12
]
total_flow = sum(m_flow for m_flow, _ in incoming)
if total_flow > 1e-12:
mixed_h = sum(m_flow * h for m_flow, h in incoming) / total_flow
else:
mixed_h = self.temperature_reference_h
reference_port = self.get_port(self.REFERENCE_PORT)
for name, port in self.ports.items():
port.h_outflow = (
mixed_h
if name == self.REFERENCE_PORT
else self.temperature_reference_h
)
if reference_port.m_flow < 0.0:
energy_without_reference = sum(
port.m_flow
* (
connected_h[name]
if port.m_flow > 1e-12
else self.temperature_reference_h
)
for name, port in self.ports.items()
if name != self.REFERENCE_PORT
)
non_reference_flow_scale = sum(
abs(port.m_flow)
for name, port in self.ports.items()
if name != self.REFERENCE_PORT
)
transition_flow = (
_REFERENCE_OUTFLOW_REGULARIZATION_RATIO
* non_reference_flow_scale
)
# Port 2 carries AMESim's residual-energy causality. Exact
# division is singular when its outflow reverses through zero, so
# use a C1 band that matches the exact balance at its boundary and
# tends to the mixed enthalpy at zero flow.
inverse_flow = _regularized_inverse_outflow(
reference_port.m_flow,
transition_flow,
)
energy_residual_at_mixed_h = (
energy_without_reference
+ reference_port.m_flow * mixed_h
)
reference_port.h_outflow = (
mixed_h - energy_residual_at_mixed_h * inverse_flow
)
class AmesimPn3Node2(_AmesimPneumaticNode):
"""AMESim PN3NODE2 pneumatic three-port junction."""
MODEL_TYPE = "amesim_pn3node2"
MODEL_VERSION = "0.3.0"
PRESSURE_FLOW_DEPENDS_ON_STREAM = False
PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
("mass_flow_balance",)
)
PORTS = (
PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_3", nominal_role="bidirectional"),
)
MODEL_TYPE = 'amesim_pn3node2'
MODEL_VERSION = '0.3.0'
PORTS = (PortDefinition.pneumatic('port_1', nominal_role='bidirectional'), PortDefinition.pneumatic('port_2', nominal_role='bidirectional'), PortDefinition.pneumatic('port_3', nominal_role='bidirectional'))
PARAMETERS = ()
RESULT_VARIABLES = ()
DISPLAY = ComponentDisplaySpec(
label="PN3NODE2 三端气动节点",
library_id="amesim",
category_id="junctions",
symbol="amesim_pn3node2",
ports=(
PortDisplaySpec("port_1", "left", order=10),
PortDisplaySpec("port_2", "right", order=20),
PortDisplaySpec("port_3", "right", order=30),
),
order=10,
)
DISPLAY = ComponentDisplaySpec(label='PN3NODE2 三端气动节点', library_id='amesim', category_id='junctions', symbol='amesim_pn3node2', ports=(PortDisplaySpec('port_1', 'left', order=10), PortDisplaySpec('port_2', 'right', order=20), PortDisplaySpec('port_3', 'right', order=30)), order=10)
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> AmesimPn3Node2:
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> AmesimPn3Node2:
return cls(name=name)
EQUATIONS = ({'id': '__MODEL__:port_1_pressure_reference', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_1.p', '__MODEL__.port_2.p'], 'role': 'effort'}, {'id': '__MODEL__:port_3_pressure_reference', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_3.p', '__MODEL__.port_2.p'], 'role': 'effort'}, {'id': '__MODEL__:mass_flow_balance', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'sumToZero', 'variables': ['__MODEL__.port_1.m_flow', '__MODEL__.port_2.m_flow', '__MODEL__.port_3.m_flow'], 'role': 'flow'})
class AmesimP4Node2(_AmesimPneumaticNode):
"""AMESim P4NODE2 pneumatic four-port junction."""
MODEL_TYPE = "amesim_p4node2"
MODEL_VERSION = "0.3.0"
PRESSURE_FLOW_DEPENDS_ON_STREAM = False
PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
("mass_flow_balance",)
)
PORTS = (
PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_3", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_4", nominal_role="bidirectional"),
)
MODEL_TYPE = 'amesim_p4node2'
MODEL_VERSION = '0.3.0'
PORTS = (PortDefinition.pneumatic('port_1', nominal_role='bidirectional'), PortDefinition.pneumatic('port_2', nominal_role='bidirectional'), PortDefinition.pneumatic('port_3', nominal_role='bidirectional'), PortDefinition.pneumatic('port_4', nominal_role='bidirectional'))
PARAMETERS = ()
RESULT_VARIABLES = ()
DISPLAY = ComponentDisplaySpec(
label="P4NODE2 四端气动节点",
library_id="amesim",
category_id="junctions",
symbol="amesim_p4node2",
ports=(
PortDisplaySpec("port_1", "left", order=10),
PortDisplaySpec("port_2", "right", order=20),
PortDisplaySpec("port_3", "right", order=30),
PortDisplaySpec("port_4", "right", order=40),
),
order=20,
)
DISPLAY = ComponentDisplaySpec(label='P4NODE2 四端气动节点', library_id='amesim', category_id='junctions', symbol='amesim_p4node2', ports=(PortDisplaySpec('port_1', 'left', order=10), PortDisplaySpec('port_2', 'right', order=20), PortDisplaySpec('port_3', 'right', order=30), PortDisplaySpec('port_4', 'right', order=40)), order=20)
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> AmesimP4Node2:
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> AmesimP4Node2:
return cls(name=name)
EQUATIONS = ({'id': '__MODEL__:port_1_pressure_reference', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_1.p', '__MODEL__.port_2.p'], 'role': 'effort'}, {'id': '__MODEL__:port_3_pressure_reference', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_3.p', '__MODEL__.port_2.p'], 'role': 'effort'}, {'id': '__MODEL__:port_4_pressure_reference', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_4.p', '__MODEL__.port_2.p'], 'role': 'effort'}, {'id': '__MODEL__:mass_flow_balance', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'sumToZero', 'variables': ['__MODEL__.port_1.m_flow', '__MODEL__.port_2.m_flow', '__MODEL__.port_3.m_flow', '__MODEL__.port_4.m_flow'], 'role': 'flow'})
@@ -1,36 +1,15 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping, Sequence
from dataclasses import dataclass
from math import isfinite, pi
from app.simulation.components.amesim.gases import (
AMESIM_GAS_INDEX_PARAMETER,
normalize_amesim_gas_index,
)
from collections.abc import Mapping
from math import pi
from app.simulation.components.amesim.gases import AMESIM_GAS_INDEX_PARAMETER, normalize_amesim_gas_index
from app.simulation.core.base import AlgebraicComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import ParameterDefinition, ResultVariableDefinition
from app.simulation.core.medium import GasMedium
from app.simulation.core.ports import PortDefinition
AMESIM_REFERENCE_PRESSURE_PA = 101300.0
@dataclass(frozen=True)
class Pnrp17Linearization:
volume: float
volume_flow: float
pressure_force: float
volume_tangent: tuple[float, ...]
volume_flow_tangent: tuple[float, ...]
pressure_force_tangent: tuple[float, ...]
valid: bool = True
reason: str | None = None
class AmesimPnrp17(AlgebraicComponent):
"""AMESim PNRP17 pneumatic piston with two mechanical faces.
@@ -38,268 +17,32 @@ class AmesimPnrp17(AlgebraicComponent):
cylinder-side motion. The pneumatic port contributes its swept volume and
volume rate to the connected variable-volume chamber.
"""
MODEL_TYPE = 'amesim_pnrp17'
MODEL_VERSION = '0.1.0'
PORTS = (PortDefinition.pneumatic('port_1', nominal_role='bidirectional'), PortDefinition.mechanical_translational('port_2'), PortDefinition.mechanical_translational('port_3'), PortDefinition.mechanical_translational('port_4'), PortDefinition.mechanical_translational('port_5'))
PARAMETERS = (AMESIM_GAS_INDEX_PARAMETER, ParameterDefinition('dp', 0.2, label='活塞直径', quantity='length', unit='m', minimum=0.0, minimum_exclusive=True, description='活塞外径;与活塞杆直径共同确定有效受压面积。'), ParameterDefinition('dr', 0.001, label='活塞杆直径', quantity='length', unit='m', minimum=0.0, description='穿过气室一侧的活塞杆直径,必须不大于活塞直径。'), ParameterDefinition('x0', 0.0, label='初始腔长', quantity='length', unit='m', description='机械端位移均为零时的气动腔长度。'))
RESULT_VARIABLES = (ResultVariableDefinition('volume', '扫掠容积', 'volume', 'm3', 'derived', 10), ResultVariableDefinition('volume_flow', '扫掠容积变化率', 'volume_flow', 'm3/s', 'derived', 20), ResultVariableDefinition('length', '气动腔长度', 'length', 'm', 'derived', 30), ResultVariableDefinition('pressure_force', '气压力', 'force', 'N', 'derived', 40))
DISPLAY = ComponentDisplaySpec(label='PNRP17 气动活塞', library_id='amesim', category_id='mechanical', symbol='amesim_pnrp17', ports=(PortDisplaySpec('port_1', 'left', order=10), PortDisplaySpec('port_3', 'left', order=20), PortDisplaySpec('port_2', 'left', order=30), PortDisplaySpec('port_4', 'right', order=40), PortDisplaySpec('port_5', 'right', order=50)), order=60)
MODEL_TYPE = "amesim_pnrp17"
MODEL_VERSION = "0.1.0"
PRESSURE_FLOW_DEPENDS_ON_STREAM = False
PORTS = (
PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
PortDefinition.mechanical_translational("port_2"),
PortDefinition.mechanical_translational("port_3"),
PortDefinition.mechanical_translational("port_4"),
PortDefinition.mechanical_translational("port_5"),
)
PARAMETERS = (
AMESIM_GAS_INDEX_PARAMETER,
ParameterDefinition(
"dp",
0.2,
label="活塞直径",
quantity="length",
unit="m",
minimum=0.0,
minimum_exclusive=True,
description="活塞外径;与活塞杆直径共同确定有效受压面积。",
),
ParameterDefinition(
"dr",
0.001,
label="活塞杆直径",
quantity="length",
unit="m",
minimum=0.0,
description="穿过气室一侧的活塞杆直径,必须不大于活塞直径。",
),
ParameterDefinition(
"x0",
0.0,
label="初始腔长",
quantity="length",
unit="m",
description="机械端位移均为零时的气动腔长度。",
),
)
RESULT_VARIABLES = (
ResultVariableDefinition("volume", "扫掠容积", "volume", "m3", "derived", 10),
ResultVariableDefinition(
"volume_flow",
"扫掠容积变化率",
"volume_flow",
"m3/s",
"derived",
20,
),
ResultVariableDefinition("length", "气动腔长度", "length", "m", "derived", 30),
ResultVariableDefinition(
"pressure_force",
"气压力",
"force",
"N",
"derived",
40,
),
)
DISPLAY = ComponentDisplaySpec(
label="PNRP17 气动活塞",
library_id="amesim",
category_id="mechanical",
symbol="amesim_pnrp17",
ports=(
PortDisplaySpec("port_1", "left", order=10),
PortDisplaySpec("port_3", "left", order=20),
PortDisplaySpec("port_2", "left", order=30),
PortDisplaySpec("port_4", "right", order=40),
PortDisplaySpec("port_5", "right", order=50),
),
order=60,
)
def __init__(
self,
name: str,
medium: GasMedium,
*,
gi: float = 0.0,
dp: float = 0.2,
dr: float = 0.001,
x0: float = 0.0,
) -> None:
def __init__(self, name: str, medium: GasMedium, *, gi: float=0.0, dp: float=0.2, dr: float=0.001, x0: float=0.0) -> None:
super().__init__(name=name)
self.set_parameter_values({"gi": gi, "dp": dp, "dr": dr, "x0": x0})
self.set_parameter_values({'gi': gi, 'dp': dp, 'dr': dr, 'x0': x0})
self.medium = medium
self.gi = normalize_amesim_gas_index(gi)
self.dp = float(dp)
self.dr = float(dr)
self.x0 = float(x0)
if self.dr > self.dp:
raise ValueError("PNRP17 rod diameter dr must not exceed piston diameter dp.")
raise ValueError('PNRP17 rod diameter dr must not exceed piston diameter dp.')
for definition in self.PORTS:
port = self.register_declared_port(definition.name)
setattr(self, definition.name, port)
self.port_1.h_outflow = medium.specific_enthalpy(medium.T_ref)
@classmethod
def create(
cls,
*,
name: str,
medium: GasMedium,
parameters: Mapping[str, float],
) -> "AmesimPnrp17":
def create(cls, *, name: str, medium: GasMedium, parameters: Mapping[str, float]) -> 'AmesimPnrp17':
return cls(name=name, medium=medium, **dict(parameters))
@property
def effective_area(self) -> float:
return pi * (self.dp * self.dp - self.dr * self.dr) / 4.0
@property
def chamber_length(self) -> float:
return self.x0 + self.port_5.x - self.port_4.x
@property
def chamber_volume(self) -> float:
return self.effective_area * self.chamber_length
@property
def chamber_volume_flow(self) -> float:
return self.effective_area * (self.port_5.v - self.port_4.v)
@property
def pressure_force(self) -> float:
return (self.port_1.p - AMESIM_REFERENCE_PRESSURE_PA) * self.effective_area
def pressure_flow_equation_values(self) -> tuple[float, ...]:
values = [self.port_1.m_flow]
effort_pairs = (("port_2", "port_5"), ("port_3", "port_4"))
for first_name, second_name in effort_pairs:
first = self.get_port(first_name)
second = self.get_port(second_name)
values.extend((first.x - second.x, first.v - second.v))
force = self.pressure_force
values.extend(
(
self.port_2.f + self.port_5.f + force,
self.port_3.f + self.port_4.f - force,
)
)
return tuple(values)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
effort_pairs = (("port_2", "port_5"), ("port_3", "port_4"))
residuals: list[EquationResidual] = [
EquationResidual(
id=f"{self.name}:pneumatic_zero_mass_flow",
owner="component",
owner_id=self.name,
relation="constitutive",
variables=(f"{self.name}.port_1.m_flow",),
role="flow",
value=self.port_1.m_flow,
)
]
for first_name, second_name in effort_pairs:
first = self.get_port(first_name)
second = self.get_port(second_name)
for variable in ("x", "v"):
residuals.append(
EquationResidual(
id=f"{self.name}:{first_name}_{second_name}_{variable}_equal",
owner="component",
owner_id=self.name,
relation="equal",
variables=(
f"{self.name}.{first_name}.{variable}",
f"{self.name}.{second_name}.{variable}",
),
role="effort",
value=getattr(first, variable) - getattr(second, variable),
)
)
force = self.pressure_force
residuals.extend(
(
EquationResidual(
id=f"{self.name}:piston_side_force_balance",
owner="component",
owner_id=self.name,
relation="constitutive",
variables=(f"{self.name}.port_2.f", f"{self.name}.port_5.f", f"{self.name}.port_1.p"),
role="flow",
value=self.port_2.f + self.port_5.f + force,
),
EquationResidual(
id=f"{self.name}:cylinder_side_force_balance",
owner="component",
owner_id=self.name,
relation="constitutive",
variables=(f"{self.name}.port_3.f", f"{self.name}.port_4.f", f"{self.name}.port_1.p"),
role="flow",
value=self.port_3.f + self.port_4.f - force,
),
)
)
return tuple(residuals)
def pneumatic_volume_outputs(self) -> Mapping[str, tuple[float, float]]:
return {"port_1": (self.chamber_volume, self.chamber_volume_flow)}
def linearize_geometry_and_force(
self,
port_4_x_tangent: Sequence[float],
port_5_x_tangent: Sequence[float],
port_4_v_tangent: Sequence[float],
port_5_v_tangent: Sequence[float],
port_1_pressure_tangent: Sequence[float],
) -> Pnrp17Linearization:
"""Return exact piston geometry and pressure-force tangents."""
vectors = tuple(
tuple(float(value) for value in values)
for values in (
port_4_x_tangent,
port_5_x_tangent,
port_4_v_tangent,
port_5_v_tangent,
port_1_pressure_tangent,
)
)
widths = {len(values) for values in vectors}
if len(widths) != 1:
raise ValueError("PNRP17 tangent vectors must have equal lengths.")
valid = all(isfinite(value) for values in vectors for value in values)
area = self.effective_area
volume_tangent = tuple(
area * (right - left)
for left, right in zip(vectors[0], vectors[1], strict=True)
)
volume_flow_tangent = tuple(
area * (right - left)
for left, right in zip(vectors[2], vectors[3], strict=True)
)
pressure_force_tangent = tuple(
area * value for value in vectors[4]
)
return Pnrp17Linearization(
volume=self.chamber_volume,
volume_flow=self.chamber_volume_flow,
pressure_force=self.pressure_force,
volume_tangent=volume_tangent,
volume_flow_tangent=volume_flow_tangent,
pressure_force_tangent=pressure_force_tangent,
valid=valid,
reason=None if valid else "non_finite_tangent_input",
)
def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
self.port_1.h_outflow = connected_h.get(
"port_1",
self.medium.specific_enthalpy(self.medium.T_ref),
)
def component_result_values(self) -> Mapping[str, float]:
return {
"volume": self.chamber_volume,
"volume_flow": self.chamber_volume_flow,
"length": self.chamber_length,
"pressure_force": self.pressure_force,
}
EQUATIONS = ({'id': '__MODEL__:pneumatic_zero_mass_flow', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'constitutive', 'variables': ['__MODEL__.port_1.m_flow'], 'role': 'flow'}, {'id': '__MODEL__:port_2_port_5_x_equal', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_2.x', '__MODEL__.port_5.x'], 'role': 'effort'}, {'id': '__MODEL__:port_2_port_5_v_equal', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_2.v', '__MODEL__.port_5.v'], 'role': 'effort'}, {'id': '__MODEL__:port_3_port_4_x_equal', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_3.x', '__MODEL__.port_4.x'], 'role': 'effort'}, {'id': '__MODEL__:port_3_port_4_v_equal', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_3.v', '__MODEL__.port_4.v'], 'role': 'effort'}, {'id': '__MODEL__:piston_side_force_balance', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'constitutive', 'variables': ['__MODEL__.port_2.f', '__MODEL__.port_5.f', '__MODEL__.port_1.p'], 'role': 'flow'}, {'id': '__MODEL__:cylinder_side_force_balance', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'constitutive', 'variables': ['__MODEL__.port_3.f', '__MODEL__.port_4.f', '__MODEL__.port_1.p'], 'role': 'flow'})
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@@ -1,488 +1,42 @@
"""Gas identities and constants passed to the native compiler."""
from __future__ import annotations
from collections.abc import Callable, Sequence
from collections.abc import Callable
from dataclasses import dataclass
from math import exp, isfinite, log
from typing import ClassVar
from app.simulation.core.errors import RecoverableTrialStateError
from app.simulation.core.medium import (
GasMedium,
IdealGasMedium,
ThermodynamicProperties,
ThermodynamicPropertiesLinearization,
ThermodynamicPropertyTangents,
)
from app.simulation.core.peng_robinson import HELIUM_PR, PengRobinsonFluid
from app.simulation.performance import profile_property, record_property_iterations
from app.simulation.property_cache import cache_property_calculation
from app.simulation.core.medium import GasMedium, IdealGasMedium
@dataclass(frozen=True)
class AmesimIdealAirMedium(IdealGasMedium):
"""AMESim air properties evaluated with the ideal-gas method.
Substance identity and property method are part of the concrete Python
type. A future air correlation or helium Peng-Robinson implementation can
therefore coexist as a sibling type without turning ``gi`` into a fluid
enumeration.
"""
SUBSTANCE_ID: ClassVar[str] = "air"
PROPERTY_METHOD_ID: ClassVar[str] = "ideal_gas"
name: str = "AMESimAirIdealGas"
SUBSTANCE_ID: ClassVar[str] = 'air'
PROPERTY_METHOD_ID: ClassVar[str] = 'ideal_gas'
name: str = 'AMESimAirIdealGas'
R_gas: float = 287.0
cp_ref: float = 1005.0
T_ref: float = 300.0
cp_slope: float = 0.0
viscosity_ref: float = 1.82e-5
viscosity_ref: float = 1.82e-05
viscosity_T_ref: float = 293.15
sutherland_constant: float = 110.4
@dataclass(frozen=True)
class AmesimHeliumPengRobinsonMedium(IdealGasMedium):
"""AMESim helium with a Peng-Robinson mechanical equation of state.
The pressure-density-temperature relation is evaluated by the shared
``HELIUM_PR`` fluid. The caloric reference follows the constant NASA
polynomial from Simcenter Amesim 2404 ``helium_cp_h_s.data``.
"""
SUBSTANCE_ID: ClassVar[str] = "helium"
PROPERTY_METHOD_ID: ClassVar[str] = "peng_robinson"
fluid: ClassVar[PengRobinsonFluid] = HELIUM_PR
SUBSTANCE_ID: ClassVar[str] = 'helium'
PROPERTY_METHOD_ID: ClassVar[str] = 'peng_robinson'
nasa_cp_over_R: ClassVar[float] = 2.5
nasa_enthalpy_constant_K: ClassVar[float] = -745.375
nasa_viscosity_coefficients: ClassVar[tuple[float, float, float, float]] = (
0.7501594,
35.76324,
-2212.129,
0.9212635,
)
name: str = "AMESimHeliumPengRobinson"
R_gas: float = HELIUM_PR.specific_gas_constant
cp_ref: float = nasa_cp_over_R * HELIUM_PR.specific_gas_constant
nasa_viscosity_coefficients: ClassVar[tuple[float, float, float, float]] = (0.7501594, 35.76324, -2212.129, 0.9212635)
name: str = 'AMESimHeliumPengRobinson'
R_gas: float = 8.31446261815324 / 0.004002602
cp_ref: float = 2.5 * (8.31446261815324 / 0.004002602)
T_ref: float = 293.15
cp_slope: float = 0.0
viscosity_ref: float = 1.96e-5
viscosity_ref: float = 1.96e-05
viscosity_T_ref: float = 293.15
sutherland_constant: float = 79.4
@property
def cv(self) -> float:
return (self.nasa_cp_over_R - 1.0) * self.R_gas
def cv_at_temperature(self, T: float) -> float:
del T
return self.cv
def diagnostic_dynamic_viscosity(self, T: float) -> float:
"""Return the AMESim NASA-table viscosity used by pipe diagnostics.
pn2pipefr reports Reynolds number with sagum viscosity. Keep this
separate from dynamic_viscosity so matching that diagnostic cannot
alter the already-validated pipe flow or friction dynamics.
"""
if T <= 0.0:
raise ValueError("Temperature must be positive.")
a, b, c, d = self.nasa_viscosity_coefficients
return 1.0e-7 * exp(a * log(T) + b / T + c / (T * T) + d)
@profile_property("density")
@cache_property_calculation("density")
def density(self, p: float, T: float) -> float:
return self.fluid.density(p, T)
def _real_heat_capacities(
self,
p: float,
T: float,
) -> tuple[float, float, float, float, float]:
density = self.density(p, T)
pressure_density_derivative = (
self.fluid.pressure_density_derivative_at_temperature(
T,
density,
)
)
pressure_temperature_derivative = (
self.fluid.pressure_temperature_derivative_at_density(
T,
density,
)
)
cv = (
self.cv_at_temperature(T)
+ self.fluid.residual_isochoric_heat_capacity_at_density(T, density)
)
cp = (
cv
+ T
* pressure_temperature_derivative
* pressure_temperature_derivative
/ (density * density * pressure_density_derivative)
)
if cp <= 0.0 or cv <= 0.0:
raise ValueError("Real-gas heat capacities must be positive.")
return (
cp,
cv,
density,
pressure_density_derivative,
pressure_temperature_derivative,
)
def _local_isentropic_density_pressure_factor(
self,
p: float,
T: float,
) -> tuple[float, float]:
cp, cv, density, pressure_density_derivative, pressure_temperature_derivative = (
self._real_heat_capacities(p, T)
)
heat_capacity_ratio = cp / cv
factor = p / (
density * pressure_density_derivative * heat_capacity_ratio
)
exponent = (
p
* (heat_capacity_ratio - 1.0)
/ (
heat_capacity_ratio
* T
* pressure_temperature_derivative
)
)
return factor, exponent
@profile_property("isentropic_density_pressure_factor")
@cache_property_calculation("isentropic_density_pressure_factor")
def isentropic_density_pressure_factor(
self,
p: float,
T: float,
downstream_pressure: float | None = None,
) -> float:
upstream_factor, isentropic_temperature_exponent = (
self._local_isentropic_density_pressure_factor(p, T)
)
if downstream_pressure is None or downstream_pressure >= p:
return upstream_factor
pressure_ratio = max(downstream_pressure / p, 1.0e-12)
isentropic_temperature = max(
T * pressure_ratio**isentropic_temperature_exponent,
2.2,
)
downstream_factor, _unused_exponent = (
self._local_isentropic_density_pressure_factor(
max(downstream_pressure, 1.0),
isentropic_temperature,
)
)
# AMESim 2404 saggs_ evaluates the local factor at the upstream
# state and at an approximate isentropic downstream state.
return 0.5 * (upstream_factor + downstream_factor)
def pressure(self, m: float, T: float, V: float) -> float:
if V <= 0.0:
raise ValueError("Volume must stay positive.")
return self.fluid.pressure_from_density(T, m / V)
@profile_property("specific_internal_energy")
def specific_internal_energy(self, T: float) -> float:
return self.R_gas * (
(self.nasa_cp_over_R - 1.0) * T
+ self.nasa_enthalpy_constant_K
)
@profile_property("specific_internal_energy_at_pressure")
def specific_internal_energy_at_pressure(self, p: float, T: float) -> float:
density = self.density(p, T)
return (
self.specific_internal_energy(T)
+ self.fluid.residual_specific_internal_energy_at_density(T, density)
)
@profile_property("specific_enthalpy")
def specific_enthalpy(self, T: float) -> float:
return self.R_gas * (
self.nasa_cp_over_R * T
+ self.nasa_enthalpy_constant_K
)
@profile_property("specific_enthalpy_at_pressure")
def specific_enthalpy_at_pressure(self, p: float, T: float) -> float:
return self.specific_enthalpy(T) + self.fluid.residual_specific_enthalpy(p, T)
def temperature_from_internal_energy(self, u: float) -> float:
return (
u / self.R_gas - self.nasa_enthalpy_constant_K
) / (self.nasa_cp_over_R - 1.0)
def temperature_from_enthalpy(self, h: float) -> float:
return (
h / self.R_gas - self.nasa_enthalpy_constant_K
) / self.nasa_cp_over_R
@profile_property("temperature_from_pressure_enthalpy")
@cache_property_calculation("temperature_from_pressure_enthalpy")
def temperature_from_pressure_enthalpy(self, p: float, h: float) -> float:
temperature = max(self.temperature_from_enthalpy(h), 2.2)
for _iteration in range(16):
residual_enthalpy = self.fluid.residual_specific_enthalpy(p, temperature)
next_temperature = max(
self.temperature_from_enthalpy(h - residual_enthalpy),
2.2,
)
if abs(next_temperature - temperature) <= 1.0e-10 * max(
temperature,
1.0,
):
record_property_iterations(
"temperature_from_pressure_enthalpy",
_iteration + 1,
True,
)
return next_temperature
temperature = next_temperature
record_property_iterations(
"temperature_from_pressure_enthalpy",
16,
False,
)
return temperature
def temperature_from_mass_internal_energy(self, m: float, U: float) -> float:
if m <= 0.0:
raise RecoverableTrialStateError(
"Mass must stay positive when recovering temperature."
)
return self.temperature_from_internal_energy(U / m)
@profile_property("properties_from_mU")
@cache_property_calculation("properties_from_mU")
def properties_from_mU(
self,
m: float,
U: float,
V: float,
) -> ThermodynamicProperties:
"""Recover a real-gas state, reusing exact repeated evaluations.
Implicit integration asks several component interfaces for the same
``(m, U, V)`` state while closing one RHS evaluation and while building
finite-difference Jacobians. The calculation is pure and its result is
immutable, so an exact-key bounded cache avoids repeating the
Peng-Robinson temperature iteration without changing model semantics.
"""
if m <= 0.0:
raise RecoverableTrialStateError(
"Mass must stay positive when recovering temperature."
)
if V <= 0.0:
raise ValueError("Volume must stay positive.")
density = m / V
target_internal_energy = U / m
temperature = max(
self.temperature_from_internal_energy(target_internal_energy),
2.2,
)
converged = False
for _iteration in range(16):
residual_internal_energy = (
self.fluid.residual_specific_internal_energy_at_density(
temperature,
density,
)
)
next_temperature = max(
self.temperature_from_internal_energy(
target_internal_energy - residual_internal_energy
),
2.2,
)
if abs(next_temperature - temperature) <= 1.0e-10 * max(
temperature,
1.0,
):
temperature = next_temperature
converged = True
break
temperature = next_temperature
record_property_iterations(
"properties_from_mU",
_iteration + 1,
converged,
)
pressure = self.fluid.pressure_from_density(temperature, density)
return ThermodynamicProperties(
p=pressure,
T=temperature,
rho=density,
u=target_internal_energy,
h=self.specific_enthalpy_at_pressure(
pressure,
temperature,
),
)
def linearize_properties_from_mU(
self,
m: float,
U: float,
V: float,
dm: Sequence[float],
dU: Sequence[float],
dV: Sequence[float],
*,
properties: ThermodynamicProperties | None = None,
) -> ThermodynamicPropertiesLinearization:
"""Implicitly differentiate the Peng-Robinson m/U/V recovery."""
dm_values = tuple(float(value) for value in dm)
dU_values = tuple(float(value) for value in dU)
dV_values = tuple(float(value) for value in dV)
if not (len(dm_values) == len(dU_values) == len(dV_values)):
raise ValueError("Thermodynamic tangent vectors must have equal lengths.")
props = properties or self.properties_from_mU(m, U, V)
width = len(dm_values)
def invalid(reason: str) -> ThermodynamicPropertiesLinearization:
return ThermodynamicPropertiesLinearization(
properties=props,
tangents=ThermodynamicPropertyTangents.zeros(width),
valid=False,
reason=reason,
)
expected_density = m / V
expected_internal_energy = U / m
if (
abs(props.rho - expected_density)
> 1.0e-12 * max(abs(expected_density), 1.0)
or abs(props.u - expected_internal_energy)
> 1.0e-12 * max(abs(expected_internal_energy), 1.0)
):
return invalid("properties_primal_mismatch")
if not all(
isfinite(value)
for values in (dm_values, dU_values, dV_values)
for value in values
):
return invalid("non_finite_tangent_input")
if props.T <= 2.2 * (1.0 + 1.0e-10):
return invalid("temperature_floor_boundary")
pressure_temperature_derivative = (
self.fluid.pressure_temperature_derivative_at_density(
props.T,
props.rho,
)
)
pressure_density_derivative = (
self.fluid.pressure_density_derivative_at_temperature(
props.T,
props.rho,
)
)
cv = (
self.cv_at_temperature(props.T)
+ self.fluid.residual_isochoric_heat_capacity_at_density(
props.T,
props.rho,
)
)
recovered_internal_energy = (
self.specific_internal_energy(props.T)
+ self.fluid.residual_specific_internal_energy_at_density(
props.T,
props.rho,
)
)
recovery_scale = max(
abs(props.u),
abs(cv * props.T) if isfinite(cv) else 0.0,
1.0,
)
if (
not all(
isfinite(value)
for value in (
pressure_temperature_derivative,
pressure_density_derivative,
cv,
recovered_internal_energy,
)
)
or cv <= 0.0
):
return invalid("invalid_peng_robinson_derivative")
if abs(recovered_internal_energy - props.u) > 1.0e-8 * recovery_scale:
return invalid("properties_recovery_not_converged")
internal_energy_density_derivative = (
props.p - props.T * pressure_temperature_derivative
) / (props.rho * props.rho)
drho: list[float] = []
du: list[float] = []
dT: list[float] = []
dp: list[float] = []
dh: list[float] = []
for mass_tangent, energy_tangent, volume_tangent in zip(
dm_values,
dU_values,
dV_values,
strict=True,
):
density_tangent = (
mass_tangent / V - m * volume_tangent / (V * V)
)
internal_energy_tangent = (
energy_tangent / m - U * mass_tangent / (m * m)
)
temperature_tangent = (
internal_energy_tangent
- internal_energy_density_derivative * density_tangent
) / cv
pressure_tangent = (
pressure_temperature_derivative * temperature_tangent
+ pressure_density_derivative * density_tangent
)
enthalpy_tangent = (
internal_energy_tangent
+ pressure_tangent / props.rho
- props.p * density_tangent / (props.rho * props.rho)
)
drho.append(density_tangent)
du.append(internal_energy_tangent)
dT.append(temperature_tangent)
dp.append(pressure_tangent)
dh.append(enthalpy_tangent)
tangent_values = (*drho, *du, *dT, *dp, *dh)
if not all(isfinite(value) for value in tangent_values):
return invalid("non_finite_property_tangent")
return ThermodynamicPropertiesLinearization(
properties=props,
tangents=ThermodynamicPropertyTangents(
p=tuple(dp),
T=tuple(dT),
rho=tuple(drho),
u=tuple(du),
h=tuple(dh),
),
)
@dataclass(frozen=True)
class AmesimGasPropertyModelSpec:
"""A selectable calculation method for one AMESim gas substance."""
value: int
label: str
method_id: str
@@ -491,27 +45,7 @@ class AmesimGasPropertyModelSpec:
def build_medium(self) -> GasMedium:
return self.factory()
AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL = 0
AMESIM_AIR_PROPERTY_MODELS = (
AmesimGasPropertyModelSpec(
value=AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL,
label="理想气体",
method_id=AmesimIdealAirMedium.PROPERTY_METHOD_ID,
factory=AmesimIdealAirMedium,
eos_type=1,
),
)
AMESIM_AIR_PROPERTY_MODELS = (AmesimGasPropertyModelSpec(value=AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL, label='理想气体', method_id=AmesimIdealAirMedium.PROPERTY_METHOD_ID, factory=AmesimIdealAirMedium, eos_type=1),)
AMESIM_HELIUM_PENG_ROBINSON_PROPERTY_MODEL = 0
AMESIM_HELIUM_PROPERTY_MODELS = (
AmesimGasPropertyModelSpec(
value=AMESIM_HELIUM_PENG_ROBINSON_PROPERTY_MODEL,
label="Peng–Robinson",
method_id=AmesimHeliumPengRobinsonMedium.PROPERTY_METHOD_ID,
factory=AmesimHeliumPengRobinsonMedium,
eos_type=6,
),
)
AMESIM_HELIUM_PROPERTY_MODELS = (AmesimGasPropertyModelSpec(value=AMESIM_HELIUM_PENG_ROBINSON_PROPERTY_MODEL, label='Peng–Robinson', method_id=AmesimHeliumPengRobinsonMedium.PROPERTY_METHOD_ID, factory=AmesimHeliumPengRobinsonMedium, eos_type=6),)
@@ -1,355 +1,79 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping
from math import floor
from app.simulation.core.base import AlgebraicComponent
from app.simulation.core.catalog import (
ComponentDisplaySpec,
ParameterGroupDisplaySpec,
PortDisplaySpec,
)
from app.simulation.core.metadata import (
ParameterCondition,
ParameterDefinition,
ParameterOption,
ResultVariableDefinition,
)
from app.simulation.core.catalog import ComponentDisplaySpec, ParameterGroupDisplaySpec, PortDisplaySpec
from app.simulation.core.metadata import ParameterCondition, ParameterDefinition, ParameterOption, ResultVariableDefinition
from app.simulation.core.medium import IdealGasMedium
from app.simulation.core.ports import PortDefinition
def _ud00_stage_parameters(index: int) -> tuple[ParameterDefinition, ...]:
visible_when = (
()
if index == 1
else (
ParameterCondition(
"nstages",
tuple(float(stage_count) for stage_count in range(index, 9)),
),
)
)
return (
ParameterDefinition(
f"start{index}",
0.0 if index == 1 else 1.0,
label=f"第 {index} 段起点",
quantity="dimensionless",
unit="",
description=f"第 {index} 段开始时的输出值。",
visible_when=visible_when,
),
ParameterDefinition(
f"end{index}",
1.0,
label=f"第 {index} 段终点",
quantity="dimensionless",
unit="",
description=f"第 {index} 段结束时的输出值。",
visible_when=visible_when,
),
ParameterDefinition(
f"t{index}",
1.0 if index == 1 else 0.0,
label=f"第 {index} 段时长",
quantity="time",
unit="s",
minimum=0.0,
description=f"第 {index} 段的持续时间。",
visible_when=visible_when,
),
)
_UD00_STAGE_PARAMETERS = tuple(
parameter
for stage_index in range(1, 9)
for parameter in _ud00_stage_parameters(stage_index)
)
visible_when = () if index == 1 else (ParameterCondition('nstages', tuple((float(stage_count) for stage_count in range(index, 9)))),)
return (ParameterDefinition(f'start{index}', 0.0 if index == 1 else 1.0, label=f'第 {index} 段起点', quantity='dimensionless', unit='', description=f'第 {index} 段开始时的输出值。', visible_when=visible_when), ParameterDefinition(f'end{index}', 1.0, label=f'第 {index} 段终点', quantity='dimensionless', unit='', description=f'第 {index} 段结束时的输出值。', visible_when=visible_when), ParameterDefinition(f't{index}', 1.0 if index == 1 else 0.0, label=f'第 {index} 段时长', quantity='time', unit='s', minimum=0.0, description=f'第 {index} 段的持续时间。', visible_when=visible_when))
_UD00_STAGE_PARAMETERS = tuple((parameter for stage_index in range(1, 9) for parameter in _ud00_stage_parameters(stage_index)))
class AmesimStep0(AlgebraicComponent):
"""AMESim STEP0 scalar step signal source."""
MODEL_TYPE = 'amesim_step0'
MODEL_VERSION = '0.1.0'
PORTS = (PortDefinition.signal('out', nominal_role='output'),)
PARAMETERS = (ParameterDefinition('initial', 0.0, label='初始值', quantity='dimensionless', unit=''), ParameterDefinition('final', 1.0, label='阶跃后值', quantity='dimensionless', unit=''), ParameterDefinition('time', 0.0, label='阶跃时间', quantity='time', unit='s'))
RESULT_VARIABLES = (ResultVariableDefinition('y', '输出', 'dimensionless', '', 'signal', 10),)
DISPLAY = ComponentDisplaySpec(label='STEP0 阶跃信号', library_id='amesim', category_id='signals', symbol='amesim_step0', ports=(PortDisplaySpec('out', 'right', order=10),), order=10)
MODEL_TYPE = "amesim_step0"
MODEL_VERSION = "0.1.0"
PORTS = (PortDefinition.signal("out", nominal_role="output"),)
PARAMETERS = (
ParameterDefinition("initial", 0.0, label="初始值", quantity="dimensionless", unit=""),
ParameterDefinition("final", 1.0, label="阶跃后值", quantity="dimensionless", unit=""),
ParameterDefinition("time", 0.0, label="阶跃时间", quantity="time", unit="s"),
)
RESULT_VARIABLES = (
ResultVariableDefinition("y", "输出", "dimensionless", "", "signal", 10),
)
DISPLAY = ComponentDisplaySpec(
label="STEP0 阶跃信号",
library_id="amesim",
category_id="signals",
symbol="amesim_step0",
ports=(PortDisplaySpec("out", "right", order=10),),
order=10,
)
def __init__(
self,
name: str,
medium: IdealGasMedium,
*,
initial: float = 0.0,
final: float = 1.0,
time: float = 0.0,
) -> None:
def __init__(self, name: str, medium: IdealGasMedium, *, initial: float=0.0, final: float=1.0, time: float=0.0) -> None:
super().__init__(name=name)
self.set_parameter_values({"initial": initial, "final": final, "time": time})
self.set_parameter_values({'initial': initial, 'final': final, 'time': time})
self.initial = float(initial)
self.final = float(final)
self.time = float(time)
self.out = self.register_declared_port("out")
self.out.signal = self.output_at(0.0)
self.out = self.register_declared_port('out')
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> "AmesimStep0":
return cls(
name=name,
medium=medium,
initial=parameters["initial"],
final=parameters["final"],
time=parameters["time"],
)
def output_at(self, time: float) -> float:
return self.final if time >= self.time else self.initial
def signal_output_values(self, time: float) -> dict[str, float]:
return {"out": self.output_at(time)}
def signal_event_times(
self,
start_time: float,
stop_time: float,
) -> tuple[float, ...]:
"""Expose the exact STEP0 switch time as an integration split point."""
return (self.time,) if start_time < self.time < stop_time else ()
def component_result_values(self) -> Mapping[str, float]:
return {"y": self.out.signal}
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> 'AmesimStep0':
return cls(name=name, medium=medium, initial=parameters['initial'], final=parameters['final'], time=parameters['time'])
EQUATIONS = ()
class AmesimUd00(AlgebraicComponent):
"""AMESim UD00 piecewise-linear scalar signal source."""
MODEL_TYPE = 'amesim_ud00'
MODEL_VERSION = '0.2.0'
PORTS = (PortDefinition.signal('out', nominal_role='output'),)
PARAMETERS = (ParameterDefinition('tstart', 0.0, label='启动时间', quantity='time', unit='s', description='分段信号开始输出第一段之前的等待时间。'), *_UD00_STAGE_PARAMETERS, ParameterDefinition('nstages', 1.0, label='段数', quantity='dimensionless', unit='', minimum=1.0, maximum=8.0, editor='choice', options=tuple((ParameterOption(float(stage_count), str(stage_count)) for stage_count in range(1, 9))), description='参与输出计算的有效线性分段数量。'), ParameterDefinition('iscyclic', 0.0, label='循环', quantity='dimensionless', unit='', minimum=0.0, maximum=1.0, editor='choice', options=(ParameterOption(0.0, '否'), ParameterOption(1.0, '是')), description='当前公共协议编码:0 表示单次输出,1 表示循环输出。'))
RESULT_VARIABLES = (ResultVariableDefinition('y', '输出', 'dimensionless', '', 'signal', 10),)
DISPLAY = ComponentDisplaySpec(label='UD00 分段线性信号', library_id='amesim', category_id='signals', symbol='amesim_ud00', ports=(PortDisplaySpec('out', 'right', order=10),), order=20, parameter_groups=(ParameterGroupDisplaySpec(id='stages', label='分段参数', parameters=tuple((parameter.name for parameter in _UD00_STAGE_PARAMETERS)), order=10),))
MODEL_TYPE = "amesim_ud00"
MODEL_VERSION = "0.2.0"
PORTS = (PortDefinition.signal("out", nominal_role="output"),)
PARAMETERS = (
ParameterDefinition(
"tstart",
0.0,
label="启动时间",
quantity="time",
unit="s",
description="分段信号开始输出第一段之前的等待时间。",
),
*_UD00_STAGE_PARAMETERS,
ParameterDefinition(
"nstages",
1.0,
label="段数",
quantity="dimensionless",
unit="",
minimum=1.0,
maximum=8.0,
editor="choice",
options=tuple(
ParameterOption(float(stage_count), str(stage_count))
for stage_count in range(1, 9)
),
description="参与输出计算的有效线性分段数量。",
),
ParameterDefinition(
"iscyclic",
0.0,
label="循环",
quantity="dimensionless",
unit="",
minimum=0.0,
maximum=1.0,
editor="choice",
options=(
ParameterOption(0.0, "否"),
ParameterOption(1.0, "是"),
),
description="当前公共协议编码:0 表示单次输出,1 表示循环输出。",
),
)
RESULT_VARIABLES = (
ResultVariableDefinition("y", "输出", "dimensionless", "", "signal", 10),
)
DISPLAY = ComponentDisplaySpec(
label="UD00 分段线性信号",
library_id="amesim",
category_id="signals",
symbol="amesim_ud00",
ports=(PortDisplaySpec("out", "right", order=10),),
order=20,
parameter_groups=(
ParameterGroupDisplaySpec(
id="stages",
label="分段参数",
parameters=tuple(
parameter.name for parameter in _UD00_STAGE_PARAMETERS
),
order=10,
),
),
)
def __init__(
self,
name: str,
medium: IdealGasMedium,
*,
tstart: float = 0.0,
starts: tuple[float, ...] = (0.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0),
ends: tuple[float, ...] = (1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0),
durations: tuple[float, ...] = (1.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0),
nstages: int = 1,
iscyclic: bool = False,
) -> None:
def __init__(self, name: str, medium: IdealGasMedium, *, tstart: float=0.0, starts: tuple[float, ...]=(0.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0), ends: tuple[float, ...]=(1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0), durations: tuple[float, ...]=(1.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0), nstages: int=1, iscyclic: bool=False) -> None:
super().__init__(name=name)
if len(starts) != 8 or len(ends) != 8 or len(durations) != 8:
raise ValueError("UD00 requires exactly eight start, end, and duration values.")
raise ValueError('UD00 requires exactly eight start, end, and duration values.')
if nstages < 1 or nstages > 8:
raise ValueError("UD00 nstages must be between 1 and 8.")
raise ValueError('UD00 nstages must be between 1 and 8.')
self.tstart = float(tstart)
self.starts = tuple(float(value) for value in starts)
self.ends = tuple(float(value) for value in ends)
self.durations = tuple(float(value) for value in durations)
self.starts = tuple((float(value) for value in starts))
self.ends = tuple((float(value) for value in ends))
self.durations = tuple((float(value) for value in durations))
self.nstages = int(nstages)
self.iscyclic = bool(iscyclic)
values: dict[str, float] = {"tstart": self.tstart, "nstages": float(self.nstages), "iscyclic": float(int(self.iscyclic))}
values: dict[str, float] = {'tstart': self.tstart, 'nstages': float(self.nstages), 'iscyclic': float(int(self.iscyclic))}
for index in range(1, 9):
values[f"start{index}"] = self.starts[index - 1]
values[f"end{index}"] = self.ends[index - 1]
values[f"t{index}"] = self.durations[index - 1]
values[f'start{index}'] = self.starts[index - 1]
values[f'end{index}'] = self.ends[index - 1]
values[f't{index}'] = self.durations[index - 1]
self.set_parameter_values(values)
self.out = self.register_declared_port("out")
self.out.signal = self.output_at(0.0)
self.out = self.register_declared_port('out')
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> "AmesimUd00":
nstages = parameters["nstages"]
iscyclic = parameters["iscyclic"]
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> 'AmesimUd00':
nstages = parameters['nstages']
iscyclic = parameters['iscyclic']
definitions = {definition.name: definition for definition in cls.PARAMETERS}
for parameter_name, value in (
("nstages", nstages),
("iscyclic", iscyclic),
):
for parameter_name, value in (('nstages', nstages), ('iscyclic', iscyclic)):
numeric_value = float(value)
if not numeric_value.is_integer():
raise ValueError(f"UD00 {parameter_name} must be an integer.")
raise ValueError(f'UD00 {parameter_name} must be an integer.')
message = definitions[parameter_name].validation_message(numeric_value)
if message is not None:
raise ValueError(f"UD00 {parameter_name} {message}.")
return cls(
name=name,
medium=medium,
tstart=parameters["tstart"],
starts=tuple(parameters[f"start{index}"] for index in range(1, 9)),
ends=tuple(parameters[f"end{index}"] for index in range(1, 9)),
durations=tuple(parameters[f"t{index}"] for index in range(1, 9)),
nstages=int(nstages),
iscyclic=bool(int(iscyclic)),
)
def output_at(self, time: float) -> float:
elapsed = max(float(time) - self.tstart, 0.0)
active_durations = self.durations[: self.nstages]
total_duration = sum(active_durations)
if self.iscyclic and total_duration > 0.0:
elapsed = elapsed % total_duration
stage_start_time = 0.0
for index, duration in enumerate(active_durations):
stage_end_time = stage_start_time + duration
if elapsed < stage_end_time or index == self.nstages - 1:
if duration <= 0.0:
return self.ends[index]
fraction = (elapsed - stage_start_time) / duration
return self.starts[index] + fraction * (self.ends[index] - self.starts[index])
stage_start_time = stage_end_time
return self.ends[self.nstages - 1]
def signal_output_values(self, time: float) -> dict[str, float]:
return {"out": self.output_at(time)}
def signal_event_times(
self,
start_time: float,
stop_time: float,
) -> tuple[float, ...]:
"""Return UD00 start, stage, and repeated cycle boundaries.
The final non-cyclic stage is intentionally not given an end event:
``output_at`` continues that stage's slope after its configured duration.
"""
if stop_time <= start_time:
return ()
active_durations = self.durations[: self.nstages]
stage_offsets = [0.0]
elapsed = 0.0
for duration in active_durations[:-1]:
elapsed += duration
stage_offsets.append(elapsed)
if not self.iscyclic:
return tuple(
sorted(
{
event_time
for offset in stage_offsets
if start_time
< (event_time := self.tstart + offset)
< stop_time
}
)
)
cycle_duration = sum(active_durations)
if cycle_duration <= 0.0:
return ()
events: set[float] = set()
for offset in stage_offsets:
first_boundary = self.tstart + offset
cycle_index = max(
0,
floor((start_time - first_boundary) / cycle_duration) + 1,
)
event_time = first_boundary + cycle_index * cycle_duration
while event_time < stop_time:
if event_time > start_time:
events.add(event_time)
cycle_index += 1
event_time = first_boundary + cycle_index * cycle_duration
return tuple(sorted(events))
def component_result_values(self) -> Mapping[str, float]:
return {"y": self.out.signal}
raise ValueError(f'UD00 {parameter_name} {message}.')
return cls(name=name, medium=medium, tstart=parameters['tstart'], starts=tuple((parameters[f'start{index}'] for index in range(1, 9))), ends=tuple((parameters[f'end{index}'] for index in range(1, 9))), durations=tuple((parameters[f't{index}'] for index in range(1, 9))), nstages=int(nstages), iscyclic=bool(int(iscyclic)))
EQUATIONS = ()
@@ -1,38 +1,12 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping, Sequence
from dataclasses import dataclass
from math import isfinite
from app.simulation.components.amesim.gases import (
AMESIM_GAS_INDEX_PARAMETER,
normalize_amesim_gas_index,
)
from collections.abc import Mapping
from app.simulation.components.amesim.gases import AMESIM_GAS_INDEX_PARAMETER, normalize_amesim_gas_index
from app.simulation.core.base import ThermodynamicVolumeComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import (
ParameterDefinition,
ResultVariableDefinition,
THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
)
from app.simulation.core.medium import (
GasMedium,
ThermodynamicProperties,
ThermodynamicPropertiesLinearization,
)
from app.simulation.core.metadata import ParameterDefinition, ResultVariableDefinition, THERMODYNAMIC_VOLUME_RESULT_VARIABLES
from app.simulation.core.medium import GasMedium
from app.simulation.core.ports import PortDefinition
from app.simulation.core.state import VolumeState
@dataclass(frozen=True)
class Pnch012DerivativeLinearization:
derivative: tuple[float, float]
tangents: tuple[tuple[float, ...], tuple[float, ...]]
properties: ThermodynamicPropertiesLinearization
valid: bool = True
reason: str | None = None
class AmesimPnch023(ThermodynamicVolumeComponent):
"""AMESim PNCH023 simple pneumatic chamber with heat exchange.
@@ -42,112 +16,16 @@ class AmesimPnch023(ThermodynamicVolumeComponent):
framework's mass/internal-energy volume state and keeps the AMESim
heat-transfer contract `kth * sth * (extemp - T)`.
"""
MODEL_TYPE = "amesim_pnch023"
MODEL_VERSION = "0.1.0"
PORTS = (
PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
)
PARAMETERS = (
AMESIM_GAS_INDEX_PARAMETER,
ParameterDefinition(
"cvol",
0.057,
label="气室容积",
quantity="volume",
unit="m3",
minimum=0.0,
minimum_exclusive=True,
description="气室内部用于储存气体的固定有效容积。",
),
ParameterDefinition(
"kth",
0.0,
label="换热系数",
quantity="heat_transfer_coefficient",
unit="W/(m2*K)",
minimum=0.0,
description="气室与环境之间的对流换热系数,与换热面积共同决定换热功率。",
),
ParameterDefinition(
"sth",
0.1,
label="换热面积",
quantity="area",
unit="m2",
minimum=0.0,
description="气室与环境进行热交换的有效表面积。",
),
ParameterDefinition(
"extemp",
293.15,
label="外部温度",
quantity="temperature",
unit="K",
minimum=0.0,
minimum_exclusive=True,
description="气室外部环境的绝对温度,用于计算气体与环境之间的换热。",
),
ParameterDefinition(
"p0",
100000.0,
label="初始压力",
quantity="pressure",
unit="Pa",
minimum=0.0,
minimum_exclusive=True,
description="仿真开始时气室内气体的绝对压力。",
),
ParameterDefinition(
"T0",
293.15,
label="初始温度",
quantity="temperature",
unit="K",
minimum=0.0,
minimum_exclusive=True,
description="仿真开始时气室内气体的绝对温度。",
),
)
MODEL_TYPE = 'amesim_pnch023'
MODEL_VERSION = '0.1.0'
PORTS = (PortDefinition.pneumatic('port_1', nominal_role='bidirectional'), PortDefinition.pneumatic('port_2', nominal_role='bidirectional'))
PARAMETERS = (AMESIM_GAS_INDEX_PARAMETER, ParameterDefinition('cvol', 0.057, label='气室容积', quantity='volume', unit='m3', minimum=0.0, minimum_exclusive=True, description='气室内部用于储存气体的固定有效容积。'), ParameterDefinition('kth', 0.0, label='换热系数', quantity='heat_transfer_coefficient', unit='W/(m2*K)', minimum=0.0, description='气室与环境之间的对流换热系数,与换热面积共同决定换热功率。'), ParameterDefinition('sth', 0.1, label='换热面积', quantity='area', unit='m2', minimum=0.0, description='气室与环境进行热交换的有效表面积。'), ParameterDefinition('extemp', 293.15, label='外部温度', quantity='temperature', unit='K', minimum=0.0, minimum_exclusive=True, description='气室外部环境的绝对温度,用于计算气体与环境之间的换热。'), ParameterDefinition('p0', 100000.0, label='初始压力', quantity='pressure', unit='Pa', minimum=0.0, minimum_exclusive=True, description='仿真开始时气室内气体的绝对压力。'), ParameterDefinition('T0', 293.15, label='初始温度', quantity='temperature', unit='K', minimum=0.0, minimum_exclusive=True, description='仿真开始时气室内气体的绝对温度。'))
RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
DISPLAY = ComponentDisplaySpec(
label="PNCH023 固定容积气室",
library_id="amesim",
category_id="storage",
symbol="amesim_pnch023",
ports=(
PortDisplaySpec("port_1", "left", order=10),
PortDisplaySpec("port_2", "right", order=20),
),
order=10,
)
DISPLAY = ComponentDisplaySpec(label='PNCH023 固定容积气室', library_id='amesim', category_id='storage', symbol='amesim_pnch023', ports=(PortDisplaySpec('port_1', 'left', order=10), PortDisplaySpec('port_2', 'right', order=20)), order=10)
def __init__(
self,
name: str,
medium: GasMedium,
*,
cvol: float = 0.057,
kth: float = 0.0,
sth: float = 0.1,
extemp: float = 293.15,
gi: float = 1.0,
p0: float = 100000.0,
T0: float = 293.15,
) -> None:
def __init__(self, name: str, medium: GasMedium, *, cvol: float=0.057, kth: float=0.0, sth: float=0.1, extemp: float=293.15, gi: float=1.0, p0: float=100000.0, T0: float=293.15) -> None:
super().__init__(name=name)
self.set_parameter_values(
{
"cvol": cvol,
"kth": kth,
"sth": sth,
"extemp": extemp,
"gi": gi,
"p0": p0,
"T0": T0,
}
)
self.set_parameter_values({'cvol': cvol, 'kth': kth, 'sth': sth, 'extemp': extemp, 'gi': gi, 'p0': p0, 'T0': T0})
self.medium = medium
self.cvol = float(cvol)
self.kth = float(kth)
@@ -156,120 +34,13 @@ class AmesimPnch023(ThermodynamicVolumeComponent):
self.gi = normalize_amesim_gas_index(gi)
self.p0 = float(p0)
self.T0 = float(T0)
m0 = medium.density(self.p0, self.T0) * self.cvol
U0 = m0 * medium.specific_internal_energy_at_pressure(self.p0, self.T0)
self.state = VolumeState(m=m0, U=U0)
initial_h = medium.specific_enthalpy_at_pressure(self.p0, self.T0)
self.port_1 = self.register_declared_port("port_1")
self.port_1.p = self.p0
self.port_1.h_outflow = initial_h
self.port_2 = self.register_declared_port("port_2")
self.port_2.p = self.p0
self.port_2.h_outflow = initial_h
self.port_1 = self.register_declared_port('port_1')
self.port_2 = self.register_declared_port('port_2')
@classmethod
def create(
cls,
*,
name: str,
medium: GasMedium,
parameters: Mapping[str, float],
) -> AmesimPnch023:
return cls(
name=name,
medium=medium,
cvol=parameters["cvol"],
kth=parameters["kth"],
sth=parameters["sth"],
extemp=parameters["extemp"],
gi=parameters["gi"],
p0=parameters["p0"],
T0=parameters["T0"],
)
def get_state_vector(self) -> list[float]:
return self.state.as_vector()
def set_state_vector(self, values: list[float]) -> None:
self.state = VolumeState.from_vector(values)
def properties(self) -> ThermodynamicProperties:
props = self.medium.properties_from_mU(self.state.m, self.state.U, self.cvol)
self.port_1.p = props.p
self.port_1.h_outflow = props.h
self.port_2.p = props.p
self.port_2.h_outflow = props.h
return props
def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
return self.properties()
def thermal_energy_flow_w(self, temperature: float) -> float:
return self.kth * self.sth * (self.extemp - temperature)
def state_derivative_from_ports(
self,
connected_h: Mapping[str, float],
) -> list[float]:
props = self.properties()
inlet_h_1 = self.connection_inlet_enthalpy(
port_m_flow=self.port_1.m_flow,
connected_h=connected_h["port_1"],
internal_h=props.h,
)
inlet_h_2 = self.connection_inlet_enthalpy(
port_m_flow=self.port_2.m_flow,
connected_h=connected_h["port_2"],
internal_h=props.h,
)
derivative = VolumeState(
m=self.port_1.m_flow + self.port_2.m_flow,
U=(
self.port_1.m_flow * inlet_h_1
+ self.port_2.m_flow * inlet_h_2
+ self.thermal_energy_flow_w(props.T)
),
)
return derivative.as_vector()
def pressure_flow_equation_values(self) -> tuple[float, ...]:
pressure = self.medium.properties_from_mU(
self.state.m,
self.state.U,
self.cvol,
).p
return (
self.port_1.p - pressure,
self.port_2.p - pressure,
)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
pressure = self.medium.properties_from_mU(
self.state.m,
self.state.U,
self.cvol,
).p
return (
EquationResidual(
id=f"{self.name}:port_1_pressure_state",
owner="component",
owner_id=self.name,
relation="state",
variables=(f"{self.name}.port_1.p", f"{self.name}.state"),
role="effort",
value=self.port_1.p - pressure,
),
EquationResidual(
id=f"{self.name}:port_2_pressure_state",
owner="component",
owner_id=self.name,
relation="state",
variables=(f"{self.name}.port_2.p", f"{self.name}.state"),
role="effort",
value=self.port_2.p - pressure,
),
)
def create(cls, *, name: str, medium: GasMedium, parameters: Mapping[str, float]) -> AmesimPnch023:
return cls(name=name, medium=medium, cvol=parameters['cvol'], kth=parameters['kth'], sth=parameters['sth'], extemp=parameters['extemp'], gi=parameters['gi'], p0=parameters['p0'], T0=parameters['T0'])
EQUATIONS = ({'id': '__MODEL__:port_1_pressure_state', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'state', 'variables': ['__MODEL__.port_1.p', '__MODEL__.state'], 'role': 'effort'}, {'id': '__MODEL__:port_2_pressure_state', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'state', 'variables': ['__MODEL__.port_2.p', '__MODEL__.state'], 'role': 'effort'})
class AmesimPnch012(ThermodynamicVolumeComponent):
"""AMESim PNCH012 variable-volume pneumatic chamber.
@@ -279,143 +50,16 @@ class AmesimPnch012(ThermodynamicVolumeComponent):
parameters, while connected moving-boundary components can now add live
volume and volume-rate values through the pneumatic connector contract.
"""
MODEL_TYPE = 'amesim_pnch012'
MODEL_VERSION = '0.1.0'
PORTS = (PortDefinition.pneumatic('port_1', nominal_role='bidirectional'), PortDefinition.pneumatic('port_2', nominal_role='bidirectional'), PortDefinition.pneumatic('port_3', nominal_role='bidirectional'), PortDefinition.pneumatic('port_4', nominal_role='bidirectional'))
PARAMETERS = (AMESIM_GAS_INDEX_PARAMETER, ParameterDefinition('cvol0', 0.015, label='死容积', quantity='volume', unit='m3', minimum=0.0, minimum_exclusive=True, description='变容气室在所有外部容积为零时仍保留的基础容积。'), ParameterDefinition('kth', 0.0, label='换热系数', quantity='heat_transfer_coefficient', unit='W/(m2*K)', minimum=0.0, description='气室与环境之间的对流换热系数,与换热面积共同决定换热功率。'), ParameterDefinition('sth', 0.1, label='换热面积', quantity='area', unit='m2', minimum=0.0, description='气室与环境进行热交换的有效表面积。'), ParameterDefinition('extemp', 293.15, label='外部温度', quantity='temperature', unit='K', minimum=0.0, minimum_exclusive=True, description='气室外部环境的绝对温度,用于计算气体与环境之间的换热。'), ParameterDefinition('p0', 100000.0, label='初始压力', quantity='pressure', unit='Pa', minimum=0.0, minimum_exclusive=True, description='仿真开始时气室内气体的绝对压力。'), ParameterDefinition('T0', 293.15, label='初始温度', quantity='temperature', unit='K', minimum=0.0, minimum_exclusive=True, description='仿真开始时气室内气体的绝对温度。'), ParameterDefinition('vol1', 0.0, label='端口 1 外部容积', quantity='volume', unit='m3'), ParameterDefinition('vol2', 0.0, label='端口 2 外部容积', quantity='volume', unit='m3'), ParameterDefinition('vol3', 0.0, label='端口 3 外部容积', quantity='volume', unit='m3'), ParameterDefinition('vol4', 0.0, label='端口 4 外部容积', quantity='volume', unit='m3'), ParameterDefinition('dvol1', 0.0, label='端口 1 容积变化率', quantity='volume_flow', unit='m3/s'), ParameterDefinition('dvol2', 0.0, label='端口 2 容积变化率', quantity='volume_flow', unit='m3/s'), ParameterDefinition('dvol3', 0.0, label='端口 3 容积变化率', quantity='volume_flow', unit='m3/s'), ParameterDefinition('dvol4', 0.0, label='端口 4 容积变化率', quantity='volume_flow', unit='m3/s'))
RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES + (ResultVariableDefinition('vol', '气室总容积', 'volume', 'm3', 'derived', 100), ResultVariableDefinition('dvol', '总容积变化率', 'volume_flow', 'm3/s', 'derived', 110))
DISPLAY = ComponentDisplaySpec(label='PNCH012 变容气室', library_id='amesim', category_id='storage', symbol='amesim_pnch012', ports=(PortDisplaySpec('port_1', 'left', order=10), PortDisplaySpec('port_2', 'right', order=20), PortDisplaySpec('port_3', 'left', order=30), PortDisplaySpec('port_4', 'right', order=40)), order=20)
MODEL_TYPE = "amesim_pnch012"
MODEL_VERSION = "0.1.0"
PORTS = (
PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_3", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_4", nominal_role="bidirectional"),
)
PARAMETERS = (
AMESIM_GAS_INDEX_PARAMETER,
ParameterDefinition(
"cvol0",
0.015,
label="死容积",
quantity="volume",
unit="m3",
minimum=0.0,
minimum_exclusive=True,
description="变容气室在所有外部容积为零时仍保留的基础容积。",
),
ParameterDefinition(
"kth",
0.0,
label="换热系数",
quantity="heat_transfer_coefficient",
unit="W/(m2*K)",
minimum=0.0,
description="气室与环境之间的对流换热系数,与换热面积共同决定换热功率。",
),
ParameterDefinition(
"sth",
0.1,
label="换热面积",
quantity="area",
unit="m2",
minimum=0.0,
description="气室与环境进行热交换的有效表面积。",
),
ParameterDefinition(
"extemp",
293.15,
label="外部温度",
quantity="temperature",
unit="K",
minimum=0.0,
minimum_exclusive=True,
description="气室外部环境的绝对温度,用于计算气体与环境之间的换热。",
),
ParameterDefinition(
"p0",
100000.0,
label="初始压力",
quantity="pressure",
unit="Pa",
minimum=0.0,
minimum_exclusive=True,
description="仿真开始时气室内气体的绝对压力。",
),
ParameterDefinition(
"T0",
293.15,
label="初始温度",
quantity="temperature",
unit="K",
minimum=0.0,
minimum_exclusive=True,
description="仿真开始时气室内气体的绝对温度。",
),
ParameterDefinition("vol1", 0.0, label="端口 1 外部容积", quantity="volume", unit="m3"),
ParameterDefinition("vol2", 0.0, label="端口 2 外部容积", quantity="volume", unit="m3"),
ParameterDefinition("vol3", 0.0, label="端口 3 外部容积", quantity="volume", unit="m3"),
ParameterDefinition("vol4", 0.0, label="端口 4 外部容积", quantity="volume", unit="m3"),
ParameterDefinition("dvol1", 0.0, label="端口 1 容积变化率", quantity="volume_flow", unit="m3/s"),
ParameterDefinition("dvol2", 0.0, label="端口 2 容积变化率", quantity="volume_flow", unit="m3/s"),
ParameterDefinition("dvol3", 0.0, label="端口 3 容积变化率", quantity="volume_flow", unit="m3/s"),
ParameterDefinition("dvol4", 0.0, label="端口 4 容积变化率", quantity="volume_flow", unit="m3/s"),
)
RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES + (
ResultVariableDefinition("vol", "气室总容积", "volume", "m3", "derived", 100),
ResultVariableDefinition("dvol", "总容积变化率", "volume_flow", "m3/s", "derived", 110),
)
DISPLAY = ComponentDisplaySpec(
label="PNCH012 变容气室",
library_id="amesim",
category_id="storage",
symbol="amesim_pnch012",
ports=(
PortDisplaySpec("port_1", "left", order=10),
PortDisplaySpec("port_2", "right", order=20),
PortDisplaySpec("port_3", "left", order=30),
PortDisplaySpec("port_4", "right", order=40),
),
order=20,
)
def __init__(
self,
name: str,
medium: GasMedium,
*,
cvol0: float = 0.015,
kth: float = 0.0,
sth: float = 0.1,
extemp: float = 293.15,
gi: float = 1.0,
p0: float = 100000.0,
T0: float = 293.15,
vol1: float = 0.0,
vol2: float = 0.0,
vol3: float = 0.0,
vol4: float = 0.0,
dvol1: float = 0.0,
dvol2: float = 0.0,
dvol3: float = 0.0,
dvol4: float = 0.0,
) -> None:
def __init__(self, name: str, medium: GasMedium, *, cvol0: float=0.015, kth: float=0.0, sth: float=0.1, extemp: float=293.15, gi: float=1.0, p0: float=100000.0, T0: float=293.15, vol1: float=0.0, vol2: float=0.0, vol3: float=0.0, vol4: float=0.0, dvol1: float=0.0, dvol2: float=0.0, dvol3: float=0.0, dvol4: float=0.0) -> None:
super().__init__(name=name)
self.set_parameter_values(
{
"cvol0": cvol0,
"kth": kth,
"sth": sth,
"extemp": extemp,
"gi": gi,
"p0": p0,
"T0": T0,
"vol1": vol1,
"vol2": vol2,
"vol3": vol3,
"vol4": vol4,
"dvol1": dvol1,
"dvol2": dvol2,
"dvol3": dvol3,
"dvol4": dvol4,
}
)
self.set_parameter_values({'cvol0': cvol0, 'kth': kth, 'sth': sth, 'extemp': extemp, 'gi': gi, 'p0': p0, 'T0': T0, 'vol1': vol1, 'vol2': vol2, 'vol3': vol3, 'vol4': vol4, 'dvol1': dvol1, 'dvol2': dvol2, 'dvol3': dvol3, 'dvol4': dvol4})
self.medium = medium
self.cvol0 = float(cvol0)
self.kth = float(kth)
@@ -424,267 +68,13 @@ class AmesimPnch012(ThermodynamicVolumeComponent):
self.gi = normalize_amesim_gas_index(gi)
self.p0 = float(p0)
self.T0 = float(T0)
self.external_volumes = {
"port_1": float(vol1),
"port_2": float(vol2),
"port_3": float(vol3),
"port_4": float(vol4),
}
self.external_volume_rates = {
"port_1": float(dvol1),
"port_2": float(dvol2),
"port_3": float(dvol3),
"port_4": float(dvol4),
}
if self.total_volume() <= 0.0:
raise ValueError("PNCH012 total volume must be positive.")
m0 = medium.density(self.p0, self.T0) * self.total_volume()
U0 = m0 * medium.specific_internal_energy_at_pressure(self.p0, self.T0)
self.state = VolumeState(m=m0, U=U0)
initial_h = medium.specific_enthalpy_at_pressure(self.p0, self.T0)
for port_name in ("port_1", "port_2", "port_3", "port_4"):
self.external_volumes = {'port_1': float(vol1), 'port_2': float(vol2), 'port_3': float(vol3), 'port_4': float(vol4)}
self.external_volume_rates = {'port_1': float(dvol1), 'port_2': float(dvol2), 'port_3': float(dvol3), 'port_4': float(dvol4)}
for port_name in ('port_1', 'port_2', 'port_3', 'port_4'):
port = self.register_declared_port(port_name)
port.p = self.p0
port.h_outflow = initial_h
setattr(self, port_name, port)
@classmethod
def create(
cls,
*,
name: str,
medium: GasMedium,
parameters: Mapping[str, float],
) -> "AmesimPnch012":
def create(cls, *, name: str, medium: GasMedium, parameters: Mapping[str, float]) -> 'AmesimPnch012':
return cls(name=name, medium=medium, **dict(parameters))
def connected_external_volume(self) -> float:
return sum(
getattr(getattr(self, port_name, None), "volume", 0.0)
for port_name in self.external_volumes
)
def connected_external_volume_rate(self) -> float:
return sum(
getattr(getattr(self, port_name, None), "volume_flow", 0.0)
for port_name in self.external_volume_rates
)
def total_volume(self) -> float:
minimum_volume = self.cvol0 / 100.0
return max(
self.cvol0 + sum(self.external_volumes.values()) + self.connected_external_volume(),
minimum_volume,
)
def total_volume_rate(self) -> float:
if self.total_volume() <= self.cvol0 / 100.0:
return 0.0
return sum(self.external_volume_rates.values()) + self.connected_external_volume_rate()
def get_state_vector(self) -> list[float]:
return self.state.as_vector()
def set_state_vector(self, values: list[float]) -> None:
self.state = VolumeState.from_vector(values)
def properties(self) -> ThermodynamicProperties:
props = self.medium.properties_from_mU(self.state.m, self.state.U, self.total_volume())
for port_name in ("port_1", "port_2", "port_3", "port_4"):
port = self.get_port(port_name)
port.p = props.p
port.h_outflow = props.h
return props
def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
return self.properties()
def thermal_energy_flow_w(self, temperature: float) -> float:
return self.kth * self.sth * (self.extemp - temperature)
def component_result_values(self) -> Mapping[str, float]:
props = self.properties()
return {
"m": self.state.m,
"U": self.state.U,
"p": props.p,
"T": props.T,
"rho": props.rho,
"u": props.u,
"h": props.h,
"vol": self.total_volume(),
"dvol": self.total_volume_rate(),
}
def state_derivative_from_ports(self, connected_h: Mapping[str, float]) -> list[float]:
props = self.properties()
mass_derivative = 0.0
energy_derivative = 0.0
for port_name in ("port_1", "port_2", "port_3", "port_4"):
port = self.get_port(port_name)
inlet_h = self.connection_inlet_enthalpy(
port_m_flow=port.m_flow,
connected_h=connected_h[port_name],
internal_h=props.h,
)
mass_derivative += port.m_flow
energy_derivative += port.m_flow * inlet_h
energy_derivative += self.thermal_energy_flow_w(props.T)
energy_derivative -= props.p * self.total_volume_rate()
return VolumeState(m=mass_derivative, U=energy_derivative).as_vector()
def linearize_state_derivative(
self,
connected_h: Mapping[str, float],
*,
state_mass_tangent: Sequence[float],
state_energy_tangent: Sequence[float],
external_volume_tangent: Sequence[float],
external_volume_rate_tangent: Sequence[float],
port_mass_flow_tangents: Mapping[str, Sequence[float]],
connected_h_tangents: Mapping[str, Sequence[float]],
property_linearization: ThermodynamicPropertiesLinearization | None = None,
flow_boundary_tolerance: float = 1.0e-12,
) -> Pnch012DerivativeLinearization:
"""Linearize the chamber balance while keeping stream modes fixed."""
port_names = ("port_1", "port_2", "port_3", "port_4")
vectors = {
"state_mass": tuple(float(value) for value in state_mass_tangent),
"state_energy": tuple(float(value) for value in state_energy_tangent),
"volume": tuple(float(value) for value in external_volume_tangent),
"volume_rate": tuple(
float(value) for value in external_volume_rate_tangent
),
}
for port_name in port_names:
vectors[f"flow:{port_name}"] = tuple(
float(value) for value in port_mass_flow_tangents[port_name]
)
vectors[f"enthalpy:{port_name}"] = tuple(
float(value) for value in connected_h_tangents[port_name]
)
widths = {len(values) for values in vectors.values()}
if len(widths) != 1:
raise ValueError("PNCH012 tangent vectors must have equal lengths.")
width = len(vectors["state_mass"])
invalid_reason: str | None = None
if not all(isfinite(value) for values in vectors.values() for value in values):
invalid_reason = "non_finite_tangent_input"
raw_volume = (
self.cvol0
+ sum(self.external_volumes.values())
+ self.connected_external_volume()
)
minimum_volume = self.cvol0 / 100.0
volume_scale = max(abs(raw_volume), abs(minimum_volume), 1.0e-18)
on_volume_boundary = (
abs(raw_volume - minimum_volume) <= 1.0e-12 * volume_scale
)
supplied_volume_tangent = vectors["volume"]
if raw_volume < minimum_volume or on_volume_boundary:
used_volume_tangent = (0.0,) * width
used_volume_rate_tangent = (0.0,) * width
if on_volume_boundary and any(
value != 0.0
for value in (
*supplied_volume_tangent,
*vectors["volume_rate"],
)
):
invalid_reason = invalid_reason or "volume_floor_boundary"
else:
used_volume_tangent = supplied_volume_tangent
used_volume_rate_tangent = vectors["volume_rate"]
properties = property_linearization or self.medium.linearize_properties_from_mU(
self.state.m,
self.state.U,
self.total_volume(),
vectors["state_mass"],
vectors["state_energy"],
used_volume_tangent,
)
if properties.tangents.width != width:
raise ValueError(
"PNCH012 property tangent width must match balance tangents."
)
props = properties.properties
if not properties.valid:
invalid_reason = invalid_reason or properties.reason
mass_derivative = sum(
self.get_port(port_name).m_flow for port_name in port_names
)
volume_rate = self.total_volume_rate()
energy_derivative = self.thermal_energy_flow_w(props.T) - props.p * volume_rate
mass_tangent = [0.0] * width
energy_tangent = [
-self.kth * self.sth * properties.tangents.T[index]
- volume_rate * properties.tangents.p[index]
- props.p * used_volume_rate_tangent[index]
for index in range(width)
]
for port_name in port_names:
port = self.get_port(port_name)
flow_tangent = vectors[f"flow:{port_name}"]
if (
abs(port.m_flow) <= flow_boundary_tolerance
and any(value != 0.0 for value in flow_tangent)
):
invalid_reason = invalid_reason or (
f"flow_direction_boundary:{port_name}"
)
if port.m_flow > 0.0:
inlet_h = connected_h[port_name]
inlet_h_tangent = vectors[f"enthalpy:{port_name}"]
else:
inlet_h = props.h
inlet_h_tangent = properties.tangents.h
energy_derivative += port.m_flow * inlet_h
for index in range(width):
mass_tangent[index] += flow_tangent[index]
energy_tangent[index] += (
inlet_h * flow_tangent[index]
+ port.m_flow * inlet_h_tangent[index]
)
return Pnch012DerivativeLinearization(
derivative=(mass_derivative, energy_derivative),
tangents=(tuple(mass_tangent), tuple(energy_tangent)),
properties=properties,
valid=invalid_reason is None,
reason=invalid_reason,
)
def pressure_flow_equation_values(self) -> tuple[float, ...]:
pressure = self.medium.properties_from_mU(
self.state.m,
self.state.U,
self.total_volume(),
).p
return tuple(
self.get_port(port_name).p - pressure
for port_name in ("port_1", "port_2", "port_3", "port_4")
)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
pressure = self.medium.properties_from_mU(
self.state.m,
self.state.U,
self.total_volume(),
).p
return tuple(
EquationResidual(
id=f"{self.name}:{port_name}_pressure_state",
owner="component",
owner_id=self.name,
relation="state",
variables=(f"{self.name}.{port_name}.p", f"{self.name}.state"),
role="effort",
value=self.get_port(port_name).p - pressure,
)
for port_name in ("port_1", "port_2", "port_3", "port_4")
)
EQUATIONS = ({'id': '__MODEL__:port_1_pressure_state', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'state', 'variables': ['__MODEL__.port_1.p', '__MODEL__.state'], 'role': 'effort'}, {'id': '__MODEL__:port_2_pressure_state', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'state', 'variables': ['__MODEL__.port_2.p', '__MODEL__.state'], 'role': 'effort'}, {'id': '__MODEL__:port_3_pressure_state', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'state', 'variables': ['__MODEL__.port_3.p', '__MODEL__.state'], 'role': 'effort'}, {'id': '__MODEL__:port_4_pressure_state', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'state', 'variables': ['__MODEL__.port_4.p', '__MODEL__.state'], 'role': 'effort'})
+10 -278
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@@ -1,282 +1,14 @@
# 元件建模规范与示例
# 元件开发示例
规范的权威版本位于
[`docs/standard/component-model-authoring-spec-v1.md`](../../../docs/standard/component-model-authoring-spec-v1.md)。
本文档保留在组件目录中,作为离模型源码最近的完整示例;若两者不一致,应在同一次
修改中同步,不能让示例形成另一套规则。
权威规则见 [组件模型建模规范](../../../docs/standard/component-model-authoring-spec-v1.md)。当前模型采用 Python 声明、C 数值实现。
本文档是 `app/simulation/components` 下新增元件的最小开发规范。当前
`experimental` 是用于验证规范的临时组件库;后续正式模型应建立独立组件库,
不要继续堆放在 `experimental` 中。
以气瓶为例:
目标是让元件的端口、输入参数和可展示结果都由元件类显式声明,避免 XML
校验、求解器和前端分别维护同一份含义。
1. 在 [cylinder.py](experimental/storage/cylinder.py) 声明 `MODEL_TYPE`、`MODEL_VERSION`、`PORTS`、`PARAMETERS`、`RESULT_VARIABLES`、`DISPLAY` 和 `create()`。
2. 构造函数调用 `set_parameter_values()`、`register_declared_port()`,保存介质选择和容积。不要在 Python 中计算密度、内能或状态导数。
3. 通过 `EQUATIONS` 声明端口压力与气瓶状态之间的约束;只保存变量名和关系。
4. 在 [extended.py](../native_codegen/extended.py) 分配状态及输出位置,生成 `native_medium_init()` 初始化调用和气瓶质量/能量导数计算。
5. 公共物性和数值公式由 [kernels.c](../../../native/components/kernels.c) 实现,积分和事件由 `native/runtime/` 处理。
6. 加入组件库 `library.py` 及 C 版本白名单,验证目录/XML 合同、边界输入、逆流、守恒、RK45/BDF 和输出键。
## 一、元件类必须声明的内容
每个对外注册的元件类至少需要声明以下六个类属性:
```python
MODEL_TYPE = "example_component"
MODEL_VERSION = "1.0.0"
PORTS = (...)
PARAMETERS = (...)
RESULT_VARIABLES = (...)
DISPLAY = ...
```
- `MODEL_TYPE`:稳定的模型类型标识,对应 System XML 中的 `Component/@type`。发布后不要随意改名。
- `MODEL_VERSION`:模型契约版本,采用 `主版本.次版本.修订版本`。
- `PORTS`:端口契约,包括端口名、物理域、变量和正流量方向。
- `PARAMETERS`:用户可配置的输入参数,包括默认值、物理量、SI 单位和取值范围。
- `RESULT_VARIABLES`:允许写入仿真结果并显示在结果页的组件级变量。端口结果由 `PORTS` 中的端口变量定义自动生成。
- `DISPLAY`:组件库名称、分类、图标、排序和端口画布位置,不参与物理求解。
元件构造函数还必须:
1. 调用 `super().__init__(name)`。
2. 使用 `set_parameter_values()` 保存规范化后的输入参数。
3. 使用 `register_declared_port()` 创建已声明端口。
4. 若声明了组件结果变量,实现 `component_result_values()` 并返回对应数值;标准热力学容腔可以直接继承 `ThermodynamicVolumeComponent` 的实现。
5. 实现统一的类方法 `create()`,接收规范化后的 SI 参数。
## 二、输入参数与结果变量
输入参数和仿真结果必须分开声明:
- 输入参数描述一次仿真开始前由用户配置的量,例如 `volume`、`p0`、`T0`。
- 结果变量描述随时间变化、允许绘图的量,例如 `p`、`T`、`m`、`m_flow`。
- 求解器缓存、中间残差和调试字段不得自动暴露为结果变量。
- 参数名和结果变量名使用稳定的英文机器标识;`label` 专门用于界面显示。
参数定义示例:
```python
ParameterDefinition(
name="volume",
label="容积",
quantity="volume",
unit="m3",
default=0.1,
minimum=0.0,
minimum_exclusive=True,
)
```
结果变量定义示例:
```python
ResultVariableDefinition(
name="p",
label="压力",
quantity="pressure",
unit="Pa",
category="thermodynamic",
order=30,
)
```
## 三、命名和单位约定
- 模型类型、参数、端口和变量名使用 `snake_case`,已有热力学惯例 `T`、`U` 可以保留。
- 输入参数保存和计算统一使用 SI 基准值;界面单位换算不能改变后端存储值。
- 无量纲参数的 `unit` 使用空字符串。
- `quantity` 表示稳定的物理量类型,例如 `pressure`、`temperature`、`mass_flow`,不能使用界面文案代替。
- 正质量流量统一定义为流入元件,即 `positiveFlowDirection="intoComponent"`。
- 端口变量 `p`、`m_flow`、`h_outflow` 的连接规则由 `PortDefinition.pneumatic()` 统一提供。
## 四、完整示例:单端口储气容腔
下面的示例展示一个可直接接入当前框架的动态元件。真实新增元件时应放入独立的 `.py` 文件,并补充对应测试。
```python
from __future__ import annotations
from collections.abc import Mapping
from app.simulation.core.base import ThermodynamicVolumeComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import (
ParameterDefinition,
THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
)
from app.simulation.core.medium import IdealGasMedium, ThermodynamicProperties
from app.simulation.core.ports import PortDefinition
from app.simulation.core.state import VolumeState
class ExampleVolume(ThermodynamicVolumeComponent):
MODEL_TYPE = "example_volume"
MODEL_VERSION = "1.0.0"
PORTS = (
PortDefinition.pneumatic("port_a", nominal_role="bidirectional"),
)
PARAMETERS = (
ParameterDefinition(
name="volume",
label="容积",
quantity="volume",
unit="m3",
default=0.1,
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
name="p0",
label="初始压力",
quantity="pressure",
unit="Pa",
default=100000.0,
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
name="T0",
label="初始温度",
quantity="temperature",
unit="K",
default=300.0,
minimum=0.0,
minimum_exclusive=True,
),
)
RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
DISPLAY = ComponentDisplaySpec(
label="示例容腔",
library_id="experimental",
category_id="storage",
symbol="generic",
ports=(PortDisplaySpec("port_a", "left"),),
order=90,
)
def __init__(
self,
name: str,
medium: IdealGasMedium,
volume: float = 0.1,
p0: float = 100000.0,
T0: float = 300.0,
) -> None:
super().__init__(name)
self.set_parameter_values(
{"volume": volume, "p0": p0, "T0": T0}
)
self.medium = medium
self.V = volume
initial_mass = p0 * volume / (medium.R_gas * T0)
initial_energy = initial_mass * medium.specific_internal_energy(T0)
self.state = VolumeState(m=initial_mass, U=initial_energy)
self.port_a = self.register_declared_port("port_a")
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> ExampleVolume:
return cls(
name=name,
medium=medium,
volume=parameters["volume"],
p0=parameters["p0"],
T0=parameters["T0"],
)
def get_state_vector(self) -> list[float]:
return self.state.as_vector()
def set_state_vector(self, values: list[float]) -> None:
self.state = VolumeState.from_vector(values)
def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
properties = self.medium.properties_from_mU(
self.state.m, self.state.U, self.V
)
self.port_a.p = properties.p
self.port_a.h_outflow = properties.h
return properties
def state_derivative_from_ports(
self,
connected_h: Mapping[str, float],
) -> list[float]:
properties = self.refresh_thermodynamic_ports()
inlet_h = self.connection_inlet_enthalpy(
port_m_flow=self.port_a.m_flow,
connected_h=connected_h["port_a"],
internal_h=properties.h,
)
return [self.port_a.m_flow, self.port_a.m_flow * inlet_h]
def pressure_flow_equation_residuals(
self,
) -> tuple[EquationResidual, ...]:
pressure = self.medium.properties_from_mU(
self.state.m, self.state.U, self.V
).p
return (
EquationResidual(
id=f"{self.name}:port_a_pressure_state",
owner="component",
owner_id=self.name,
relation="state",
variables=(f"{self.name}.port_a.p", f"{self.name}.state"),
role="effort",
value=self.port_a.p - pressure,
),
)
```
模型文件不再直接修改全局注册表。完成模型类后,只把类路径加入所属库
`library.py` 的 `models` 清单:
```python
models=(
# ...已有模型
"app.simulation.components.experimental.storage.example_volume:ExampleVolume",
)
```
后端会受控导入清单中的类,校验版本、分类、端口、参数、单位、显示信息和默认实例,
再自动建立注册表。校验通过后,`GET /api/components/catalog` 会输出该元件,
前端刷新时即可加载。
当前 `experimental` 仅用于规范验证;正式模型应先建立新的库声明,再把
`library_id` 指向正式库。
完成仿真后,每个已声明结果都会得到一条结构化元数据。前端应按字段筛选,不能再拆解 `key` 猜测含义:
```json
{
"key": "example_volume_1.port_a.m_flow",
"componentId": "example_volume_1",
"componentType": "example_volume",
"scope": "port",
"portName": "port_a",
"name": "m_flow",
"label": "质量流量",
"quantity": "mass_flow",
"unit": "kg/s",
"category": "flow",
"order": 20
}
```
## 五、新增元件检查清单
1. `MODEL_TYPE` 是否唯一,并与 XML 的模型类型一致。
2. 所有构造参数是否在 `PARAMETERS` 中声明并保存。
3. 所有端口是否在 `PORTS` 中声明并通过 `register_declared_port()` 创建。
4. `RESULT_VARIABLES` 与 `component_result_values()` 的键是否完全一致。
5. 结果变量是否包含明确的 `quantity`、`label`、`unit` 和显示顺序。
6. 是否只暴露有工程意义的结果,而非内部计算变量。
7. `MODEL_VERSION` 和 `DISPLAY` 是否完整,显示端口是否与物理端口完全一致。
8. 是否实现统一的 `create()`,并能用默认参数创建模型。
9. 模型类路径是否只加入所属库的 `library.py` 清单。
10. 是否补充参数边界、端口契约、目录输出、结果元数据和最小仿真的自动测试。
组件库、分类和自动发现的完整规则参见
[`组件库分类、发现与读取规范 v1`](../../../docs/standard/component-library-spec-v1.md)。
新增模型的参考值应来自独立解析结果、外部可信结果或已有冻结基准;不恢复第二套 Python 数值实现。
@@ -1,121 +1,34 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping
from math import sqrt
from app.simulation.core.base import AlgebraicComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import ParameterDefinition
from app.simulation.core.medium import IdealGasMedium
from app.simulation.core.ports import PortDefinition
class Orifice(AlgebraicComponent):
"""Python port of ModelicaModels.Myorifice."""
MODEL_TYPE = "orifice"
MODEL_VERSION = "1.0.0"
PRESSURE_FLOW_DEPENDS_ON_STREAM = False
PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
("mass_flow_balance",)
)
PORTS = (
PortDefinition.pneumatic("port_a", nominal_role="inlet"),
PortDefinition.pneumatic("port_b", nominal_role="outlet"),
)
PARAMETERS = (
ParameterDefinition(
"K",
1e-5,
label="流量系数",
quantity="flow_coefficient",
unit="kg/(s*Pa^0.5)",
minimum=0.0,
),
ParameterDefinition(
"opening",
1.0,
label="开度",
minimum=0.0,
maximum=1.0,
),
)
MODEL_TYPE = 'orifice'
MODEL_VERSION = '1.0.0'
PORTS = (PortDefinition.pneumatic('port_a', nominal_role='inlet'), PortDefinition.pneumatic('port_b', nominal_role='outlet'))
PARAMETERS = (ParameterDefinition('K', 1e-05, label='流量系数', quantity='flow_coefficient', unit='kg/(s*Pa^0.5)', minimum=0.0), ParameterDefinition('opening', 1.0, label='开度', minimum=0.0, maximum=1.0))
RESULT_VARIABLES = ()
DISPLAY = ComponentDisplaySpec(
label="孔板/阀门",
library_id="experimental",
category_id="flow",
symbol="orifice",
ports=(
PortDisplaySpec("port_a", "left", order=10),
PortDisplaySpec("port_b", "right", order=20),
),
order=40,
)
DISPLAY = ComponentDisplaySpec(label='孔板/阀门', library_id='experimental', category_id='flow', symbol='orifice', ports=(PortDisplaySpec('port_a', 'left', order=10), PortDisplaySpec('port_b', 'right', order=20)), order=40)
def __init__(self, name: str, opening: float = 1.0, K: float = 1e-5) -> None:
def __init__(self, name: str, opening: float=1.0, K: float=1e-05) -> None:
super().__init__(name=name)
self.set_parameter_values({"K": K, "opening": opening})
self.set_parameter_values({'K': K, 'opening': opening})
self.opening = opening
self.K = K
self.port_a = self.register_declared_port("port_a")
self.port_b = self.register_declared_port("port_b")
self.port_a = self.register_declared_port('port_a')
self.port_b = self.register_declared_port('port_b')
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> Orifice:
return cls(
name=name,
opening=parameters["opening"],
K=parameters["K"],
)
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> Orifice:
return cls(name=name, opening=parameters['opening'], K=parameters['K'])
@property
def K_eff(self) -> float:
return self.K * max(self.opening, 0.001)
def mass_flow(self, p_a: float, p_b: float) -> float:
dp = p_a - p_b
if dp == 0.0:
return 0.0
return self.K_eff * sqrt(abs(dp)) * (1.0 if dp > 0.0 else -1.0)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
return (
EquationResidual(
id=f"{self.name}:mass_flow_balance",
owner="component",
owner_id=self.name,
relation="sumToZero",
variables=(
f"{self.name}.port_a.m_flow",
f"{self.name}.port_b.m_flow",
),
role="flow",
value=self.port_a.m_flow + self.port_b.m_flow,
),
EquationResidual(
id=f"{self.name}:pressure_flow_relation",
owner="component",
owner_id=self.name,
relation="constitutive",
variables=(
f"{self.name}.port_a.p",
f"{self.name}.port_b.p",
f"{self.name}.port_a.m_flow",
),
role="flow",
value=self.port_a.m_flow
- self.mass_flow(self.port_a.p, self.port_b.p),
),
)
def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
self.port_a.h_outflow = connected_h["port_b"]
self.port_b.h_outflow = connected_h["port_a"]
EQUATIONS = ({'id': '__MODEL__:mass_flow_balance', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'sumToZero', 'variables': ['__MODEL__.port_a.m_flow', '__MODEL__.port_b.m_flow'], 'role': 'flow'}, {'id': '__MODEL__:pressure_flow_relation', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'constitutive', 'variables': ['__MODEL__.port_a.p', '__MODEL__.port_b.p', '__MODEL__.port_a.m_flow'], 'role': 'flow'})
@@ -1,10 +0,0 @@
"""Compatibility import for the TestModel-only dynamic pipe.
The public ``pipe`` catalog model is ``ResistivePipe``. New code should import
this legacy dynamic model from ``app.simulation.examples.testmodel.dynamic_pipe``.
"""
from app.simulation.examples.testmodel.dynamic_pipe import Pipe
__all__ = ("Pipe",)
@@ -1,106 +1,25 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping
from math import pi
from app.simulation.core.base import AlgebraicComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import ParameterDefinition
from app.simulation.core.medium import IdealGasMedium
from app.simulation.core.ports import PortDefinition
class ResistivePipe(AlgebraicComponent):
"""Quasi-steady Darcy resistance used by topology-driven simulation."""
MODEL_TYPE = "pipe"
MODEL_VERSION = "1.0.0"
PRESSURE_FLOW_DEPENDS_ON_STREAM = False
PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
("mass_flow_balance",)
)
PORTS = (
PortDefinition.pneumatic("port_a", nominal_role="inlet"),
PortDefinition.pneumatic("port_b", nominal_role="outlet"),
)
PARAMETERS = (
ParameterDefinition(
"length",
5.0,
label="长度",
quantity="length",
unit="m",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"diameter",
0.02,
label="直径",
quantity="length",
unit="m",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"lambda_darcy",
0.02,
label="摩阻系数",
minimum=0.0,
),
ParameterDefinition(
"p0",
1e5,
label="初始压力",
quantity="pressure",
unit="Pa",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"T0",
300.0,
label="初始温度",
quantity="temperature",
unit="K",
minimum=0.0,
minimum_exclusive=True,
),
)
MODEL_TYPE = 'pipe'
MODEL_VERSION = '1.0.0'
PORTS = (PortDefinition.pneumatic('port_a', nominal_role='inlet'), PortDefinition.pneumatic('port_b', nominal_role='outlet'))
PARAMETERS = (ParameterDefinition('length', 5.0, label='长度', quantity='length', unit='m', minimum=0.0, minimum_exclusive=True), ParameterDefinition('diameter', 0.02, label='直径', quantity='length', unit='m', minimum=0.0, minimum_exclusive=True), ParameterDefinition('lambda_darcy', 0.02, label='摩阻系数', minimum=0.0), ParameterDefinition('p0', 100000.0, label='初始压力', quantity='pressure', unit='Pa', minimum=0.0, minimum_exclusive=True), ParameterDefinition('T0', 300.0, label='初始温度', quantity='temperature', unit='K', minimum=0.0, minimum_exclusive=True))
RESULT_VARIABLES = ()
DISPLAY = ComponentDisplaySpec(
label="管段",
library_id="experimental",
category_id="flow",
symbol="pipe",
ports=(
PortDisplaySpec("port_a", "left", order=10),
PortDisplaySpec("port_b", "right", order=20),
),
order=30,
)
DISPLAY = ComponentDisplaySpec(label='管段', library_id='experimental', category_id='flow', symbol='pipe', ports=(PortDisplaySpec('port_a', 'left', order=10), PortDisplaySpec('port_b', 'right', order=20)), order=30)
def __init__(
self,
name: str,
medium: IdealGasMedium,
L: float = 5.0,
D: float = 0.02,
lambda_darcy: float = 0.02,
p0: float = 1e5,
T0: float = 300.0,
) -> None:
def __init__(self, name: str, medium: IdealGasMedium, L: float=5.0, D: float=0.02, lambda_darcy: float=0.02, p0: float=100000.0, T0: float=300.0) -> None:
super().__init__(name=name)
self.set_parameter_values(
{
"length": L,
"diameter": D,
"lambda_darcy": lambda_darcy,
"p0": p0,
"T0": T0,
}
)
self.set_parameter_values({'length': L, 'diameter': D, 'lambda_darcy': lambda_darcy, 'p0': p0, 'T0': T0})
self.medium = medium
self.L = L
self.D = D
@@ -108,82 +27,10 @@ class ResistivePipe(AlgebraicComponent):
self.p0 = p0
self.T0 = T0
self.area = pi * D * D / 4.0
initial_h = medium.specific_enthalpy(T0)
self.port_a = self.register_declared_port("port_a")
self.port_a.p = p0
self.port_a.h_outflow = initial_h
self.port_b = self.register_declared_port("port_b")
self.port_b.p = p0
self.port_b.h_outflow = initial_h
self.port_a = self.register_declared_port('port_a')
self.port_b = self.register_declared_port('port_b')
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> ResistivePipe:
return cls(
name=name,
medium=medium,
L=parameters["length"],
D=parameters["diameter"],
lambda_darcy=parameters["lambda_darcy"],
p0=parameters["p0"],
T0=parameters["T0"],
)
def pressure_drop(self, m_flow_a: float, p_a: float, p_b: float) -> float:
average_pressure = max(0.5 * (p_a + p_b), 1.0)
density = max(self.medium.density(average_pressure, self.T0), 1e-12)
resistance = self.lambda_darcy * (self.L / self.D)
return (
resistance
* m_flow_a
* abs(m_flow_a)
/ (2.0 * density * self.area * self.area)
)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
return (
EquationResidual(
id=f"{self.name}:mass_flow_balance",
owner="component",
owner_id=self.name,
relation="sumToZero",
variables=(
f"{self.name}.port_a.m_flow",
f"{self.name}.port_b.m_flow",
),
role="flow",
value=self.port_a.m_flow + self.port_b.m_flow,
),
EquationResidual(
id=f"{self.name}:darcy_pressure_loss",
owner="component",
owner_id=self.name,
relation="constitutive",
variables=(
f"{self.name}.port_a.p",
f"{self.name}.port_b.p",
f"{self.name}.port_a.m_flow",
),
role="effort",
value=(
self.port_a.p
- self.port_b.p
- self.pressure_drop(
self.port_a.m_flow,
self.port_a.p,
self.port_b.p,
)
),
),
)
def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
self.port_a.h_outflow = connected_h["port_b"]
self.port_b.h_outflow = connected_h["port_a"]
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> ResistivePipe:
return cls(name=name, medium=medium, L=parameters['length'], D=parameters['diameter'], lambda_darcy=parameters['lambda_darcy'], p0=parameters['p0'], T0=parameters['T0'])
EQUATIONS = ({'id': '__MODEL__:mass_flow_balance', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'sumToZero', 'variables': ['__MODEL__.port_a.m_flow', '__MODEL__.port_b.m_flow'], 'role': 'flow'}, {'id': '__MODEL__:darcy_pressure_loss', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'constitutive', 'variables': ['__MODEL__.port_a.p', '__MODEL__.port_b.p', '__MODEL__.port_a.m_flow'], 'role': 'effort'})
@@ -1,270 +1,28 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping
from app.simulation.core.base import AlgebraicComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.medium import IdealGasMedium
from app.simulation.core.ports import PortDefinition
class Tee(AlgebraicComponent):
"""Python port of ModelicaModels.Mytee."""
MODEL_TYPE = "tee"
MODEL_VERSION = "1.0.0"
PRESSURE_FLOW_DEPENDS_ON_STREAM = False
PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
("mass_flow_balance",)
)
PORTS = (
PortDefinition.pneumatic("port_in", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_out1", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_out2", nominal_role="bidirectional"),
)
MODEL_TYPE = 'tee'
MODEL_VERSION = '1.0.0'
PORTS = (PortDefinition.pneumatic('port_in', nominal_role='bidirectional'), PortDefinition.pneumatic('port_out1', nominal_role='bidirectional'), PortDefinition.pneumatic('port_out2', nominal_role='bidirectional'))
PARAMETERS = ()
RESULT_VARIABLES = ()
DISPLAY = ComponentDisplaySpec(
label="三通",
library_id="experimental",
category_id="junctions",
symbol="tee",
ports=(
PortDisplaySpec("port_in", "left", order=10),
PortDisplaySpec("port_out1", "right", order=20),
PortDisplaySpec("port_out2", "right", order=30),
),
order=50,
)
DISPLAY = ComponentDisplaySpec(label='三通', library_id='experimental', category_id='junctions', symbol='tee', ports=(PortDisplaySpec('port_in', 'left', order=10), PortDisplaySpec('port_out1', 'right', order=20), PortDisplaySpec('port_out2', 'right', order=30)), order=50)
def __init__(self, name: str) -> None:
super().__init__(name=name)
self.set_parameter_values({})
self.port_in = self.register_declared_port("port_in")
self.port_out1 = self.register_declared_port("port_out1")
self.port_out2 = self.register_declared_port("port_out2")
self.port_in = self.register_declared_port('port_in')
self.port_out1 = self.register_declared_port('port_out1')
self.port_out2 = self.register_declared_port('port_out2')
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> Tee:
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> Tee:
return cls(name=name)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
return (
EquationResidual(
id=f"{self.name}:common_pressure_out1",
owner="component",
owner_id=self.name,
relation="equal",
variables=(f"{self.name}.port_in.p", f"{self.name}.port_out1.p"),
role="effort",
value=self.port_in.p - self.port_out1.p,
),
EquationResidual(
id=f"{self.name}:common_pressure_out2",
owner="component",
owner_id=self.name,
relation="equal",
variables=(f"{self.name}.port_in.p", f"{self.name}.port_out2.p"),
role="effort",
value=self.port_in.p - self.port_out2.p,
),
EquationResidual(
id=f"{self.name}:mass_flow_balance",
owner="component",
owner_id=self.name,
relation="sumToZero",
variables=(
f"{self.name}.port_in.m_flow",
f"{self.name}.port_out1.m_flow",
f"{self.name}.port_out2.m_flow",
),
role="flow",
value=(
self.port_in.m_flow
+ self.port_out1.m_flow
+ self.port_out2.m_flow
),
),
)
def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
incoming = [
(port.m_flow, connected_h[name])
for name, port in self.ports.items()
if port.m_flow > 1e-12
]
total_flow = sum(m_flow for m_flow, _ in incoming)
if total_flow > 1e-12:
mixed_h = sum(
m_flow * enthalpy for m_flow, enthalpy in incoming
) / total_flow
else:
values = list(connected_h.values())
mixed_h = sum(values) / len(values) if values else 0.0
for port in self.ports.values():
port.h_outflow = mixed_h
def mixed_inlet_enthalpy(
self,
branch1_m_flow: float,
branch1_h: float,
branch2_m_flow: float,
branch2_h: float,
fallback_h: float = 0.0,
) -> float:
positive_1 = max(branch1_m_flow, 0.0)
positive_2 = max(branch2_m_flow, 0.0)
total = positive_1 + positive_2
if total <= 1e-9:
return fallback_h
return (positive_1 * branch1_h + positive_2 * branch2_h) / total
def inlet_stream_enthalpy(
self,
branch1_m_flow: float,
branch1_h: float,
branch2_m_flow: float,
branch2_h: float,
fallback_h: float,
) -> float:
"""Approximate `inStream(port_in.h_outflow)` for the current tee topology."""
return self.mixed_inlet_enthalpy(
branch1_m_flow,
branch1_h,
branch2_m_flow,
branch2_h,
fallback_h=fallback_h,
)
def branch_actual_stream_enthalpy(
self,
branch_m_flow: float,
branch_h: float,
inlet_h: float,
) -> float:
"""Approximate `actualStream(branch.h_outflow)` for a tee branch port."""
return inlet_h if branch_m_flow > 0.0 else branch_h
@staticmethod
def _solve_linear_2x2(
a11: float,
a12: float,
a21: float,
a22: float,
b1: float,
b2: float,
) -> tuple[float, float] | None:
determinant = a11 * a22 - a12 * a21
if abs(determinant) <= 1e-12:
return None
x1 = (b1 * a22 - b2 * a12) / determinant
x2 = (a11 * b2 - a21 * b1) / determinant
return x1, x2
def solve_branch_outlet_flows_from_energy_balance(
self,
*,
ratio_branch1: float,
ratio_branch2: float,
inlet_h_branch1: float,
inlet_h_branch2: float,
branch1_h: float,
branch2_h: float,
inlet_h: float,
q_in_branch1: float,
q_in_branch2: float,
tolerance: float = 1e-12,
) -> tuple[float, float]:
"""Solve branch outlet flows for the current three-port downstream tee use-case."""
rhs_branch1 = q_in_branch1 * inlet_h_branch1
rhs_branch2 = q_in_branch2 * inlet_h_branch2
def solve_both_forward() -> tuple[float, float] | None:
return self._solve_linear_2x2(
(1.0 + ratio_branch1) * branch1_h,
ratio_branch1 * branch2_h,
ratio_branch2 * branch1_h,
(1.0 + ratio_branch2) * branch2_h,
rhs_branch1,
rhs_branch2,
)
def solve_one_reverse(
*,
branch1_reverse: bool,
) -> tuple[float, float] | None:
if branch1_reverse:
return self._solve_linear_2x2(
inlet_h * (1.0 + ratio_branch1),
ratio_branch1 * inlet_h,
ratio_branch2 * inlet_h,
branch2_h + ratio_branch2 * inlet_h,
rhs_branch1,
rhs_branch2,
)
return self._solve_linear_2x2(
branch1_h + ratio_branch1 * inlet_h,
ratio_branch1 * inlet_h,
ratio_branch2 * inlet_h,
inlet_h * (1.0 + ratio_branch2),
rhs_branch1,
rhs_branch2,
)
def solve_both_reverse() -> tuple[float, float] | None:
return self._solve_linear_2x2(
inlet_h * (1.0 + ratio_branch1),
ratio_branch1 * inlet_h,
ratio_branch2 * inlet_h,
inlet_h * (1.0 + ratio_branch2),
rhs_branch1,
rhs_branch2,
)
candidate_solvers = (
(
solve_both_forward,
lambda q1, q2: q1 >= -tolerance and q2 >= -tolerance,
),
(
lambda: solve_one_reverse(branch1_reverse=True),
lambda q1, q2: q1 < -tolerance and q2 >= -tolerance and q1 + q2 > tolerance,
),
(
lambda: solve_one_reverse(branch1_reverse=True),
lambda q1, q2: q1 < -tolerance and q2 >= -tolerance and q1 + q2 <= tolerance,
),
(
lambda: solve_one_reverse(branch1_reverse=False),
lambda q1, q2: q2 < -tolerance and q1 >= -tolerance and q1 + q2 > tolerance,
),
(
lambda: solve_one_reverse(branch1_reverse=False),
lambda q1, q2: q2 < -tolerance and q1 >= -tolerance and q1 + q2 <= tolerance,
),
(
solve_both_reverse,
lambda q1, q2: q1 < -tolerance and q2 < -tolerance,
),
)
for solver, predicate in candidate_solvers:
candidate = solver()
if candidate is None:
continue
q_out_branch1, q_out_branch2 = candidate
if predicate(q_out_branch1, q_out_branch2):
return q_out_branch1, q_out_branch2
return solve_both_forward() or (0.0, 0.0)
EQUATIONS = ({'id': '__MODEL__:common_pressure_out1', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_in.p', '__MODEL__.port_out1.p'], 'role': 'effort'}, {'id': '__MODEL__:common_pressure_out2', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'equal', 'variables': ['__MODEL__.port_in.p', '__MODEL__.port_out2.p'], 'role': 'effort'}, {'id': '__MODEL__:mass_flow_balance', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'sumToZero', 'variables': ['__MODEL__.port_in.m_flow', '__MODEL__.port_out1.m_flow', '__MODEL__.port_out2.m_flow'], 'role': 'flow'})
@@ -1,155 +1,29 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping
from app.simulation.core.base import ThermodynamicVolumeComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import (
ParameterDefinition,
THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
)
from app.simulation.core.medium import IdealGasMedium, ThermodynamicProperties
from app.simulation.core.metadata import ParameterDefinition, THERMODYNAMIC_VOLUME_RESULT_VARIABLES
from app.simulation.core.medium import IdealGasMedium
from app.simulation.core.ports import PortDefinition
from app.simulation.core.state import VolumeState
class Cylinder(ThermodynamicVolumeComponent):
"""Python port of ModelicaModels.Mycylinder."""
MODEL_TYPE = "cylinder"
MODEL_VERSION = "1.0.0"
PORTS = (PortDefinition.pneumatic("port_b", nominal_role="outlet"),)
PARAMETERS = (
ParameterDefinition(
"volume",
0.01,
label="容积",
quantity="volume",
unit="m3",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"p0",
35e6,
label="初始压力",
quantity="pressure",
unit="Pa",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"T0",
300.0,
label="初始温度",
quantity="temperature",
unit="K",
minimum=0.0,
minimum_exclusive=True,
),
)
MODEL_TYPE = 'cylinder'
MODEL_VERSION = '1.0.0'
PORTS = (PortDefinition.pneumatic('port_b', nominal_role='outlet'),)
PARAMETERS = (ParameterDefinition('volume', 0.01, label='容积', quantity='volume', unit='m3', minimum=0.0, minimum_exclusive=True), ParameterDefinition('p0', 35000000.0, label='初始压力', quantity='pressure', unit='Pa', minimum=0.0, minimum_exclusive=True), ParameterDefinition('T0', 300.0, label='初始温度', quantity='temperature', unit='K', minimum=0.0, minimum_exclusive=True))
RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
DISPLAY = ComponentDisplaySpec(
label="气瓶",
library_id="experimental",
category_id="storage",
symbol="cylinder",
ports=(PortDisplaySpec("port_b", "right"),),
order=10,
)
DISPLAY = ComponentDisplaySpec(label='气瓶', library_id='experimental', category_id='storage', symbol='cylinder', ports=(PortDisplaySpec('port_b', 'right'),), order=10)
def __init__(
self,
name: str,
medium: IdealGasMedium,
V: float = 0.01,
p0: float = 35e6,
T0: float = 300.0,
) -> None:
def __init__(self, name: str, medium: IdealGasMedium, V: float=0.01, p0: float=35000000.0, T0: float=300.0) -> None:
super().__init__(name=name)
self.set_parameter_values({"volume": V, "p0": p0, "T0": T0})
self.set_parameter_values({'volume': V, 'p0': p0, 'T0': T0})
self.medium = medium
self.V = V
m0 = p0 * V / (medium.R_gas * T0)
U0 = m0 * medium.specific_internal_energy(T0)
self.state = VolumeState(m=m0, U=U0)
self.port_b = self.register_declared_port("port_b")
self.port_b = self.register_declared_port('port_b')
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> Cylinder:
return cls(
name=name,
medium=medium,
V=parameters["volume"],
p0=parameters["p0"],
T0=parameters["T0"],
)
def get_state_vector(self) -> list[float]:
return self.state.as_vector()
def set_state_vector(self, values: list[float]) -> None:
self.state = VolumeState.from_vector(values)
def properties(self) -> ThermodynamicProperties:
props = self.medium.properties_from_mU(self.state.m, self.state.U, self.V)
self.port_b.p = props.p
self.port_b.h_outflow = props.h
return props
def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
return self.properties()
def state_derivative_from_ports(
self,
connected_h: Mapping[str, float],
) -> list[float]:
properties = self.properties()
derivative = self.derivatives_from_connection(
connected_h=connected_h["port_b"],
port_m_flow=self.port_b.m_flow,
internal_h=properties.h,
)
return derivative.as_vector()
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
pressure = self.medium.properties_from_mU(
self.state.m,
self.state.U,
self.V,
).p
return (
EquationResidual(
id=f"{self.name}:port_b_pressure_state",
owner="component",
owner_id=self.name,
relation="state",
variables=(f"{self.name}.port_b.p", f"{self.name}.state"),
role="effort",
value=self.port_b.p - pressure,
),
)
def derivatives_from_connection(
self,
*,
connected_h: float,
port_m_flow: float,
internal_h: float,
) -> VolumeState:
inlet_h = self.connection_inlet_enthalpy(
port_m_flow=port_m_flow,
connected_h=connected_h,
internal_h=internal_h,
)
return self.derivatives(inlet_h, port_m_flow)
def derivatives(self, inlet_h: float, m_flow: float) -> VolumeState:
return VolumeState(m=m_flow, U=m_flow * inlet_h)
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> Cylinder:
return cls(name=name, medium=medium, V=parameters['volume'], p0=parameters['p0'], T0=parameters['T0'])
EQUATIONS = ({'id': '__MODEL__:port_b_pressure_state', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'state', 'variables': ['__MODEL__.port_b.p', '__MODEL__.state'], 'role': 'effort'},)
@@ -1,155 +1,29 @@
"""Component parameters, ports and output definitions; numerical equations execute in C."""
from __future__ import annotations
from collections.abc import Mapping
from app.simulation.core.base import ThermodynamicVolumeComponent
from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import (
ParameterDefinition,
THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
)
from app.simulation.core.medium import IdealGasMedium, ThermodynamicProperties
from app.simulation.core.metadata import ParameterDefinition, THERMODYNAMIC_VOLUME_RESULT_VARIABLES
from app.simulation.core.medium import IdealGasMedium
from app.simulation.core.ports import PortDefinition
from app.simulation.core.state import VolumeState
class Tank(ThermodynamicVolumeComponent):
"""Python port of ModelicaModels.Mytank."""
MODEL_TYPE = "tank"
MODEL_VERSION = "1.0.0"
PORTS = (PortDefinition.pneumatic("port_a", nominal_role="inlet"),)
PARAMETERS = (
ParameterDefinition(
"volume",
0.1,
label="容积",
quantity="volume",
unit="m3",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"p0",
1e5,
label="初始压力",
quantity="pressure",
unit="Pa",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"T0",
300.0,
label="初始温度",
quantity="temperature",
unit="K",
minimum=0.0,
minimum_exclusive=True,
),
)
MODEL_TYPE = 'tank'
MODEL_VERSION = '1.0.0'
PORTS = (PortDefinition.pneumatic('port_a', nominal_role='inlet'),)
PARAMETERS = (ParameterDefinition('volume', 0.1, label='容积', quantity='volume', unit='m3', minimum=0.0, minimum_exclusive=True), ParameterDefinition('p0', 100000.0, label='初始压力', quantity='pressure', unit='Pa', minimum=0.0, minimum_exclusive=True), ParameterDefinition('T0', 300.0, label='初始温度', quantity='temperature', unit='K', minimum=0.0, minimum_exclusive=True))
RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
DISPLAY = ComponentDisplaySpec(
label="贮箱",
library_id="experimental",
category_id="storage",
symbol="tank",
ports=(PortDisplaySpec("port_a", "left"),),
order=20,
)
DISPLAY = ComponentDisplaySpec(label='贮箱', library_id='experimental', category_id='storage', symbol='tank', ports=(PortDisplaySpec('port_a', 'left'),), order=20)
def __init__(
self,
name: str,
medium: IdealGasMedium,
V: float = 0.1,
p0: float = 1e5,
T0: float = 300.0,
) -> None:
def __init__(self, name: str, medium: IdealGasMedium, V: float=0.1, p0: float=100000.0, T0: float=300.0) -> None:
super().__init__(name=name)
self.set_parameter_values({"volume": V, "p0": p0, "T0": T0})
self.set_parameter_values({'volume': V, 'p0': p0, 'T0': T0})
self.medium = medium
self.V = V
m0 = p0 * V / (medium.R_gas * T0)
U0 = m0 * medium.specific_internal_energy(T0)
self.state = VolumeState(m=m0, U=U0)
self.port_a = self.register_declared_port("port_a")
self.port_a = self.register_declared_port('port_a')
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> Tank:
return cls(
name=name,
medium=medium,
V=parameters["volume"],
p0=parameters["p0"],
T0=parameters["T0"],
)
def get_state_vector(self) -> list[float]:
return self.state.as_vector()
def set_state_vector(self, values: list[float]) -> None:
self.state = VolumeState.from_vector(values)
def properties(self) -> ThermodynamicProperties:
props = self.medium.properties_from_mU(self.state.m, self.state.U, self.V)
self.port_a.p = props.p
self.port_a.h_outflow = props.h
return props
def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
return self.properties()
def state_derivative_from_ports(
self,
connected_h: Mapping[str, float],
) -> list[float]:
properties = self.properties()
derivative = self.derivatives_from_connection(
connected_h=connected_h["port_a"],
port_m_flow=self.port_a.m_flow,
internal_h=properties.h,
)
return derivative.as_vector()
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
pressure = self.medium.properties_from_mU(
self.state.m,
self.state.U,
self.V,
).p
return (
EquationResidual(
id=f"{self.name}:port_a_pressure_state",
owner="component",
owner_id=self.name,
relation="state",
variables=(f"{self.name}.port_a.p", f"{self.name}.state"),
role="effort",
value=self.port_a.p - pressure,
),
)
def derivatives_from_connection(
self,
*,
connected_h: float,
port_m_flow: float,
internal_h: float,
) -> VolumeState:
inlet_h = self.connection_inlet_enthalpy(
port_m_flow=port_m_flow,
connected_h=connected_h,
internal_h=internal_h,
)
return self.derivatives(inlet_h, port_m_flow)
def derivatives(self, inlet_h: float, m_flow: float) -> VolumeState:
return VolumeState(m=m_flow, U=m_flow * inlet_h)
def create(cls, *, name: str, medium: IdealGasMedium, parameters: Mapping[str, float]) -> Tank:
return cls(name=name, medium=medium, V=parameters['volume'], p0=parameters['p0'], T0=parameters['T0'])
EQUATIONS = ({'id': '__MODEL__:port_a_pressure_state', 'owner': 'component', 'ownerId': '__MODEL__', 'relation': 'state', 'variables': ['__MODEL__.port_a.p', '__MODEL__.state'], 'role': 'effort'},)
+148
View File
@@ -0,0 +1,148 @@
"""Simulation options and progress data; no numerical solver implementation."""
from __future__ import annotations
from dataclasses import dataclass
from typing import Sequence
@dataclass(frozen=True)
class SolverActivitySnapshot:
"""Low-cost, additive view of work inside an integration task.
``accepted_time`` deliberately changes only after an accepted solver step.
Trial evaluations may continue to advance ``activity_sequence`` and
``current_trial_time`` while that public progress value stays fixed.
"""
activity_sequence: int
activity_kind: str
current_trial_time: float | None
rhs_call_count: int
accepted_step_sequence: int
accepted_time: float | None
solver_step_sequence: int
jacobian_evaluation_count: int
thermofluid_closure_count: int
def as_dict(self) -> dict[str, object]:
return {
"activitySequence": self.activity_sequence,
"activityKind": self.activity_kind,
"currentTrialTime": self.current_trial_time,
"rhsCallCount": self.rhs_call_count,
"acceptedStepSequence": self.accepted_step_sequence,
"acceptedTime": self.accepted_time,
"solverStepSequence": self.solver_step_sequence,
"jacobianEvaluationCount": self.jacobian_evaluation_count,
"thermofluidClosureCount": self.thermofluid_closure_count,
}
class SolverActivityTracker:
"""Single-writer activity telemetry for a solver worker.
The solver thread is the only writer and the stream thread only snapshots
scalar attributes. The sequence is published last, so a reader never
treats partially published fields as a newer completed activity update.
The tracker receives aggregate counters from the independent C worker.
"""
__slots__ = (
"_accepted_step_sequence",
"_accepted_time",
"_activity_kind",
"_activity_sequence",
"_current_trial_time",
"_jacobian_evaluation_count",
"_rhs_call_count",
"_solver_step_sequence",
"_thermofluid_closure_count",
)
def __init__(self) -> None:
self._activity_sequence = 0
self._activity_kind = "idle"
self._current_trial_time: float | None = None
self._rhs_call_count = 0
self._accepted_step_sequence = 0
self._accepted_time: float | None = None
self._solver_step_sequence = 0
self._jacobian_evaluation_count = 0
self._thermofluid_closure_count = 0
def _publish(self, kind: str, time: float | None = None) -> None:
self._activity_kind = kind
if time is not None:
self._current_trial_time = float(time)
self._activity_sequence += 1
def start_integration(self, time: float) -> None:
self._accepted_time = float(time)
self._publish("solver_initialization", time)
def record_phase(self, kind: str, time: float | None = None) -> None:
self._publish(kind, time)
def record_solver_step(self, time: float) -> None:
self._solver_step_sequence += 1
self._publish("solver_step", time)
def record_rhs(self, time: float) -> None:
self._rhs_call_count += 1
self._publish("rhs", time)
def record_native_progress(self, time: float, rhs_count: int, accepted_count: int) -> None:
"""Publish aggregate counters from an isolated C worker without per-RHS callbacks."""
self._rhs_call_count = max(self._rhs_call_count, rhs_count)
self._accepted_step_sequence = max(self._accepted_step_sequence, accepted_count)
self._accepted_time = max(self._accepted_time or time, time)
self._publish("native_solver", time)
def record_jacobian(self, time: float) -> None:
self._jacobian_evaluation_count += 1
self._publish("jacobian", time)
def record_thermofluid_closure(self, time: float) -> None:
self._thermofluid_closure_count += 1
self._publish("thermofluid_closure", time)
def record_accepted_step(self, time: float) -> None:
accepted_time = float(time)
if (
self._accepted_time is not None
and accepted_time <= self._accepted_time
):
return
self._accepted_step_sequence += 1
self._accepted_time = accepted_time
self._publish("accepted_step", accepted_time)
def snapshot(self) -> SolverActivitySnapshot:
# ``activity_sequence`` is read last because writers publish it last.
activity_kind = self._activity_kind
current_trial_time = self._current_trial_time
rhs_call_count = self._rhs_call_count
accepted_step_sequence = self._accepted_step_sequence
accepted_time = self._accepted_time
solver_step_sequence = self._solver_step_sequence
jacobian_evaluation_count = self._jacobian_evaluation_count
thermofluid_closure_count = self._thermofluid_closure_count
activity_sequence = self._activity_sequence
return SolverActivitySnapshot(
activity_sequence=activity_sequence,
activity_kind=activity_kind,
current_trial_time=current_trial_time,
rhs_call_count=rhs_call_count,
accepted_step_sequence=accepted_step_sequence,
accepted_time=accepted_time,
solver_step_sequence=solver_step_sequence,
jacobian_evaluation_count=jacobian_evaluation_count,
thermofluid_closure_count=thermofluid_closure_count,
)
@dataclass(frozen=True)
class SolveIVPConfig:
t_start: float = 0.0
t_stop: float = 20.0
method: str = "BDF"
rtol: float = 1e-6
atol: float | Sequence[float] = 1e-8
max_step: float = 1e-3
first_step: float | None = None
+28 -267
View File
@@ -1,40 +1,17 @@
from __future__ import annotations
from abc import ABC, abstractmethod
from collections.abc import Callable, Mapping
from typing import TYPE_CHECKING, Any, ClassVar
from abc import ABC
from collections.abc import Mapping
from typing import TYPE_CHECKING, ClassVar
from app.simulation.core.catalog import ComponentDisplaySpec
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import (
ParameterDefinition,
ResultVariableDefinition,
ResultVariableMetadata,
THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
)
from app.simulation.core.equations import EquationDefinition
from app.simulation.core.metadata import ParameterDefinition, ResultVariableDefinition, ResultVariableMetadata, THERMODYNAMIC_VOLUME_RESULT_VARIABLES
from app.simulation.core.ports import PortDefinition, PortState
if TYPE_CHECKING:
from app.simulation.core.medium import GasMedium
class Component(ABC):
MODEL_TYPE: ClassVar[str | None] = None
MODEL_VERSION: ClassVar[str | None] = None
# ``True`` means that pressure/flow residuals read values written by
# ``update_stream_outflows`` or ``update_flow_temperature_references``.
# ``False`` is an explicit promise that those residuals are independent of
# stream propagation. ``None`` keeps custom components conservative: when
# they override either stream hook, the closure planner retains the legacy
# full-network thermofluid fixed point.
PRESSURE_FLOW_DEPENDS_ON_STREAM: ClassVar[bool | None] = None
# Exact residual suffixes whose declared variables are summed, in order,
# to form a ``sumToZero`` flow equation. The causal solver deliberately
# reads this capability from the concrete class ``__dict__``: subclasses
# must repeat the promise after changing any equation semantics.
PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES: ClassVar[
frozenset[str]
] = frozenset()
PORTS: ClassVar[tuple[PortDefinition, ...]] = ()
PARAMETERS: ClassVar[tuple[ParameterDefinition, ...]] = ()
RESULT_VARIABLES: ClassVar[tuple[ResultVariableDefinition, ...]] = ()
@@ -52,80 +29,53 @@ class Component(ABC):
@property
def port_definitions(self) -> tuple[PortDefinition, ...]:
return tuple(
port.definition
for port in self._ports.values()
if port.definition is not None
)
return tuple((port.definition for port in self._ports.values() if port.definition is not None))
@classmethod
def active_port_definitions_for_parameters(
cls,
parameters: Mapping[str, float],
) -> tuple[PortDefinition, ...]:
def active_port_definitions_for_parameters(cls, parameters: Mapping[str, float]) -> tuple[PortDefinition, ...]:
"""Declared ports enabled by one normalized parameter set."""
return cls.PORTS
@property
def active_port_definitions(self) -> tuple[PortDefinition, ...]:
"""Instance ports that participate in execution and result reporting."""
return self.port_definitions
@property
def required_connection_ports(self) -> tuple[str, ...]:
"""Physical ports that must have an external connection before simulation."""
return tuple(
definition.name
for definition in self.active_port_definitions
if definition.kind == "physical"
)
return tuple((definition.name for definition in self.active_port_definitions if definition.kind == 'physical'))
def register_port(self, port: PortState) -> PortState:
definition = port.definition
if definition is None:
raise ValueError(f"Component {self.name} cannot register an undefined port.")
raise ValueError(f'Component {self.name} cannot register an undefined port.')
if definition.name in self._ports:
raise ValueError(f"Duplicate port {self.name}.{definition.name}.")
raise ValueError(f'Duplicate port {self.name}.{definition.name}.')
self._ports[definition.name] = port
return port
def register_declared_port(self, name: str) -> PortState:
try:
definition = next(item for item in self.PORTS if item.name == name)
definition = next((item for item in self.PORTS if item.name == name))
except StopIteration as exc:
raise ValueError(
f"Component model {self.model_type} does not declare port {name}."
) from exc
raise ValueError(f'Component model {self.model_type} does not declare port {name}.') from exc
return self.register_port(PortState(definition=definition))
def set_parameter_values(self, values: Mapping[str, float]) -> None:
definitions = {definition.name: definition for definition in self.PARAMETERS}
unknown = sorted(set(values) - set(definitions))
if unknown:
raise ValueError(
f"Component {self.name} contains unsupported parameters: "
+ ", ".join(unknown)
+ "."
)
raise ValueError(f'Component {self.name} contains unsupported parameters: ' + ', '.join(unknown) + '.')
missing = sorted(set(definitions) - set(values))
if missing:
raise ValueError(
f"Component {self.name} is missing parameters: "
+ ", ".join(missing)
+ "."
)
raise ValueError(f'Component {self.name} is missing parameters: ' + ', '.join(missing) + '.')
resolved: dict[str, float] = {}
for name, definition in definitions.items():
value = float(values[name])
message = definition.validation_message(value)
if message is not None:
raise ValueError(
f"Parameter '{name}' on component '{self.name}' {message}."
)
raise ValueError(f"Parameter '{name}' on component '{self.name}' {message}.")
resolved[name] = value
self._parameter_values = resolved
@@ -137,229 +87,40 @@ class Component(ABC):
try:
return self._ports[name]
except KeyError as exc:
raise ValueError(f"Component {self.name} has no port named {name}.") from exc
def component_result_values(self) -> Mapping[str, float]:
return {}
def result_values(self) -> dict[str, float]:
component_values = dict(self.component_result_values())
declared = {definition.name: definition for definition in self.RESULT_VARIABLES}
unknown = sorted(set(component_values) - set(declared))
if unknown:
raise ValueError(
f"Component {self.name} returned undeclared result variables: "
+ ", ".join(unknown)
+ "."
)
values: dict[str, float] = {}
for name, definition in declared.items():
if not definition.visible:
continue
if name not in component_values:
raise ValueError(
f"Component {self.name} did not provide declared result variable {name}."
)
values[name] = float(component_values[name])
for port_definition in self.active_port_definitions:
port = self.get_port(port_definition.name)
for variable in port_definition.variables:
if not variable.result_visible:
continue
values[f"{port_definition.name}.{variable.name}"] = float(
getattr(port, variable.name)
)
return values
raise ValueError(f'Component {self.name} has no port named {name}.') from exc
def result_variable_metadata(self) -> tuple[ResultVariableMetadata, ...]:
metadata = [
ResultVariableMetadata(
key=f"{self.name}.{definition.name}",
component_id=self.name,
component_type=self.model_type,
scope="component",
name=definition.name,
label=definition.label,
quantity=definition.quantity,
unit=definition.unit,
category=definition.category,
order=definition.order,
)
for definition in self.RESULT_VARIABLES
if definition.visible
]
metadata = [ResultVariableMetadata(key=f'{self.name}.{definition.name}', component_id=self.name, component_type=self.model_type, scope='component', name=definition.name, label=definition.label, quantity=definition.quantity, unit=definition.unit, category=definition.category, order=definition.order) for definition in self.RESULT_VARIABLES if definition.visible]
for port_definition in self.active_port_definitions:
for variable in port_definition.variables:
if not variable.result_visible:
continue
metadata.append(
ResultVariableMetadata(
key=f"{self.name}.{port_definition.name}.{variable.name}",
component_id=self.name,
component_type=self.model_type,
scope="port",
port_name=port_definition.name,
name=variable.name,
label=variable.label or variable.name,
quantity=variable.quantity or variable.name,
unit=variable.unit,
category=variable.role,
order=variable.order,
)
)
metadata.append(ResultVariableMetadata(key=f'{self.name}.{port_definition.name}.{variable.name}', component_id=self.name, component_type=self.model_type, scope='port', port_name=port_definition.name, name=variable.name, label=variable.label or variable.name, quantity=variable.quantity or variable.name, unit=variable.unit, category=variable.role, order=variable.order))
return tuple(metadata)
def parameter_interface_dicts(self) -> list[dict[str, object]]:
return [
definition.as_interface_dict(
value=self._parameter_values.get(definition.name)
)
for definition in self.PARAMETERS
]
return [definition.as_interface_dict(value=self._parameter_values.get(definition.name)) for definition in self.PARAMETERS]
@classmethod
def create(
cls,
*,
name: str,
medium: GasMedium,
parameters: Mapping[str, float],
) -> Component:
def create(cls, *, name: str, medium: GasMedium, parameters: Mapping[str, float]) -> Component:
"""Create a catalog model from normalized SI parameters."""
raise NotImplementedError(f'Component model {cls.__name__} must implement create().')
EQUATIONS = ()
raise NotImplementedError(
f"Component model {cls.__name__} must implement create()."
)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
"""Return algebraic residuals after the network assigns port states."""
return ()
def pressure_flow_equation_values(self) -> tuple[float, ...]:
"""Return live residual values in the declared equation order.
Components with frequently evaluated equations can override this
method to avoid rebuilding immutable equation metadata during closure.
The default keeps third-party components compatible with the public
residual API.
"""
return tuple(
float(equation.value)
for equation in self.pressure_flow_equation_residuals()
)
def pressure_flow_equation_value_readers(
self,
) -> Mapping[str, Callable[[], float]]:
"""Return explicitly separable scalar residual readers.
The solver consumes this optional capability only when the concrete
component class declares the method itself. Subclasses therefore
cannot accidentally inherit an equation-purity promise.
"""
return {}
def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
"""Update connector outflow properties from current flow directions."""
return None
def update_flow_temperature_references(
self,
connected_h: Mapping[str, float],
) -> None:
"""Update enthalpy references used only by pressure-flow laws.
Most components use the normal stream enthalpy for both energy
transport and upstream-property evaluation. AMESim node submodels can
expose a distinct temperature reference, so the default is a no-op.
"""
return None
def pneumatic_volume_outputs(self) -> Mapping[str, tuple[float, float]]:
"""Return directed ``volume``/``volume_flow`` values by pneumatic port.
Most pneumatic components contribute no external chamber volume. Moving
boundaries such as PNRP17 override this hook; the network resolver then
propagates the pair to the component connected at the same physical port.
"""
return {}
def equation_definitions(self):
def bind(value):
if isinstance(value, str):
return value.replace('__MODEL__', self.name)
return tuple((bind(v) for v in value))
return tuple((EquationDefinition(id=bind(e['id']), owner=e['owner'], owner_id=self.name, relation=e['relation'], variables=bind(e['variables']), role=e['role']) for e in self.EQUATIONS))
class DynamicComponent(Component):
state_size = 2
@staticmethod
def actual_stream_enthalpy(
port_m_flow: float,
connected_h: float,
internal_h: float,
) -> float:
"""Approximate `actualStream(port.h_outflow)` for a mixed control volume port."""
return connected_h if port_m_flow > 0.0 else internal_h
def connection_inlet_enthalpy(
self,
port_m_flow: float,
connected_h: float,
internal_h: float,
) -> float:
"""Resolve the enthalpy convected into this control volume through one port."""
return self.actual_stream_enthalpy(
port_m_flow=port_m_flow,
connected_h=connected_h,
internal_h=internal_h,
)
@abstractmethod
def get_state_vector(self) -> list[float]:
raise NotImplementedError
@abstractmethod
def set_state_vector(self, values: list[float]) -> None:
raise NotImplementedError
def refresh_thermodynamic_ports(self) -> Any:
raise NotImplementedError
def state_derivative_from_ports(
self,
connected_h: Mapping[str, float],
) -> list[float]:
raise NotImplementedError
class ThermodynamicVolumeComponent(DynamicComponent):
"""Two-state gas volume exposing the shared thermodynamic result contract."""
RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
def component_result_values(self) -> Mapping[str, float]:
state = self.get_state_vector()
if len(state) < 2:
raise ValueError(
f"Thermodynamic component {self.name} must expose mass and energy states."
)
properties = self.refresh_thermodynamic_ports()
return {
"m": float(state[0]),
"U": float(state[1]),
"p": float(properties.p),
"T": float(properties.T),
"rho": float(properties.rho),
"u": float(properties.u),
"h": float(properties.h),
}
class AlgebraicComponent(Component):
"""Stateless element described by algebraic constraints only."""
+3 -4
View File
@@ -11,15 +11,14 @@ EquationRelation = Literal["equal", "sumToZero", "constitutive", "state"]
@dataclass(frozen=True, slots=True)
class EquationResidual:
"""One executable scalar equation in the pressure-flow subsystem."""
class EquationDefinition:
"""One declarative equation in the compiled model interface."""
id: str
owner: EquationOwner
owner_id: str
relation: EquationRelation
variables: tuple[str, ...]
value: float
role: VariableRole | None = None
def as_definition_dict(self) -> dict[str, object]:
@@ -33,4 +32,4 @@ class EquationResidual:
}
def as_interface_dict(self) -> dict[str, object]:
return {**self.as_definition_dict(), "residual": self.value}
return self.as_definition_dict()
+4 -366
View File
@@ -1,378 +1,16 @@
"""Compile-time gas property constants. No Python property evaluator."""
from __future__ import annotations
from dataclasses import dataclass
from math import isfinite
from typing import Protocol, Sequence
from app.simulation.core.errors import RecoverableTrialStateError
from app.simulation.performance import profile_property
@dataclass(frozen=True)
class ThermodynamicProperties:
p: float
T: float
rho: float
u: float
h: float
@dataclass(frozen=True)
class ThermodynamicPropertyTangents:
"""Directional derivatives of a recovered thermodynamic state."""
p: tuple[float, ...]
T: tuple[float, ...]
rho: tuple[float, ...]
u: tuple[float, ...]
h: tuple[float, ...]
@property
def width(self) -> int:
return len(self.p)
@classmethod
def zeros(cls, width: int) -> "ThermodynamicPropertyTangents":
values = (0.0,) * width
return cls(p=values, T=values, rho=values, u=values, h=values)
@dataclass(frozen=True)
class ThermodynamicPropertiesLinearization:
"""Primal properties and a validity-checked directional linearization."""
properties: ThermodynamicProperties
tangents: ThermodynamicPropertyTangents
valid: bool = True
reason: str | None = None
class GasMedium(Protocol):
"""Thermodynamic contract required by pneumatic components.
``IdealGasMedium`` is the default implementation. Keeping the component
boundary structural allows a later helium/Peng-Robinson implementation to
be registered without changing every AMESim component constructor.
"""
name: str
R_gas: float
cp_ref: float
T_ref: float
@property
def cv(self) -> float: ...
@property
def gamma(self) -> float: ...
def cp_at_temperature(self, T: float) -> float: ...
def cv_at_temperature(self, T: float) -> float: ...
def density(self, p: float, T: float) -> float: ...
def isentropic_density_pressure_factor(
self,
p: float,
T: float,
downstream_pressure: float | None = None,
) -> float: ...
def dynamic_viscosity(self, T: float) -> float: ...
def diagnostic_dynamic_viscosity(self, T: float) -> float: ...
def specific_internal_energy(self, T: float) -> float: ...
def specific_internal_energy_at_pressure(self, p: float, T: float) -> float: ...
def specific_enthalpy(self, T: float) -> float: ...
def specific_enthalpy_at_pressure(self, p: float, T: float) -> float: ...
def temperature_from_internal_energy(self, u: float) -> float: ...
def temperature_from_enthalpy(self, h: float) -> float: ...
def temperature_from_pressure_enthalpy(self, p: float, h: float) -> float: ...
def temperature_from_mass_internal_energy(self, m: float, U: float) -> float: ...
def pressure(self, m: float, T: float, V: float) -> float: ...
def properties_from_mU(
self,
m: float,
U: float,
V: float,
) -> ThermodynamicProperties: ...
def linearize_properties_from_mU(
self,
m: float,
U: float,
V: float,
dm: Sequence[float],
dU: Sequence[float],
dV: Sequence[float],
*,
properties: ThermodynamicProperties | None = None,
) -> ThermodynamicPropertiesLinearization: ...
@dataclass(frozen=True)
class IdealGasMedium:
"""Temperature-dependent ideal-gas air approximation.
This is still not a strict clone of `Modelica.Media.Air.SimpleAir`.
The small linear `cp(T)` term is kept configurable for calibration, but the
current default is calibrated against the committed Testmodel baseline and
therefore falls back to the constant-heat-capacity limit.
"""
name: str = "SimpleAirApprox"
name: str = 'SimpleAirApprox'
R_gas: float = 287.0
cp_ref: float = 1005.0
T_ref: float = 300.0
cp_slope: float = 0.0
viscosity_ref: float = 1.82e-5
viscosity_ref: float = 1.82e-05
viscosity_T_ref: float = 293.15
sutherland_constant: float = 110.4
@property
def cv(self) -> float:
return self.cv_at_temperature(self.T_ref)
@property
def gamma(self) -> float:
return self.cp_at_temperature(self.T_ref) / self.cv
def cp_at_temperature(self, T: float) -> float:
return self.cp_ref + self.cp_slope * (T - self.T_ref)
def cv_at_temperature(self, T: float) -> float:
return self.cp_at_temperature(T) - self.R_gas
@profile_property("density")
def density(self, p: float, T: float) -> float:
return p / (self.R_gas * T)
@profile_property("isentropic_density_pressure_factor")
def isentropic_density_pressure_factor(
self,
p: float,
T: float,
downstream_pressure: float | None = None,
) -> float:
del p
del downstream_pressure
cp = self.cp_at_temperature(T)
cv = self.cv_at_temperature(T)
return cv / cp
@profile_property("dynamic_viscosity")
def dynamic_viscosity(self, T: float) -> float:
"""Return dynamic viscosity using the default air Sutherland law."""
if T <= 0.0:
raise ValueError("Temperature must be positive.")
return (
self.viscosity_ref
* (T / self.viscosity_T_ref) ** 1.5
* (self.viscosity_T_ref + self.sutherland_constant)
/ (T + self.sutherland_constant)
)
def diagnostic_dynamic_viscosity(self, T: float) -> float:
"""Return the viscosity convention used by derived diagnostics.
Most media use the same transport property for dynamics and reported
diagnostics. Reference-library media may override this without
changing a calibrated constitutive flow relation.
"""
return self.dynamic_viscosity(T)
@profile_property("specific_internal_energy")
def specific_internal_energy(self, T: float) -> float:
delta_T = T - self.T_ref
return (
self.cv * self.T_ref
+ self.cv * delta_T
+ 0.5 * self.cp_slope * delta_T * delta_T
)
@profile_property("specific_internal_energy_at_pressure")
def specific_internal_energy_at_pressure(self, p: float, T: float) -> float:
del p
return self.specific_internal_energy(T)
@profile_property("specific_enthalpy")
def specific_enthalpy(self, T: float) -> float:
delta_T = T - self.T_ref
return (
self.cp_ref * self.T_ref
+ self.cp_ref * delta_T
+ 0.5 * self.cp_slope * delta_T * delta_T
)
@profile_property("specific_enthalpy_at_pressure")
def specific_enthalpy_at_pressure(self, p: float, T: float) -> float:
del p
return self.specific_enthalpy(T)
def temperature_from_internal_energy(self, u: float) -> float:
reference_internal_energy = self.cv * self.T_ref
delta_u = u - reference_internal_energy
if abs(self.cp_slope) <= 1e-15:
return self.T_ref + delta_u / self.cv
a = 0.5 * self.cp_slope
b = self.cv
c = -delta_u
discriminant = max(b * b - 4.0 * a * c, 0.0)
positive_root = (-b + discriminant**0.5) / (2.0 * a)
negative_root = (-b - discriminant**0.5) / (2.0 * a)
delta_T = positive_root if abs(positive_root) <= abs(negative_root) else negative_root
return self.T_ref + delta_T
def temperature_from_enthalpy(self, h: float) -> float:
reference_enthalpy = self.cp_ref * self.T_ref
delta_h = h - reference_enthalpy
if abs(self.cp_slope) <= 1e-15:
return self.T_ref + delta_h / self.cp_ref
a = 0.5 * self.cp_slope
b = self.cp_ref
c = -delta_h
discriminant = max(b * b - 4.0 * a * c, 0.0)
positive_root = (-b + discriminant**0.5) / (2.0 * a)
negative_root = (-b - discriminant**0.5) / (2.0 * a)
delta_T = positive_root if abs(positive_root) <= abs(negative_root) else negative_root
return self.T_ref + delta_T
@profile_property("temperature_from_pressure_enthalpy")
def temperature_from_pressure_enthalpy(self, p: float, h: float) -> float:
del p
return self.temperature_from_enthalpy(h)
def temperature_from_mass_internal_energy(self, m: float, U: float) -> float:
if m <= 0.0:
raise RecoverableTrialStateError(
"Mass must stay positive when recovering temperature."
)
return self.temperature_from_internal_energy(U / m)
def pressure(self, m: float, T: float, V: float) -> float:
if V <= 0.0:
raise ValueError("Volume must stay positive.")
return m * self.R_gas * T / V
@profile_property("properties_from_mU")
def properties_from_mU(self, m: float, U: float, V: float) -> ThermodynamicProperties:
T = self.temperature_from_mass_internal_energy(m, U)
p = self.pressure(m, T, V)
rho = m / V
u = U / m
h = self.specific_enthalpy(T)
return ThermodynamicProperties(p=p, T=T, rho=rho, u=u, h=h)
def linearize_properties_from_mU(
self,
m: float,
U: float,
V: float,
dm: Sequence[float],
dU: Sequence[float],
dV: Sequence[float],
*,
properties: ThermodynamicProperties | None = None,
) -> ThermodynamicPropertiesLinearization:
"""Linearize properties_from_mU for several seed directions."""
dm_values = tuple(float(value) for value in dm)
dU_values = tuple(float(value) for value in dU)
dV_values = tuple(float(value) for value in dV)
if not (len(dm_values) == len(dU_values) == len(dV_values)):
raise ValueError("Thermodynamic tangent vectors must have equal lengths.")
props = properties or self.properties_from_mU(m, U, V)
width = len(dm_values)
expected_density = m / V
expected_internal_energy = U / m
if (
abs(props.rho - expected_density)
> 1.0e-12 * max(abs(expected_density), 1.0)
or abs(props.u - expected_internal_energy)
> 1.0e-12 * max(abs(expected_internal_energy), 1.0)
):
return ThermodynamicPropertiesLinearization(
properties=props,
tangents=ThermodynamicPropertyTangents.zeros(width),
valid=False,
reason="properties_primal_mismatch",
)
if not all(
isfinite(value)
for values in (dm_values, dU_values, dV_values)
for value in values
):
return ThermodynamicPropertiesLinearization(
properties=props,
tangents=ThermodynamicPropertyTangents.zeros(width),
valid=False,
reason="non_finite_tangent_input",
)
cv = self.cv_at_temperature(props.T)
cp = self.cp_at_temperature(props.T)
if not isfinite(cv) or not isfinite(cp) or cv <= 0.0 or cp <= 0.0:
return ThermodynamicPropertiesLinearization(
properties=props,
tangents=ThermodynamicPropertyTangents.zeros(width),
valid=False,
reason="non_positive_heat_capacity",
)
drho: list[float] = []
du: list[float] = []
dT: list[float] = []
dp: list[float] = []
dh: list[float] = []
for mass_tangent, energy_tangent, volume_tangent in zip(
dm_values,
dU_values,
dV_values,
strict=True,
):
density_tangent = mass_tangent / V - m * volume_tangent / (V * V)
internal_energy_tangent = (
energy_tangent / m - U * mass_tangent / (m * m)
)
temperature_tangent = internal_energy_tangent / cv
pressure_tangent = self.R_gas * (
props.T * density_tangent + props.rho * temperature_tangent
)
enthalpy_tangent = cp * temperature_tangent
drho.append(density_tangent)
du.append(internal_energy_tangent)
dT.append(temperature_tangent)
dp.append(pressure_tangent)
dh.append(enthalpy_tangent)
tangent_values = (*drho, *du, *dT, *dp, *dh)
valid = all(isfinite(value) for value in tangent_values)
return ThermodynamicPropertiesLinearization(
properties=props,
tangents=ThermodynamicPropertyTangents(
p=tuple(dp),
T=tuple(dT),
rho=tuple(drho),
u=tuple(du),
h=tuple(dh),
),
valid=valid,
reason=None if valid else "non_finite_property_tangent",
)
GasMedium = IdealGasMedium
-424
View File
@@ -1,424 +0,0 @@
from __future__ import annotations
from app.simulation.core.errors import RecoverableTrialStateError
from dataclasses import dataclass
from math import acos, cos, isfinite, log, pi, sqrt
from app.simulation.performance import profile_property
UNIVERSAL_GAS_CONSTANT = 8.31446261815324
# Simcenter Amesim 2404 ``sag_reinit_eos_`` keeps more digits than the
# commonly printed Peng-Robinson constants 0.45724 and 0.07780.
PENG_ROBINSON_A_COEFFICIENT = 0.457235583
PENG_ROBINSON_B_COEFFICIENT = 0.07779607
@dataclass(frozen=True)
class PengRobinsonFluid:
"""Pure-fluid Peng-Robinson equation-of-state helper.
The class covers the equation-of-state layer plus the enthalpy departure
needed to compare AMESim pneumatic ``pn2hpti`` reference enthalpy flows.
"""
name: str
molar_mass: float
critical_temperature: float
critical_pressure: float
acentric_factor: float
@property
def specific_gas_constant(self) -> float:
return UNIVERSAL_GAS_CONSTANT / self.molar_mass
@property
def a_parameter(self) -> float:
return (
PENG_ROBINSON_A_COEFFICIENT
* UNIVERSAL_GAS_CONSTANT
* UNIVERSAL_GAS_CONSTANT
* self.critical_temperature
* self.critical_temperature
/ self.critical_pressure
)
@property
def b_parameter(self) -> float:
return (
PENG_ROBINSON_B_COEFFICIENT
* UNIVERSAL_GAS_CONSTANT
* self.critical_temperature
/ self.critical_pressure
)
@property
def kappa(self) -> float:
omega = self.acentric_factor
return 0.37464 + 1.54226 * omega - 0.26992 * omega * omega
def alpha(self, temperature: float) -> float:
self._validate_temperature(temperature)
reduced_temperature = temperature / self.critical_temperature
return (1.0 + self.kappa * (1.0 - sqrt(reduced_temperature))) ** 2.0
def alpha_temperature_derivative(self, temperature: float) -> float:
self._validate_temperature(temperature)
reduced_temperature = temperature / self.critical_temperature
sqrt_reduced_temperature = sqrt(reduced_temperature)
alpha_base = 1.0 + self.kappa * (1.0 - sqrt_reduced_temperature)
return -(
alpha_base
* self.kappa
/ (self.critical_temperature * sqrt_reduced_temperature)
)
def alpha_temperature_second_derivative(self, temperature: float) -> float:
self._validate_temperature(temperature)
reduced_temperature = temperature / self.critical_temperature
sqrt_reduced_temperature = sqrt(reduced_temperature)
alpha_base = 1.0 + self.kappa * (1.0 - sqrt_reduced_temperature)
return (
self.kappa
/ (2.0 * self.critical_temperature * self.critical_temperature)
* (
self.kappa / reduced_temperature
+ alpha_base / (reduced_temperature * sqrt_reduced_temperature)
)
)
def attractive_parameter(self, temperature: float) -> float:
return self.a_parameter * self.alpha(temperature)
def attractive_parameter_temperature_derivative(self, temperature: float) -> float:
return self.a_parameter * self.alpha_temperature_derivative(temperature)
def attractive_parameter_temperature_second_derivative(
self,
temperature: float,
) -> float:
return self.a_parameter * self.alpha_temperature_second_derivative(temperature)
@profile_property(
"pressure_from_molar_volume",
layer="kernel",
minimum_mode="audit",
)
def pressure_from_molar_volume(self, temperature: float, molar_volume: float) -> float:
self._validate_temperature(temperature)
if molar_volume <= self.b_parameter:
raise RecoverableTrialStateError("Molar volume must be larger than Peng-Robinson b parameter.")
a_alpha = self.attractive_parameter(temperature)
b = self.b_parameter
repulsive = UNIVERSAL_GAS_CONSTANT * temperature / (molar_volume - b)
attractive = a_alpha / (molar_volume * (molar_volume + b) + b * (molar_volume - b))
return repulsive - attractive
@profile_property(
"pressure_from_density",
layer="kernel",
minimum_mode="audit",
)
def pressure_from_density(self, temperature: float, density: float) -> float:
if density <= 0.0:
raise ValueError("Density must be positive.")
return self.pressure_from_molar_volume(temperature, self.molar_mass / density)
@profile_property(
"pressure_temperature_derivative_at_density",
layer="kernel",
minimum_mode="audit",
)
def pressure_temperature_derivative_at_density(
self,
temperature: float,
density: float,
) -> float:
self._validate_temperature(temperature)
if density <= 0.0:
raise ValueError("Density must be positive.")
molar_volume = self.molar_mass / density
if molar_volume <= self.b_parameter:
raise RecoverableTrialStateError(
"Molar volume must be larger than Peng-Robinson b parameter."
)
b = self.b_parameter
denominator = molar_volume * (molar_volume + b) + b * (molar_volume - b)
return (
UNIVERSAL_GAS_CONSTANT / (molar_volume - b)
- self.attractive_parameter_temperature_derivative(temperature) / denominator
)
@profile_property(
"pressure_density_derivative_at_temperature",
layer="kernel",
minimum_mode="audit",
)
def pressure_density_derivative_at_temperature(
self,
temperature: float,
density: float,
) -> float:
self._validate_temperature(temperature)
if density <= 0.0:
raise ValueError("Density must be positive.")
molar_volume = self.molar_mass / density
if molar_volume <= self.b_parameter:
raise RecoverableTrialStateError(
"Molar volume must be larger than Peng-Robinson b parameter."
)
b = self.b_parameter
denominator = molar_volume * (molar_volume + b) + b * (molar_volume - b)
pressure_molar_volume_derivative = (
-UNIVERSAL_GAS_CONSTANT * temperature / (molar_volume - b) ** 2
+ self.attractive_parameter(temperature)
* 2.0
* (molar_volume + b)
/ denominator**2
)
molar_volume_density_derivative = -self.molar_mass / (density * density)
return pressure_molar_volume_derivative * molar_volume_density_derivative
def reduced_parameters(self, pressure: float, temperature: float) -> tuple[float, float]:
self._validate_pressure_temperature(pressure, temperature)
a_alpha = self.attractive_parameter(temperature)
b = self.b_parameter
A = a_alpha * pressure / (UNIVERSAL_GAS_CONSTANT * UNIVERSAL_GAS_CONSTANT * temperature * temperature)
B = b * pressure / (UNIVERSAL_GAS_CONSTANT * temperature)
return A, B
@profile_property(
"compressibility_roots",
layer="kernel",
minimum_mode="audit",
)
def compressibility_roots(self, pressure: float, temperature: float) -> tuple[float, ...]:
A, B = self.reduced_parameters(pressure, temperature)
coefficients = (
-(1.0 - B),
A - 3.0 * B * B - 2.0 * B,
-(A * B - B * B - B * B * B),
)
roots = _real_cubic_roots(*coefficients)
physical_roots = tuple(sorted(root for root in roots if root > B and isfinite(root)))
if not physical_roots:
raise ValueError("Peng-Robinson cubic produced no physical compressibility root.")
return physical_roots
@profile_property(
"compressibility_factor",
layer="kernel",
minimum_mode="audit",
)
def compressibility_factor(
self,
pressure: float,
temperature: float,
phase: str = "vapor",
) -> float:
roots = self.compressibility_roots(pressure, temperature)
if phase == "vapor":
return roots[-1]
if phase == "liquid":
return roots[0]
if phase == "stable-single-root":
return roots[-1]
raise ValueError(f"Unsupported phase selector: {phase!r}")
@profile_property(
"molar_volume",
layer="kernel",
minimum_mode="audit",
)
def molar_volume(
self,
pressure: float,
temperature: float,
phase: str = "vapor",
) -> float:
z = self.compressibility_factor(pressure, temperature, phase=phase)
return z * UNIVERSAL_GAS_CONSTANT * temperature / pressure
@profile_property("density", layer="kernel", minimum_mode="audit")
def density(
self,
pressure: float,
temperature: float,
phase: str = "vapor",
) -> float:
return self.molar_mass / self.molar_volume(pressure, temperature, phase=phase)
@profile_property(
"residual_specific_enthalpy",
layer="kernel",
minimum_mode="audit",
)
def residual_specific_enthalpy(
self,
pressure: float,
temperature: float,
phase: str = "vapor",
) -> float:
"""Return Peng-Robinson enthalpy departure from ideal gas, J/kg."""
self._validate_pressure_temperature(pressure, temperature)
z = self.compressibility_factor(pressure, temperature, phase=phase)
_, B = self.reduced_parameters(pressure, temperature)
b = self.b_parameter
attractive = self.attractive_parameter(temperature)
d_attractive_d_temperature = (
self.attractive_parameter_temperature_derivative(temperature)
)
log_argument = (z + (1.0 + sqrt(2.0)) * B) / (
z + (1.0 - sqrt(2.0)) * B
)
residual_molar_enthalpy = (
UNIVERSAL_GAS_CONSTANT * temperature * (z - 1.0)
+ (
temperature * d_attractive_d_temperature
- attractive
)
* log(log_argument)
/ (2.0 * sqrt(2.0) * b)
)
return residual_molar_enthalpy / self.molar_mass
@profile_property(
"residual_specific_internal_energy_at_density",
layer="kernel",
minimum_mode="audit",
)
def residual_specific_internal_energy_at_density(
self,
temperature: float,
density: float,
) -> float:
"""Return Peng-Robinson internal-energy departure, J/kg."""
self._validate_temperature(temperature)
if density <= 0.0:
raise ValueError("Density must be positive.")
molar_volume = self.molar_mass / density
b = self.b_parameter
if molar_volume <= b:
raise RecoverableTrialStateError(
"Molar volume must be larger than Peng-Robinson b parameter."
)
attractive = self.attractive_parameter(temperature)
d_attractive_d_temperature = (
self.attractive_parameter_temperature_derivative(temperature)
)
log_argument = (
molar_volume + (1.0 + sqrt(2.0)) * b
) / (
molar_volume + (1.0 - sqrt(2.0)) * b
)
residual_molar_internal_energy = (
temperature * d_attractive_d_temperature - attractive
) * log(log_argument) / (2.0 * sqrt(2.0) * b)
return residual_molar_internal_energy / self.molar_mass
@profile_property(
"residual_isochoric_heat_capacity_at_density",
layer="kernel",
minimum_mode="audit",
)
def residual_isochoric_heat_capacity_at_density(
self,
temperature: float,
density: float,
) -> float:
"""Return the constant-volume heat-capacity departure, J/kg/K."""
self._validate_temperature(temperature)
if density <= 0.0:
raise ValueError("Density must be positive.")
molar_volume = self.molar_mass / density
b = self.b_parameter
if molar_volume <= b:
raise RecoverableTrialStateError(
"Molar volume must be larger than Peng-Robinson b parameter."
)
log_argument = (
molar_volume + (1.0 + sqrt(2.0)) * b
) / (
molar_volume + (1.0 - sqrt(2.0)) * b
)
residual_molar_cv = (
temperature
* self.attractive_parameter_temperature_second_derivative(temperature)
* log(log_argument)
/ (2.0 * sqrt(2.0) * b)
)
return residual_molar_cv / self.molar_mass
@staticmethod
def _validate_temperature(temperature: float) -> None:
if temperature <= 0.0:
raise RecoverableTrialStateError("Temperature must be positive.")
@classmethod
def _validate_pressure_temperature(cls, pressure: float, temperature: float) -> None:
if pressure <= 0.0:
raise RecoverableTrialStateError("Pressure must be positive.")
cls._validate_temperature(temperature)
HELIUM_PR = PengRobinsonFluid(
name="helium",
molar_mass=0.004002602,
critical_temperature=5.1953,
critical_pressure=227_460.0,
# Simcenter Amesim 2404 helium_eos.data.
acentric_factor=-0.382,
)
NITROGEN_PR = PengRobinsonFluid(
name="nitrogen",
molar_mass=0.0280134,
critical_temperature=126.192,
critical_pressure=3.3958e6,
acentric_factor=0.0372,
)
AIR_PR = PengRobinsonFluid(
name="air",
molar_mass=0.02896513,
critical_temperature=132.5306,
critical_pressure=3.786e6,
acentric_factor=0.0335,
)
def _real_cubic_roots(a: float, b: float, c: float) -> tuple[float, ...]:
"""Return real roots for x**3 + a*x**2 + b*x + c = 0."""
depressed_p = b - a * a / 3.0
depressed_q = 2.0 * a * a * a / 27.0 - a * b / 3.0 + c
discriminant = (depressed_q / 2.0) ** 2.0 + (depressed_p / 3.0) ** 3.0
offset = -a / 3.0
tolerance = 1e-14
if discriminant > tolerance:
sqrt_discriminant = sqrt(discriminant)
u = _real_cube_root(-depressed_q / 2.0 + sqrt_discriminant)
v = _real_cube_root(-depressed_q / 2.0 - sqrt_discriminant)
return (u + v + offset,)
if abs(discriminant) <= tolerance:
u = _real_cube_root(-depressed_q / 2.0)
return tuple(sorted({2.0 * u + offset, -u + offset}))
if depressed_p >= 0.0:
raise ValueError("Unexpected cubic state with three real roots and non-negative p.")
radius = 2.0 * sqrt(-depressed_p / 3.0)
argument = (3.0 * depressed_q / (2.0 * depressed_p)) * sqrt(-3.0 / depressed_p)
argument = max(-1.0, min(1.0, argument))
theta = acos(argument) / 3.0
roots = [
radius * cos(theta - 2.0 * pi * index / 3.0) + offset
for index in range(3)
]
return tuple(sorted(roots))
def _real_cube_root(value: float) -> float:
if value == 0.0:
return 0.0
return (1.0 if value > 0.0 else -1.0) * abs(value) ** (1.0 / 3.0)
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@@ -1,21 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
@dataclass
class VolumeState:
"""Primary dynamic state for rigid adiabatic control volumes."""
m: float
U: float
def as_vector(self) -> list[float]:
return [self.m, self.U]
@classmethod
def from_vector(cls, values: list[float]) -> "VolumeState":
if len(values) != 2:
raise ValueError("VolumeState requires exactly two values: [m, U].")
return cls(m=values[0], U=values[1])
-1
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@@ -1 +0,0 @@
"""Reference systems and regression examples."""
@@ -1,25 +0,0 @@
from __future__ import annotations
from app.simulation.examples.test_mql.system import (
TestMqlRunConfig,
TestMqlSimulationResult,
TestMqlSystem,
)
from app.simulation.examples.test_mql.run import (
PreparedTestMqlRun,
TestMqlRunResult,
prepare_test_mql_run,
run_prepared_test_mql,
run_test_mql,
)
__all__ = [
"PreparedTestMqlRun",
"TestMqlRunConfig",
"TestMqlRunResult",
"TestMqlSimulationResult",
"TestMqlSystem",
"prepare_test_mql_run",
"run_prepared_test_mql",
"run_test_mql",
]
@@ -1,77 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from pathlib import Path
from app.simulation.reporting.amesim_results import AmesimResults, load_test_mql_amesim_results
from app.simulation.reporting.test_mql_comparison import TestMqlComparisonResult
from app.simulation.reporting.test_mql_observations import (
TestMqlObservationCatalog,
build_test_mql_observation_catalog,
)
from app.simulation.reporting.test_mql_output_schema import (
TestMqlOutputSchema,
build_test_mql_output_schema,
)
from app.simulation.reporting.test_mql_output_validation import (
TestMqlValidatedOutput,
compare_validated_test_mql_output,
validate_test_mql_output,
)
@dataclass(frozen=True)
class TestMqlBaselineRun:
amesim_results: AmesimResults
observation_catalog: TestMqlObservationCatalog
output_schema: TestMqlOutputSchema
output: TestMqlValidatedOutput
comparison: TestMqlComparisonResult
@property
def sample_count(self) -> int:
return len(self.output.times)
@property
def signal_count(self) -> int:
return len(self.output.data_paths)
def run_test_mql_baseline_passthrough(
archive_path: Path,
*,
data_paths: tuple[str, ...] | list[str] | None = None,
) -> TestMqlBaselineRun:
amesim_results = load_test_mql_amesim_results(archive_path)
observation_catalog = build_test_mql_observation_catalog(amesim_results)
output_schema = build_test_mql_output_schema(
amesim_results,
observation_catalog=observation_catalog,
)
selected_paths = tuple(data_paths) if data_paths is not None else output_schema.data_paths()
baseline_series = observation_catalog.baseline_series_by_data_path(
amesim_results,
selected_paths,
)
output = validate_test_mql_output(
times=amesim_results.times,
series_by_data_path=baseline_series,
schema=output_schema,
data_paths=selected_paths,
require_all_schema_paths=data_paths is None,
)
comparison = compare_validated_test_mql_output(
times=output.times,
series_by_data_path=output.series_by_data_path,
schema=output_schema,
amesim_results=amesim_results,
data_paths=output.data_paths,
require_all_schema_paths=data_paths is None,
)
return TestMqlBaselineRun(
amesim_results=amesim_results,
observation_catalog=observation_catalog,
output_schema=output_schema,
output=output,
comparison=comparison,
)
File diff suppressed because it is too large. Load diff
@@ -1,468 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from pathlib import Path
from app.simulation.examples.test_mql.primitives.pneumatic import m3_to_cm3
from app.simulation.reporting.amesim_results import AmesimResults, load_test_mql_amesim_results
from app.simulation.reporting.test_mql_comparison import TestMqlComparisonResult
from app.simulation.reporting.test_mql_observations import (
TestMqlObservationCatalog,
build_test_mql_observation_catalog,
)
from app.simulation.reporting.test_mql_output_schema import (
TestMqlOutputSchema,
build_test_mql_output_schema,
)
from app.simulation.reporting.test_mql_output_validation import (
TestMqlValidatedOutput,
compare_validated_test_mql_output,
validate_test_mql_output,
)
from app.simulation.reporting.test_mql_variables import build_test_mql_variable_catalog
from app.simulation.examples.test_mql.mechanical import (
TestMqlMechanicalAssembly,
build_test_mql_mechanical_assembly,
)
from app.simulation.examples.test_mql.pneumatic import (
TestMqlPneumaticAssembly,
build_test_mql_pneumatic_assembly,
)
@dataclass(frozen=True)
class TestMqlComputedPistonGeometryRun:
amesim_results: AmesimResults
observation_catalog: TestMqlObservationCatalog
output_schema: TestMqlOutputSchema
mechanical_assembly: TestMqlMechanicalAssembly
output: TestMqlValidatedOutput
comparison: TestMqlComparisonResult
@property
def sample_count(self) -> int:
return len(self.output.times)
@property
def signal_count(self) -> int:
return len(self.output.data_paths)
@dataclass(frozen=True)
class TestMqlComputedGeometryRun:
amesim_results: AmesimResults
observation_catalog: TestMqlObservationCatalog
output_schema: TestMqlOutputSchema
mechanical_assembly: TestMqlMechanicalAssembly
pneumatic_assembly: TestMqlPneumaticAssembly
output: TestMqlValidatedOutput
comparison: TestMqlComparisonResult
@property
def sample_count(self) -> int:
return len(self.output.times)
@property
def signal_count(self) -> int:
return len(self.output.data_paths)
@dataclass(frozen=True)
class TestMqlComputedLineRelationsRun:
amesim_results: AmesimResults
observation_catalog: TestMqlObservationCatalog
output_schema: TestMqlOutputSchema
output: TestMqlValidatedOutput
comparison: TestMqlComparisonResult
@property
def sample_count(self) -> int:
return len(self.output.times)
@property
def signal_count(self) -> int:
return len(self.output.data_paths)
@dataclass(frozen=True)
class TestMqlComputedPneumaticRelationsRun:
amesim_results: AmesimResults
observation_catalog: TestMqlObservationCatalog
output_schema: TestMqlOutputSchema
output: TestMqlValidatedOutput
comparison: TestMqlComparisonResult
@property
def sample_count(self) -> int:
return len(self.output.times)
@property
def signal_count(self) -> int:
return len(self.output.data_paths)
@dataclass(frozen=True)
class TestMqlComputedMechanicalRelationsRun:
amesim_results: AmesimResults
observation_catalog: TestMqlObservationCatalog
output_schema: TestMqlOutputSchema
mechanical_assembly: TestMqlMechanicalAssembly
output: TestMqlValidatedOutput
comparison: TestMqlComparisonResult
@property
def sample_count(self) -> int:
return len(self.output.times)
@property
def signal_count(self) -> int:
return len(self.output.data_paths)
def run_test_mql_computed_piston_geometry(
archive_path: Path,
) -> TestMqlComputedPistonGeometryRun:
amesim_results = load_test_mql_amesim_results(archive_path)
observation_catalog = build_test_mql_observation_catalog(amesim_results)
output_schema = build_test_mql_output_schema(
amesim_results,
observation_catalog=observation_catalog,
)
variable_catalog = build_test_mql_variable_catalog(amesim_results)
mechanical_assembly = build_test_mql_mechanical_assembly(
amesim_results=amesim_results,
variable_catalog=variable_catalog,
)
output_series = _compute_piston_geometry_series(amesim_results, mechanical_assembly)
output_data_paths = tuple(output_series)
output = validate_test_mql_output(
times=amesim_results.times,
series_by_data_path=output_series,
schema=output_schema,
data_paths=output_data_paths,
)
comparison = compare_validated_test_mql_output(
times=output.times,
series_by_data_path=output.series_by_data_path,
schema=output_schema,
amesim_results=amesim_results,
data_paths=output.data_paths,
)
return TestMqlComputedPistonGeometryRun(
amesim_results=amesim_results,
observation_catalog=observation_catalog,
output_schema=output_schema,
mechanical_assembly=mechanical_assembly,
output=output,
comparison=comparison,
)
def run_test_mql_computed_geometry(
archive_path: Path,
) -> TestMqlComputedGeometryRun:
amesim_results = load_test_mql_amesim_results(archive_path)
observation_catalog = build_test_mql_observation_catalog(amesim_results)
output_schema = build_test_mql_output_schema(
amesim_results,
observation_catalog=observation_catalog,
)
variable_catalog = build_test_mql_variable_catalog(amesim_results)
mechanical_assembly = build_test_mql_mechanical_assembly(
amesim_results=amesim_results,
variable_catalog=variable_catalog,
)
pneumatic_assembly = build_test_mql_pneumatic_assembly()
output_series = {
**_compute_piston_geometry_series(amesim_results, mechanical_assembly),
**_compute_variable_chamber_volume_series(
amesim_results,
mechanical_assembly,
pneumatic_assembly,
),
}
output_data_paths = tuple(output_series)
output = validate_test_mql_output(
times=amesim_results.times,
series_by_data_path=output_series,
schema=output_schema,
data_paths=output_data_paths,
)
comparison = compare_validated_test_mql_output(
times=output.times,
series_by_data_path=output.series_by_data_path,
schema=output_schema,
amesim_results=amesim_results,
data_paths=output.data_paths,
)
return TestMqlComputedGeometryRun(
amesim_results=amesim_results,
observation_catalog=observation_catalog,
output_schema=output_schema,
mechanical_assembly=mechanical_assembly,
pneumatic_assembly=pneumatic_assembly,
output=output,
comparison=comparison,
)
def run_test_mql_computed_line_relations(
archive_path: Path,
) -> TestMqlComputedLineRelationsRun:
amesim_results = load_test_mql_amesim_results(archive_path)
observation_catalog = build_test_mql_observation_catalog(amesim_results)
output_schema = build_test_mql_output_schema(
amesim_results,
observation_catalog=observation_catalog,
)
output_series = _compute_line_reversed_series(amesim_results, observation_catalog)
output_data_paths = tuple(output_series)
output = validate_test_mql_output(
times=amesim_results.times,
series_by_data_path=output_series,
schema=output_schema,
data_paths=output_data_paths,
)
comparison = compare_validated_test_mql_output(
times=output.times,
series_by_data_path=output.series_by_data_path,
schema=output_schema,
amesim_results=amesim_results,
data_paths=output.data_paths,
)
return TestMqlComputedLineRelationsRun(
amesim_results=amesim_results,
observation_catalog=observation_catalog,
output_schema=output_schema,
output=output,
comparison=comparison,
)
def run_test_mql_computed_pneumatic_relations(
archive_path: Path,
) -> TestMqlComputedPneumaticRelationsRun:
amesim_results = load_test_mql_amesim_results(archive_path)
observation_catalog = build_test_mql_observation_catalog(amesim_results)
output_schema = build_test_mql_output_schema(
amesim_results,
observation_catalog=observation_catalog,
)
output_series = {
**_compute_chamber_duplicate_series(amesim_results, observation_catalog),
**_compute_orifice_reversed_series(amesim_results, observation_catalog),
}
output_data_paths = tuple(output_series)
output = validate_test_mql_output(
times=amesim_results.times,
series_by_data_path=output_series,
schema=output_schema,
data_paths=output_data_paths,
)
comparison = compare_validated_test_mql_output(
times=output.times,
series_by_data_path=output.series_by_data_path,
schema=output_schema,
amesim_results=amesim_results,
data_paths=output.data_paths,
)
return TestMqlComputedPneumaticRelationsRun(
amesim_results=amesim_results,
observation_catalog=observation_catalog,
output_schema=output_schema,
output=output,
comparison=comparison,
)
def run_test_mql_computed_mechanical_relations(
archive_path: Path,
) -> TestMqlComputedMechanicalRelationsRun:
amesim_results = load_test_mql_amesim_results(archive_path)
observation_catalog = build_test_mql_observation_catalog(amesim_results)
output_schema = build_test_mql_output_schema(
amesim_results,
observation_catalog=observation_catalog,
)
variable_catalog = build_test_mql_variable_catalog(amesim_results)
mechanical_assembly = build_test_mql_mechanical_assembly(
amesim_results=amesim_results,
variable_catalog=variable_catalog,
)
output_series = {
**_compute_mass_duplicate_series(amesim_results, mechanical_assembly),
**_compute_inactive_mass_force_series(amesim_results, mechanical_assembly),
**_compute_zero_force_source_series(amesim_results, mechanical_assembly),
}
output_data_paths = tuple(output_series)
output = validate_test_mql_output(
times=amesim_results.times,
series_by_data_path=output_series,
schema=output_schema,
data_paths=output_data_paths,
)
comparison = compare_validated_test_mql_output(
times=output.times,
series_by_data_path=output.series_by_data_path,
schema=output_schema,
amesim_results=amesim_results,
data_paths=output.data_paths,
)
return TestMqlComputedMechanicalRelationsRun(
amesim_results=amesim_results,
observation_catalog=observation_catalog,
output_schema=output_schema,
mechanical_assembly=mechanical_assembly,
output=output,
comparison=comparison,
)
def _compute_piston_geometry_series(
amesim_results: AmesimResults,
mechanical_assembly: TestMqlMechanicalAssembly,
) -> dict[str, tuple[float, ...]]:
series_by_data_path: dict[str, tuple[float, ...]] = {}
for alias in sorted(mechanical_assembly.pistons):
piston = mechanical_assembly.pistons[alias]
geometry = piston.geometry()
x4 = amesim_results.series(f"x4@{alias}")
x5 = amesim_results.series(f"x5@{alias}")
v4 = amesim_results.series(f"v4@{alias}")
v5 = amesim_results.series(f"v5@{alias}")
series_by_data_path[f"length@{alias}"] = tuple(
geometry.chamber_length_mm(port4, port5)
for port4, port5 in zip(x4, x5)
)
series_by_data_path[f"vol1@{alias}"] = tuple(
geometry.chamber_volume_cm3(port4, port5)
for port4, port5 in zip(x4, x5)
)
series_by_data_path[f"vvol1@{alias}"] = tuple(
geometry.chamber_volume_rate_l_min(port4, port5)
for port4, port5 in zip(v4, v5)
)
return series_by_data_path
def _compute_variable_chamber_volume_series(
amesim_results: AmesimResults,
mechanical_assembly: TestMqlMechanicalAssembly,
pneumatic_assembly: TestMqlPneumaticAssembly,
) -> dict[str, tuple[float, ...]]:
series_by_data_path: dict[str, tuple[float, ...]] = {}
for chamber_alias in sorted(pneumatic_assembly.variable_chambers):
chamber = pneumatic_assembly.variable_chambers[chamber_alias]
piston_alias = _piston_alias_for_variable_chamber(chamber_alias)
piston = mechanical_assembly.pistons[piston_alias]
geometry = piston.geometry()
x4 = amesim_results.series(f"x4@{piston_alias}")
x5 = amesim_results.series(f"x5@{piston_alias}")
dead_volume_cm3 = m3_to_cm3(chamber.dead_volume)
series_by_data_path[f"vol@{chamber_alias}"] = tuple(
dead_volume_cm3 + geometry.chamber_volume_cm3(port4, port5)
for port4, port5 in zip(x4, x5)
)
return series_by_data_path
def _piston_alias_for_variable_chamber(chamber_alias: str) -> str:
if not chamber_alias.startswith("pn_c1"):
raise ValueError(f"Unexpected PNCH012 alias: {chamber_alias}")
return chamber_alias.replace("pn_c1", "pn_brp2", 1)
def _compute_mass_duplicate_series(
amesim_results: AmesimResults,
mechanical_assembly: TestMqlMechanicalAssembly,
) -> dict[str, tuple[float, ...]]:
series_by_data_path: dict[str, tuple[float, ...]] = {}
for alias in sorted(mechanical_assembly.masses):
for signal_name in ("x1", "v1", "acc1"):
source_path = f"{signal_name}@{alias}"
duplicate_path = f"{signal_name}dup@{alias}"
series_by_data_path[duplicate_path] = tuple(
-value for value in amesim_results.series(source_path)
)
return series_by_data_path
def _compute_inactive_mass_force_series(
amesim_results: AmesimResults,
mechanical_assembly: TestMqlMechanicalAssembly,
) -> dict[str, tuple[float, ...]]:
series_by_data_path: dict[str, tuple[float, ...]] = {}
for alias in sorted(mechanical_assembly.masses):
mass = mechanical_assembly.masses[alias].endstop()
x1 = amesim_results.series(f"x1@{alias}")
v1 = amesim_results.series(f"v1@{alias}")
series_by_data_path[f"Fmin@{alias}"] = tuple(
mass.lower_static_force_magnitude(displacement)
for displacement in x1
)
series_by_data_path[f"Fvisc@{alias}"] = tuple(
mass.viscous_friction_force(velocity)
for velocity in v1
)
series_by_data_path[f"Ffric@{alias}"] = tuple(0.0 for _ in x1)
return series_by_data_path
def _compute_zero_force_source_series(
amesim_results: AmesimResults,
mechanical_assembly: TestMqlMechanicalAssembly,
) -> dict[str, tuple[float, ...]]:
return {
f"fzero@{alias}": tuple(0.0 for _ in amesim_results.times)
for alias in sorted(mechanical_assembly.zero_force_sources)
}
def _compute_chamber_duplicate_series(
amesim_results: AmesimResults,
observation_catalog: TestMqlObservationCatalog,
) -> dict[str, tuple[float, ...]]:
series_by_data_path: dict[str, tuple[float, ...]] = {}
for binding in observation_catalog.chambers.bindings:
pressure_series = amesim_results.series(binding.pressure_path)
temperature_series = amesim_results.series(binding.temperature_path)
for duplicate_path in binding.pressure_duplicate_paths:
series_by_data_path[duplicate_path] = tuple(pressure_series)
for duplicate_path in binding.temperature_duplicate_paths:
series_by_data_path[duplicate_path] = tuple(temperature_series)
return series_by_data_path
def _compute_orifice_reversed_series(
amesim_results: AmesimResults,
observation_catalog: TestMqlObservationCatalog,
) -> dict[str, tuple[float, ...]]:
series_by_data_path: dict[str, tuple[float, ...]] = {}
for binding in observation_catalog.orifices.bindings:
series_by_data_path[binding.reversed_mass_flow_path] = tuple(
-value for value in amesim_results.series(binding.primary_mass_flow_path)
)
series_by_data_path[binding.reversed_enthalpy_flow_path] = tuple(
-value for value in amesim_results.series(binding.primary_enthalpy_flow_path)
)
return series_by_data_path
def _compute_line_reversed_series(
amesim_results: AmesimResults,
observation_catalog: TestMqlObservationCatalog,
) -> dict[str, tuple[float, ...]]:
series_by_data_path: dict[str, tuple[float, ...]] = {}
for binding in observation_catalog.lines.by_submodel("PNL00R"):
if len(binding.mass_flow_paths) != 2 or len(binding.enthalpy_flow_paths) != 2:
raise ValueError(f"Expected two PNL00R flow paths for {binding.alias}.")
primary_mass_path, reversed_mass_path = binding.mass_flow_paths
primary_enthalpy_path, reversed_enthalpy_path = binding.enthalpy_flow_paths
series_by_data_path[reversed_mass_path] = tuple(
-value for value in amesim_results.series(primary_mass_path)
)
series_by_data_path[reversed_enthalpy_path] = tuple(
-value for value in amesim_results.series(primary_enthalpy_path)
)
return series_by_data_path
-151
View File
@@ -1,151 +0,0 @@
from __future__ import annotations
import ast
import operator
from dataclasses import dataclass
from math import isfinite
from typing import Any
from app.simulation.core.peng_robinson import HELIUM_PR, PengRobinsonFluid
from app.simulation.examples.test_mql.system import COMPONENT_SPECS, GLOBAL_PARAMETERS
_BINARY_OPERATORS = {
ast.Add: operator.add,
ast.Sub: operator.sub,
ast.Mult: operator.mul,
ast.Div: operator.truediv,
ast.Pow: operator.pow,
}
_UNARY_OPERATORS = {
ast.UAdd: operator.pos,
ast.USub: operator.neg,
}
class TestMqlExpressionError(ValueError):
"""Raised when an AMESim parameter expression cannot be resolved safely."""
@dataclass(frozen=True)
class TestMqlResolvedParameter:
name: str
title: str
raw_value: str
units: str
value: float | None
@property
def is_numeric(self) -> bool:
return self.value is not None
@dataclass(frozen=True)
class TestMqlResolvedComponent:
alias: str
component_name: str
submodel: str
label: str
parameters: dict[str, TestMqlResolvedParameter]
def parameter_value(self, name: str) -> float:
parameter = self.parameters[name]
if parameter.value is None:
raise KeyError(f"Parameter {name!r} on {self.alias!r} is not numeric")
return parameter.value
@dataclass(frozen=True)
class TestMqlConfig:
raw_global_parameters: dict[str, str]
global_parameters: dict[str, float]
fluid: PengRobinsonFluid
components: tuple[TestMqlResolvedComponent, ...]
@classmethod
def from_amesim_specs(cls) -> "TestMqlConfig":
raw_globals = dict(GLOBAL_PARAMETERS)
numeric_globals = {
name: value
for name, raw in raw_globals.items()
if (value := resolve_numeric_expression(raw, {})) is not None
}
components = tuple(
_resolve_component(spec, numeric_globals)
for spec in COMPONENT_SPECS
)
return cls(
raw_global_parameters=raw_globals,
global_parameters=numeric_globals,
fluid=HELIUM_PR,
components=components,
)
def component(self, alias: str) -> TestMqlResolvedComponent:
for component in self.components:
if component.alias == alias:
return component
raise KeyError(alias)
def components_by_submodel(self, submodel: str) -> tuple[TestMqlResolvedComponent, ...]:
return tuple(component for component in self.components if component.submodel == submodel)
def _resolve_component(
spec: dict[str, Any],
variables: dict[str, float],
) -> TestMqlResolvedComponent:
parameters = {}
for parameter in spec.get("parameters", []):
name = str(parameter["name"])
raw_value = str(parameter["value"])
parameters[name] = TestMqlResolvedParameter(
name=name,
title=str(parameter["title"]),
raw_value=raw_value,
units=str(parameter["units"]),
value=resolve_numeric_expression(raw_value, variables),
)
return TestMqlResolvedComponent(
alias=str(spec["alias"]),
component_name=str(spec["component_name"]),
submodel=str(spec["submodel"]),
label=str(spec["label"]),
parameters=parameters,
)
def resolve_numeric_expression(
expression: str,
variables: dict[str, float],
) -> float | None:
expression = expression.strip()
if not expression:
return None
normalized = expression.replace("^", "**")
try:
parsed = ast.parse(normalized, mode="eval")
value = float(_eval_node(parsed.body, variables))
except (SyntaxError, TestMqlExpressionError, ValueError, TypeError, ZeroDivisionError):
return None
return value if isfinite(value) else None
def _eval_node(node: ast.AST, variables: dict[str, float]) -> float:
if isinstance(node, ast.Constant) and isinstance(node.value, (int, float)):
return float(node.value)
if isinstance(node, ast.Name):
if node.id not in variables:
raise TestMqlExpressionError(f"Unknown variable: {node.id}")
return float(variables[node.id])
if isinstance(node, ast.BinOp):
operator_type = type(node.op)
if operator_type not in _BINARY_OPERATORS:
raise TestMqlExpressionError(f"Unsupported binary operator: {operator_type}")
return float(_BINARY_OPERATORS[operator_type](_eval_node(node.left, variables), _eval_node(node.right, variables)))
if isinstance(node, ast.UnaryOp):
operator_type = type(node.op)
if operator_type not in _UNARY_OPERATORS:
raise TestMqlExpressionError(f"Unsupported unary operator: {operator_type}")
return float(_UNARY_OPERATORS[operator_type](_eval_node(node.operand, variables)))
raise TestMqlExpressionError(f"Unsupported expression node: {type(node)}")
@@ -1,451 +0,0 @@
from __future__ import annotations
import re
import tarfile
from dataclasses import dataclass
from pathlib import Path
from app.simulation.examples.test_mql.system import CONNECTION_SPECS, GLOBAL_PARAMETERS
from app.simulation.examples.test_mql.config import resolve_numeric_expression
AMESIM_REFERENCE_PRESSURE_PA = 101_300.0
@dataclass(frozen=True)
class TestMqlPnl0001Spec:
alias: str
source_component: str
source_port: str
target_component: str
target_port: str
diameter_mm: float
length_m: float
relative_roughness: float
polytropic_constant: float
heat_transfer_coefficient: float
external_temperature_k: float
gas_type_index: int
mode: int
initial_temperature_k: float
initial_gauge_pressure_pa: float
@property
def initial_absolute_pressure_pa(self) -> float:
return self.initial_gauge_pressure_pa + AMESIM_REFERENCE_PRESSURE_PA
@dataclass(frozen=True)
class TestMqlPnl0002Spec:
alias: str
source_component: str
source_port: str
target_component: str
target_port: str
diameter_mm: float
length_m: float
relative_roughness: float
polytropic_constant: float
heat_transfer_coefficient: float
external_temperature_k: float
gas_type_index: int
mode: int
initial_center_temperature_k: float
initial_center_gauge_pressure_pa: float
@property
def initial_center_absolute_pressure_pa(self) -> float:
return self.initial_center_gauge_pressure_pa + AMESIM_REFERENCE_PRESSURE_PA
@dataclass(frozen=True)
class TestMqlPnl0003Spec:
alias: str
source_component: str
source_port: str
target_component: str
target_port: str
diameter_mm: float
length_m: float
relative_roughness: float
polytropic_constant: float
heat_transfer_coefficient: float
external_temperature_k: float
gas_type_index: int
mode: int
initial_temperature_1_k: float
initial_gauge_pressure_1_pa: float
initial_temperature_2_k: float
initial_gauge_pressure_2_pa: float
@property
def initial_absolute_pressure_1_pa(self) -> float:
return self.initial_gauge_pressure_1_pa + AMESIM_REFERENCE_PRESSURE_PA
@property
def initial_absolute_pressure_2_pa(self) -> float:
return self.initial_gauge_pressure_2_pa + AMESIM_REFERENCE_PRESSURE_PA
@dataclass(frozen=True)
class TestMqlPnl00rSpec:
alias: str
source_component: str
source_port: str
target_component: str
target_port: str
diameter_mm: float
length_m: float
relative_roughness: float
gas_type_index: int
def load_test_mql_pnl0001_specs(
archive_path: str | Path,
*,
cir_member: str = "test_mql_.cir",
) -> tuple[TestMqlPnl0001Spec, ...]:
"""Load resolved PNL0001 geometry and initial states from the AMESim source."""
with tarfile.open(archive_path) as archive:
cir_file = archive.extractfile(cir_member)
if cir_file is None:
raise ValueError(f"Missing AMESim circuit member: {cir_member}")
cir_text = cir_file.read().decode("latin1")
numeric_globals = {
name: value
for name, expression in GLOBAL_PARAMETERS.items()
if (value := resolve_numeric_expression(expression, {})) is not None
}
connections = {
str(connection["alias"]): connection
for connection in CONNECTION_SPECS
if connection["submodel"] == "PNL0001"
}
specs = []
for block in re.findall(r"<LINE>.*?</LINE>", cir_text, flags=re.DOTALL):
if _optional_text(block, "SUB_NAME") != "PNL0001":
continue
alias = _required_text(block, "ALIAS")
connection = connections.get(alias)
if connection is None:
raise ValueError(f"PNL0001 line {alias!r} is absent from CONNECTION_SPECS")
real_parameters = _parameter_expressions(block, "RPARAM")
integer_parameters = _parameter_expressions(block, "IPARAM")
state_values = _evar_values(block)
specs.append(
TestMqlPnl0001Spec(
alias=alias,
source_component=str(connection["source_component"]),
source_port=str(connection["source_port"]),
target_component=str(connection["target_component"]),
target_port=str(connection["target_port"]),
diameter_mm=_required_numeric(
alias, "diam", real_parameters, numeric_globals
),
length_m=_required_numeric(alias, "le", real_parameters, numeric_globals),
relative_roughness=_required_numeric(
alias, "rr", real_parameters, numeric_globals
),
polytropic_constant=_required_numeric(
alias, "k", real_parameters, numeric_globals
),
heat_transfer_coefficient=_required_numeric(
alias, "kth", real_parameters, numeric_globals
),
external_temperature_k=_required_numeric(
alias, "extemp", real_parameters, numeric_globals
),
gas_type_index=int(
_required_numeric(alias, "gi", integer_parameters, numeric_globals)
),
mode=int(
_required_numeric(alias, "mode", integer_parameters, numeric_globals)
),
initial_temperature_k=_required_numeric(
alias, "t2", state_values, numeric_globals
),
initial_gauge_pressure_pa=_required_numeric(
alias, "p2", state_values, numeric_globals
),
)
)
if set(connections) != {spec.alias for spec in specs}:
missing = sorted(set(connections) - {spec.alias for spec in specs})
raise ValueError(f"Missing PNL0001 parameter blocks: {missing}")
return tuple(specs)
def load_test_mql_pnl0002_specs(
archive_path: str | Path,
*,
cir_member: str = "test_mql_.cir",
) -> tuple[TestMqlPnl0002Spec, ...]:
"""Load resolved PNL0002 geometry and center compliance initial state."""
with tarfile.open(archive_path) as archive:
cir_file = archive.extractfile(cir_member)
if cir_file is None:
raise ValueError(f"Missing AMESim circuit member: {cir_member}")
cir_text = cir_file.read().decode("latin1")
numeric_globals = {
name: value
for name, expression in GLOBAL_PARAMETERS.items()
if (value := resolve_numeric_expression(expression, {})) is not None
}
connections = {
str(connection["alias"]): connection
for connection in CONNECTION_SPECS
if connection["submodel"] == "PNL0002"
}
specs = []
for block in re.findall(r"<LINE>.*?</LINE>", cir_text, flags=re.DOTALL):
if _optional_text(block, "SUB_NAME") != "PNL0002":
continue
alias = _required_text(block, "ALIAS")
connection = connections.get(alias)
if connection is None:
raise ValueError(f"PNL0002 line {alias!r} is absent from CONNECTION_SPECS")
real_parameters = _parameter_expressions(block, "RPARAM")
integer_parameters = _parameter_expressions(block, "IPARAM")
state_values = _ivar_values(block)
specs.append(
TestMqlPnl0002Spec(
alias=alias,
source_component=str(connection["source_component"]),
source_port=str(connection["source_port"]),
target_component=str(connection["target_component"]),
target_port=str(connection["target_port"]),
diameter_mm=_required_numeric(
alias, "diam", real_parameters, numeric_globals
),
length_m=_required_numeric(alias, "le", real_parameters, numeric_globals),
relative_roughness=_required_numeric(
alias, "rr", real_parameters, numeric_globals
),
polytropic_constant=_required_numeric(
alias, "k", real_parameters, numeric_globals
),
heat_transfer_coefficient=_required_numeric(
alias, "kth", real_parameters, numeric_globals
),
external_temperature_k=_required_numeric(
alias, "extemp", real_parameters, numeric_globals
),
gas_type_index=int(
_required_numeric(alias, "gi", integer_parameters, numeric_globals)
),
mode=int(
_required_numeric(alias, "mode", integer_parameters, numeric_globals)
),
initial_center_temperature_k=_required_numeric(
alias, "tctr", state_values, numeric_globals
),
initial_center_gauge_pressure_pa=_required_numeric(
alias, "pctr", state_values, numeric_globals
),
)
)
if set(connections) != {spec.alias for spec in specs}:
missing = sorted(set(connections) - {spec.alias for spec in specs})
raise ValueError(f"Missing PNL0002 parameter blocks: {missing}")
return tuple(specs)
def load_test_mql_pnl0003_specs(
archive_path: str | Path,
*,
cir_member: str = "test_mql_.cir",
) -> tuple[TestMqlPnl0003Spec, ...]:
"""Load resolved PNL0003 geometry and both compliance initial states."""
with tarfile.open(archive_path) as archive:
cir_file = archive.extractfile(cir_member)
if cir_file is None:
raise ValueError(f"Missing AMESim circuit member: {cir_member}")
cir_text = cir_file.read().decode("latin1")
numeric_globals = {
name: value
for name, expression in GLOBAL_PARAMETERS.items()
if (value := resolve_numeric_expression(expression, {})) is not None
}
connections = {
str(connection["alias"]): connection
for connection in CONNECTION_SPECS
if connection["submodel"] == "PNL0003"
}
specs = []
for block in re.findall(r"<LINE>.*?</LINE>", cir_text, flags=re.DOTALL):
if _optional_text(block, "SUB_NAME") != "PNL0003":
continue
alias = _required_text(block, "ALIAS")
connection = connections.get(alias)
if connection is None:
raise ValueError(f"PNL0003 line {alias!r} is absent from CONNECTION_SPECS")
real_parameters = _parameter_expressions(block, "RPARAM")
integer_parameters = _parameter_expressions(block, "IPARAM")
state_values = _evar_values(block)
specs.append(
TestMqlPnl0003Spec(
alias=alias,
source_component=str(connection["source_component"]),
source_port=str(connection["source_port"]),
target_component=str(connection["target_component"]),
target_port=str(connection["target_port"]),
diameter_mm=_required_numeric(
alias, "diam", real_parameters, numeric_globals
),
length_m=_required_numeric(alias, "le", real_parameters, numeric_globals),
relative_roughness=_required_numeric(
alias, "rr", real_parameters, numeric_globals
),
polytropic_constant=_required_numeric(
alias, "k", real_parameters, numeric_globals
),
heat_transfer_coefficient=_required_numeric(
alias, "kth", real_parameters, numeric_globals
),
external_temperature_k=_required_numeric(
alias, "extemp", real_parameters, numeric_globals
),
gas_type_index=int(
_required_numeric(alias, "gi", integer_parameters, numeric_globals)
),
mode=int(
_required_numeric(alias, "mode", integer_parameters, numeric_globals)
),
initial_temperature_1_k=_required_numeric(
alias, "t1", state_values, numeric_globals
),
initial_gauge_pressure_1_pa=_required_numeric(
alias, "p1", state_values, numeric_globals
),
initial_temperature_2_k=_required_numeric(
alias, "t2", state_values, numeric_globals
),
initial_gauge_pressure_2_pa=_required_numeric(
alias, "p2", state_values, numeric_globals
),
)
)
if set(connections) != {spec.alias for spec in specs}:
missing = sorted(set(connections) - {spec.alias for spec in specs})
raise ValueError(f"Missing PNL0003 parameter blocks: {missing}")
return tuple(specs)
def load_test_mql_pnl00r_specs(
archive_path: str | Path,
*,
cir_member: str = "test_mql_.cir",
) -> tuple[TestMqlPnl00rSpec, ...]:
"""Load resolved PNL00R geometry from the AMESim source."""
with tarfile.open(archive_path) as archive:
cir_file = archive.extractfile(cir_member)
if cir_file is None:
raise ValueError(f"Missing AMESim circuit member: {cir_member}")
cir_text = cir_file.read().decode("latin1")
numeric_globals = {
name: value
for name, expression in GLOBAL_PARAMETERS.items()
if (value := resolve_numeric_expression(expression, {})) is not None
}
connections = {
str(connection["alias"]): connection
for connection in CONNECTION_SPECS
if connection["submodel"] == "PNL00R"
}
specs = []
for block in re.findall(r"<LINE>.*?</LINE>", cir_text, flags=re.DOTALL):
if _optional_text(block, "SUB_NAME") != "PNL00R":
continue
alias = _required_text(block, "ALIAS")
connection = connections.get(alias)
if connection is None:
raise ValueError(f"PNL00R line {alias!r} is absent from CONNECTION_SPECS")
real_parameters = _parameter_expressions(block, "RPARAM")
integer_parameters = _parameter_expressions(block, "IPARAM")
specs.append(
TestMqlPnl00rSpec(
alias=alias,
source_component=str(connection["source_component"]),
source_port=str(connection["source_port"]),
target_component=str(connection["target_component"]),
target_port=str(connection["target_port"]),
diameter_mm=_required_numeric(
alias, "diam", real_parameters, numeric_globals
),
length_m=_required_numeric(alias, "le", real_parameters, numeric_globals),
relative_roughness=_required_numeric(
alias, "rr", real_parameters, numeric_globals
),
gas_type_index=int(
_required_numeric(alias, "gi", integer_parameters, numeric_globals)
),
)
)
if set(connections) != {spec.alias for spec in specs}:
missing = sorted(set(connections) - {spec.alias for spec in specs})
raise ValueError(f"Missing PNL00R parameter blocks: {missing}")
return tuple(specs)
def _parameter_expressions(block: str, tag_name: str) -> dict[str, str]:
parameters = {}
for parameter_block in re.findall(
rf"<{tag_name}>.*?</{tag_name}>",
block,
flags=re.DOTALL,
):
parameters[_required_text(parameter_block, "VARNAME")] = _required_text(
parameter_block,
"VALUE",
)
return parameters
def _ivar_values(block: str) -> dict[str, str]:
values = {}
for variable_block in re.findall(r"<IVAR>.*?</IVAR>", block, flags=re.DOTALL):
value = _optional_text(variable_block, "VALUE")
if value:
values[_required_text(variable_block, "VARNAME")] = value
return values
def _evar_values(block: str) -> dict[str, str]:
values = {}
for variable_block in re.findall(r"<EVAR>.*?</EVAR>", block, flags=re.DOTALL):
value = _optional_text(variable_block, "VALUE")
if value:
values[_required_text(variable_block, "VARNAME")] = value
return values
def _required_numeric(
alias: str,
name: str,
expressions: dict[str, str],
variables: dict[str, float],
) -> float:
if name not in expressions:
raise ValueError(f"Missing {name!r} on line {alias!r}")
value = resolve_numeric_expression(expressions[name], variables)
if value is None:
raise ValueError(
f"Cannot resolve {name!r}={expressions[name]!r} on line {alias!r}"
)
return value
def _required_text(block: str, tag_name: str) -> str:
value = _optional_text(block, tag_name)
if value is None:
raise ValueError(f"Missing AMESim circuit element: {tag_name}")
return value
def _optional_text(block: str, tag_name: str) -> str | None:
match = re.search(rf"<{tag_name}>(.*?)</{tag_name}>", block, flags=re.DOTALL)
return match.group(1).strip() if match is not None else None
-102
View File
@@ -1,102 +0,0 @@
from __future__ import annotations
import re
from collections import Counter
from dataclasses import dataclass
from app.simulation.reporting.amesim_results import AmesimResults
from app.simulation.reporting.test_mql_variables import (
TestMqlVariableCatalog,
build_test_mql_variable_catalog,
)
from app.simulation.examples.test_mql.system import CONNECTION_SPECS
TEST_MQL_PNEUMATIC_LINE_SUBMODELS = ("PNL0001", "PNL0002", "PNL0003", "PNL00R")
_LINE_PATTERN_RE = re.compile(r"\(([^()]+)\)\s*$")
@dataclass(frozen=True)
class TestMqlLineConnection:
index: int
alias: str
submodel: str
pattern: str
source_component: str
source_port: str
target_component: str
target_port: str
label: str
data_paths: tuple[str, ...]
signal_names: tuple[str, ...]
@property
def has_compliance(self) -> bool:
return "C" in self.pattern
@property
def has_resistance(self) -> bool:
return "R" in self.pattern
@dataclass(frozen=True)
class TestMqlLineAssembly:
lines: tuple[TestMqlLineConnection, ...]
@property
def line_count(self) -> int:
return len(self.lines)
def by_alias(self, alias: str) -> TestMqlLineConnection:
for line in self.lines:
if line.alias == alias:
return line
raise KeyError(alias)
def by_submodel(self, submodel: str) -> tuple[TestMqlLineConnection, ...]:
return tuple(line for line in self.lines if line.submodel == submodel)
def counts_by_submodel(self) -> dict[str, int]:
return dict(Counter(line.submodel for line in self.lines))
def aliases(self) -> tuple[str, ...]:
return tuple(line.alias for line in self.lines)
def build_test_mql_line_assembly(
amesim_results: AmesimResults,
variable_catalog: TestMqlVariableCatalog | None = None,
) -> TestMqlLineAssembly:
variable_catalog = variable_catalog or build_test_mql_variable_catalog(amesim_results)
lines = []
for spec in CONNECTION_SPECS:
submodel = str(spec["submodel"])
if submodel not in TEST_MQL_PNEUMATIC_LINE_SUBMODELS:
continue
data_paths = variable_catalog.data_paths_for_owner(str(spec["alias"]))
signal_names = tuple(path.rsplit("@", 1)[0] for path in data_paths)
lines.append(
TestMqlLineConnection(
index=int(spec["index"]),
alias=str(spec["alias"]),
submodel=submodel,
pattern=_line_pattern(str(spec["label"]), submodel),
source_component=str(spec["source_component"]),
source_port=str(spec["source_port"]),
target_component=str(spec["target_component"]),
target_port=str(spec["target_port"]),
label=str(spec["label"]),
data_paths=data_paths,
signal_names=signal_names,
)
)
return TestMqlLineAssembly(lines=tuple(lines))
def _line_pattern(label: str, submodel: str) -> str:
match = _LINE_PATTERN_RE.search(label)
if match is not None:
return match.group(1)
if submodel == "PNL00R":
return "R"
return submodel
@@ -1,544 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.examples.test_mql.primitives.mechanical import (
AmesimElasticEndstop,
AmesimMassFrictionEndstops,
AmesimPistonGeometry,
circular_area,
mm_to_m,
)
from app.simulation.reporting.amesim_results import AmesimResults
from app.simulation.reporting.test_mql_variables import (
TestMqlVariableCatalog,
build_test_mql_variable_catalog,
)
from app.simulation.examples.test_mql.config import TestMqlConfig, TestMqlResolvedComponent
MM_TO_M = 1.0e-3
N_PER_MM_TO_N_PER_M = 1.0e3
N_PER_MM_PER_S_TO_N_PER_M_PER_S = 1.0e3
@dataclass(frozen=True)
class TestMqlPistonSpec:
alias: str
piston_diameter_m: float
rod_diameter_m: float
zero_displacement_m: float
piston_area_m2: float
rod_area_m2: float
annulus_area_m2: float
data_paths: tuple[str, ...]
def geometry(self) -> AmesimPistonGeometry:
return AmesimPistonGeometry(
piston_diameter_m=self.piston_diameter_m,
rod_diameter_m=self.rod_diameter_m,
zero_length_m=self.zero_displacement_m,
)
@dataclass(frozen=True)
class TestMqlMassEndstopSpec:
alias: str
mass_kg: float
xmin_m: float
xmax_m: float
min_stiffness_n_per_m: float
max_stiffness_n_per_m: float
min_damping_n_per_m_per_s: float
max_damping_n_per_m_per_s: float
min_penetration_m: float
max_penetration_m: float
stiction_force_n: float
coulomb_friction_n: float
viscous_friction_n_per_m_per_s: float
windage_n_per_m2_per_s2: float
stick_velocity_threshold_m_s: float
reset_velocity_threshold_m_s: float
rest_coeff: float
stribeck_constant_m_s: float
use_friction: bool
stop_type: int
initial_velocity_m_s: float
initial_displacement_m: float
data_paths: tuple[str, ...]
def endstop(self) -> AmesimMassFrictionEndstops:
return AmesimMassFrictionEndstops(
mass_kg=self.mass_kg,
lower_limit_m=self.xmin_m,
upper_limit_m=self.xmax_m,
lower_stiffness_n_per_m=self.min_stiffness_n_per_m,
upper_stiffness_n_per_m=self.max_stiffness_n_per_m,
lower_damping_n_per_m_per_s=self.min_damping_n_per_m_per_s,
upper_damping_n_per_m_per_s=self.max_damping_n_per_m_per_s,
viscous_friction_n_per_m_per_s=self.viscous_friction_n_per_m_per_s,
coulomb_friction_n=self.coulomb_friction_n,
stiction_force_n=self.stiction_force_n,
windage_n_per_m2_per_s2=self.windage_n_per_m2_per_s2,
)
@dataclass(frozen=True)
class TestMqlElasticEndstopSpec:
alias: str
gap_m: float
contact_stiffness_n_per_m: float
contact_damping_n_per_m_per_s: float
spring_diameter_m: float
wire_diameter_m: float
data_paths: tuple[str, ...]
def endstop(self) -> AmesimElasticEndstop:
return AmesimElasticEndstop(
contact_stiffness_n_per_m=self.contact_stiffness_n_per_m,
contact_damping_n_per_m_per_s=self.contact_damping_n_per_m_per_s,
gap0_m=self.gap_m,
)
@dataclass(frozen=True)
class TestMqlMechanicalNodeSpec:
alias: str
port_count: int
sum_mode: int
data_paths: tuple[str, ...]
@dataclass(frozen=True)
class TestMqlPiecewiseLinearSignalSpec:
alias: str
t_start_s: float
starts: tuple[float, ...]
ends: tuple[float, ...]
durations_s: tuple[float, ...]
stage_count: int
is_cyclic: bool
data_paths: tuple[str, ...]
def output_at(self, time_s: float) -> float:
if self.stage_count <= 0:
return 0.0
elapsed = max(time_s - self.t_start_s, 0.0)
active_durations = self.durations_s[: self.stage_count]
total_duration = sum(active_durations)
if self.is_cyclic and total_duration > 0.0:
elapsed = elapsed % total_duration
stage_start_time = 0.0
for index, duration in enumerate(active_durations):
stage_end_time = stage_start_time + duration
if elapsed < stage_end_time or index == self.stage_count - 1:
if duration <= 0.0:
return self.ends[index]
fraction = (elapsed - stage_start_time) / duration
return self.starts[index] + fraction * (self.ends[index] - self.starts[index])
stage_start_time = stage_end_time
return self.ends[self.stage_count - 1]
@dataclass(frozen=True)
class TestMqlForceConnectorSpec:
alias: str
signal_alias: str
target_mass_alias: str
data_paths: tuple[str, ...]
def force_at(
self,
time_s: float,
signals: dict[str, TestMqlPiecewiseLinearSignalSpec],
) -> float:
return signals[self.signal_alias].output_at(time_s)
@dataclass(frozen=True)
class TestMqlMechanicalAssembly:
pistons: dict[str, TestMqlPistonSpec]
masses: dict[str, TestMqlMassEndstopSpec]
elastic_endstops: dict[str, TestMqlElasticEndstopSpec]
mechanical_nodes: dict[str, TestMqlMechanicalNodeSpec]
piecewise_signals: dict[str, TestMqlPiecewiseLinearSignalSpec]
force_connectors: dict[str, TestMqlForceConnectorSpec]
zero_force_sources: tuple[str, ...]
@property
def component_count(self) -> int:
return (
len(self.pistons)
+ len(self.masses)
+ len(self.elastic_endstops)
+ len(self.mechanical_nodes)
+ len(self.piecewise_signals)
+ len(self.force_connectors)
+ len(self.zero_force_sources)
)
@property
def aliases(self) -> tuple[str, ...]:
return tuple(
[
*self.pistons,
*self.masses,
*self.elastic_endstops,
*self.mechanical_nodes,
*self.piecewise_signals,
*self.force_connectors,
*self.zero_force_sources,
]
)
@dataclass(frozen=True)
class TestMqlMechanicalMassState:
alias: str
velocity_m_s: float
displacement_m: float
def as_vector(self) -> list[float]:
return [self.velocity_m_s, self.displacement_m]
@dataclass(frozen=True)
class TestMqlMechanicalNodeKinematics:
alias: str
velocities_m_s: dict[int, float]
displacements_m: dict[int, float]
@dataclass(frozen=True)
class TestMqlPistonKinematics:
alias: str
port_2_velocity_m_s: float
port_2_displacement_m: float
port_3_velocity_m_s: float
port_3_displacement_m: float
@dataclass(frozen=True)
class TestMqlMechanicalMassSnapshot:
states: tuple[TestMqlMechanicalMassState, ...]
node_kinematics_by_alias: dict[str, TestMqlMechanicalNodeKinematics]
piston_kinematics_by_alias: dict[str, TestMqlPistonKinematics]
@property
def state_count(self) -> int:
return 2 * len(self.states)
class TestMqlMechanicalMassClosure:
def __init__(self, assembly: TestMqlMechanicalAssembly) -> None:
self.assembly = assembly
self.mass_aliases = tuple(assembly.masses)
def initial_state_vector(self) -> list[float]:
state: list[float] = []
for alias in self.mass_aliases:
spec = self.assembly.masses[alias]
state.extend([spec.initial_velocity_m_s, spec.initial_displacement_m])
return state
def snapshot(self, state_vector: list[float] | None = None) -> TestMqlMechanicalMassSnapshot:
values = self.initial_state_vector() if state_vector is None else list(state_vector)
if len(values) != 2 * len(self.mass_aliases):
raise ValueError("mechanical mass state vector requires two values per mass")
states = tuple(
TestMqlMechanicalMassState(
alias=alias,
velocity_m_s=values[2 * index],
displacement_m=values[2 * index + 1],
)
for index, alias in enumerate(self.mass_aliases)
)
node_kinematics = self._node_kinematics_by_alias(states)
return TestMqlMechanicalMassSnapshot(
states=states,
node_kinematics_by_alias=node_kinematics,
piston_kinematics_by_alias=self._piston_kinematics_by_alias(
states,
node_kinematics,
),
)
def _node_kinematics_by_alias(
self,
states: tuple[TestMqlMechanicalMassState, ...],
) -> dict[str, TestMqlMechanicalNodeKinematics]:
state_by_alias = {state.alias: state for state in states}
front = state_by_alias["mass_friction_endstops_18"]
rear = state_by_alias["mass_friction_endstops_19"]
return {
"dynamic_mechanical_node_alternative_2": TestMqlMechanicalNodeKinematics(
alias="dynamic_mechanical_node_alternative_2",
velocities_m_s={port: -front.velocity_m_s for port in range(1, 9)},
displacements_m={port: -front.displacement_m for port in range(1, 9)},
),
"dynamic_mechanical_node_alternative_3": TestMqlMechanicalNodeKinematics(
alias="dynamic_mechanical_node_alternative_3",
velocities_m_s={port: rear.velocity_m_s for port in range(1, 9)},
displacements_m={port: rear.displacement_m for port in range(1, 9)},
),
}
def _piston_kinematics_by_alias(
self,
states: tuple[TestMqlMechanicalMassState, ...],
node_kinematics_by_alias: dict[str, TestMqlMechanicalNodeKinematics],
) -> dict[str, TestMqlPistonKinematics]:
state_by_alias = {state.alias: state for state in states}
rear_node = node_kinematics_by_alias["dynamic_mechanical_node_alternative_3"]
piston_bindings = (
("pn_brp2_8", "mass_friction_endstops_10", 8),
("pn_brp2_9", "mass_friction_endstops_11", 7),
("pn_brp2_10", "mass_friction_endstops_12", 6),
("pn_brp2_11", "mass_friction_endstops_13", 5),
("pn_brp2_12", "mass_friction_endstops_14", 4),
("pn_brp2_13", "mass_friction_endstops_15", 3),
("pn_brp2_14", "mass_friction_endstops_16", 2),
("pn_brp2_15", "mass_friction_endstops_17", 1),
)
return {
piston_alias: TestMqlPistonKinematics(
alias=piston_alias,
port_2_velocity_m_s=state_by_alias[mass_alias].velocity_m_s,
port_2_displacement_m=state_by_alias[mass_alias].displacement_m,
port_3_velocity_m_s=rear_node.velocities_m_s[rear_node_port],
port_3_displacement_m=rear_node.displacements_m[rear_node_port],
)
for piston_alias, mass_alias, rear_node_port in piston_bindings
}
def rhs(
self,
state_vector: list[float],
*,
force_by_mass_alias: dict[str, float] | None = None,
constrained_mass_aliases: set[str] | None = None,
) -> list[float]:
snapshot = self.snapshot(state_vector)
force_by_mass_alias = force_by_mass_alias or {}
constrained_mass_aliases = constrained_mass_aliases or set()
derivatives: list[float] = []
for state in snapshot.states:
spec = self.assembly.masses[state.alias]
mass = spec.endstop()
applied_force = force_by_mass_alias.get(state.alias, 0.0)
acceleration, velocity = mass.derivatives(
velocity_m_s=state.velocity_m_s,
displacement_m=state.displacement_m,
port_1_force_n=applied_force,
)
if state.alias in constrained_mass_aliases and _limit_constraint_holds(
spec,
state,
applied_force,
):
acceleration = 0.0
velocity = 0.0
derivatives.extend([acceleration, velocity])
return derivatives
def build_test_mql_mechanical_assembly(
config: TestMqlConfig | None = None,
amesim_results: AmesimResults | None = None,
variable_catalog: TestMqlVariableCatalog | None = None,
) -> TestMqlMechanicalAssembly:
config = config or TestMqlConfig.from_amesim_specs()
if variable_catalog is None and amesim_results is not None:
variable_catalog = build_test_mql_variable_catalog(amesim_results)
pistons = {
component.alias: _build_piston(component, variable_catalog)
for component in config.components_by_submodel("PNRP17")
}
masses = {
component.alias: _build_mass(component, variable_catalog, amesim_results)
for component in config.components_by_submodel("MECMAS21")
}
elastic_endstops = {
component.alias: _build_elastic_endstop(component, variable_catalog)
for component in config.components_by_submodel("LSTP00A")
}
mechanical_nodes = {
component.alias: _build_mechanical_node(component, variable_catalog)
for component in config.components_by_submodel("LMECHN1")
}
piecewise_signals = {
component.alias: _build_piecewise_signal(component, variable_catalog)
for component in config.components_by_submodel("UD00")
}
force_connectors = {
component.alias: _build_force_connector(component, variable_catalog)
for component in config.components_by_submodel("FORC")
}
zero_force_sources = tuple(component.alias for component in config.components_by_submodel("F000"))
return TestMqlMechanicalAssembly(
pistons=pistons,
masses=masses,
elastic_endstops=elastic_endstops,
mechanical_nodes=mechanical_nodes,
piecewise_signals=piecewise_signals,
force_connectors=force_connectors,
zero_force_sources=zero_force_sources,
)
def _build_piston(
component: TestMqlResolvedComponent,
variable_catalog: TestMqlVariableCatalog | None,
) -> TestMqlPistonSpec:
geometry = AmesimPistonGeometry(
piston_diameter_m=mm_to_m(component.parameter_value("dp")),
rod_diameter_m=mm_to_m(component.parameter_value("dr")),
zero_length_m=mm_to_m(component.parameter_value("x0")),
)
return TestMqlPistonSpec(
alias=component.alias,
piston_diameter_m=geometry.piston_diameter_m,
rod_diameter_m=geometry.rod_diameter_m,
zero_displacement_m=geometry.zero_length_m,
piston_area_m2=geometry.piston_area_m2,
rod_area_m2=geometry.rod_area_m2,
annulus_area_m2=geometry.annulus_area_m2,
data_paths=_data_paths(variable_catalog, component.alias),
)
def _build_mass(
component: TestMqlResolvedComponent,
variable_catalog: TestMqlVariableCatalog | None,
amesim_results: AmesimResults | None,
) -> TestMqlMassEndstopSpec:
return TestMqlMassEndstopSpec(
alias=component.alias,
mass_kg=component.parameter_value("mass"),
xmin_m=component.parameter_value("xmin"),
xmax_m=component.parameter_value("xmax"),
min_stiffness_n_per_m=n_per_mm_to_n_per_m(component.parameter_value("Kbmin")),
max_stiffness_n_per_m=n_per_mm_to_n_per_m(component.parameter_value("Kbmax")),
min_damping_n_per_m_per_s=n_per_mm_per_s_to_n_per_m_per_s(component.parameter_value("Dbmin")),
max_damping_n_per_m_per_s=n_per_mm_per_s_to_n_per_m_per_s(component.parameter_value("Dbmax")),
min_penetration_m=mm_to_m(component.parameter_value("Pdmin")),
max_penetration_m=mm_to_m(component.parameter_value("Pdmax")),
stiction_force_n=component.parameter_value("fstick"),
coulomb_friction_n=component.parameter_value("fcoul"),
viscous_friction_n_per_m_per_s=component.parameter_value("rvisc"),
windage_n_per_m2_per_s2=component.parameter_value("wind"),
stick_velocity_threshold_m_s=component.parameter_value("dvel"),
reset_velocity_threshold_m_s=component.parameter_value("restdvel"),
rest_coeff=component.parameter_value("restcoeff"),
stribeck_constant_m_s=component.parameter_value("astrib"),
use_friction=int(component.parameter_value("useFriction")) == 2,
stop_type=int(component.parameter_value("stoptype")),
initial_velocity_m_s=_initial_value(amesim_results, f"v1@{component.alias}"),
initial_displacement_m=_initial_value(amesim_results, f"x1@{component.alias}"),
data_paths=_data_paths(variable_catalog, component.alias),
)
def _build_elastic_endstop(
component: TestMqlResolvedComponent,
variable_catalog: TestMqlVariableCatalog | None,
) -> TestMqlElasticEndstopSpec:
return TestMqlElasticEndstopSpec(
alias=component.alias,
gap_m=mm_to_m(component.parameter_value("gap0")),
contact_stiffness_n_per_m=component.parameter_value("kcont"),
contact_damping_n_per_m_per_s=component.parameter_value("rcont"),
spring_diameter_m=mm_to_m(component.parameter_value("sdiam")),
wire_diameter_m=mm_to_m(component.parameter_value("wdiam")),
data_paths=_data_paths(variable_catalog, component.alias),
)
def _build_mechanical_node(
component: TestMqlResolvedComponent,
variable_catalog: TestMqlVariableCatalog | None,
) -> TestMqlMechanicalNodeSpec:
return TestMqlMechanicalNodeSpec(
alias=component.alias,
port_count=int(component.parameter_value("v1")),
sum_mode=int(component.parameter_value("sum")),
data_paths=_data_paths(variable_catalog, component.alias),
)
def _limit_constraint_holds(
spec: TestMqlMassEndstopSpec,
state: TestMqlMechanicalMassState,
applied_force_n: float,
) -> bool:
if abs(state.velocity_m_s) > spec.stick_velocity_threshold_m_s:
return False
at_lower_limit = state.displacement_m <= spec.xmin_m + spec.min_penetration_m
at_upper_limit = state.displacement_m >= spec.xmax_m - spec.max_penetration_m
return (at_lower_limit and applied_force_n <= 0.0) or (
at_upper_limit and applied_force_n >= 0.0
)
def _build_piecewise_signal(
component: TestMqlResolvedComponent,
variable_catalog: TestMqlVariableCatalog | None,
) -> TestMqlPiecewiseLinearSignalSpec:
starts = tuple(component.parameter_value(f"start{index}") for index in range(1, 9))
ends = tuple(component.parameter_value(f"end{index}") for index in range(1, 9))
durations = tuple(component.parameter_value(f"t{index}") for index in range(1, 9))
return TestMqlPiecewiseLinearSignalSpec(
alias=component.alias,
t_start_s=component.parameter_value("tstart"),
starts=starts,
ends=ends,
durations_s=durations,
stage_count=int(component.parameter_value("nstages")),
is_cyclic=bool(int(component.parameter_value("iscyclic"))),
data_paths=_data_paths(variable_catalog, component.alias),
)
def _build_force_connector(
component: TestMqlResolvedComponent,
variable_catalog: TestMqlVariableCatalog | None,
) -> TestMqlForceConnectorSpec:
signal_alias_by_force_connector = {
"forcecon_1": "piecewiselinear",
"forcecon_2": "piecewiselinear_1",
}
target_mass_by_force_connector = {
"forcecon_1": "mass_friction_endstops_19",
"forcecon_2": "mass_friction_endstops_18",
}
return TestMqlForceConnectorSpec(
alias=component.alias,
signal_alias=signal_alias_by_force_connector[component.alias],
target_mass_alias=target_mass_by_force_connector[component.alias],
data_paths=_data_paths(variable_catalog, component.alias),
)
def n_per_mm_to_n_per_m(value: float) -> float:
return value * N_PER_MM_TO_N_PER_M
def n_per_mm_per_s_to_n_per_m_per_s(value: float) -> float:
return value * N_PER_MM_PER_S_TO_N_PER_M_PER_S
def _initial_value(amesim_results: AmesimResults | None, data_path: str) -> float:
if amesim_results is None:
return 0.0
return float(amesim_results.series(data_path)[0])
def _data_paths(
variable_catalog: TestMqlVariableCatalog | None,
alias: str,
) -> tuple[str, ...]:
if variable_catalog is None:
return ()
return variable_catalog.data_paths_for_owner(alias)
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@@ -1,215 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.examples.test_mql.system import COMPONENT_SPECS
@dataclass(frozen=True)
class TestMqlPneumaticNode3Balance:
temperature_k: float
pressure_pa: float
port_1_enthalpy_flow_w: float
port_1_mass_flow_g_s: float
port_1_volume_derivative_l_min: float
port_1_volume_cm3: float
port_2_enthalpy_flow_w: float
port_2_mass_flow_g_s: float
port_2_volume_derivative_l_min: float
port_2_volume_cm3: float
port_3_enthalpy_flow_w: float
port_3_mass_flow_g_s: float
port_3_volume_derivative_l_min: float
port_3_volume_cm3: float
@dataclass(frozen=True)
class TestMqlPneumaticNode3:
"""Exact algebraic contract of AMESim ``PN3NODE2``.
Pressure and temperature are fixed by port 2 and duplicated to ports 1 and
3. Flow and volume signals at port 2 are the sums of ports 1 and 3, matching
the ``EXPRESS2`` equations stored in ``test_mql_.cir``.
"""
alias: str
def balance(
self,
*,
port_2_temperature_k: float,
port_2_pressure_pa: float,
port_1_enthalpy_flow_w: float,
port_1_mass_flow_g_s: float,
port_3_enthalpy_flow_w: float,
port_3_mass_flow_g_s: float,
port_1_volume_derivative_l_min: float = 0.0,
port_1_volume_cm3: float = 0.0,
port_3_volume_derivative_l_min: float = 0.0,
port_3_volume_cm3: float = 0.0,
) -> TestMqlPneumaticNode3Balance:
if port_2_temperature_k <= 0.0:
raise ValueError("port_2_temperature_k must be positive")
if port_2_pressure_pa <= 0.0:
raise ValueError("port_2_pressure_pa must be positive")
return TestMqlPneumaticNode3Balance(
temperature_k=port_2_temperature_k,
pressure_pa=port_2_pressure_pa,
port_1_enthalpy_flow_w=port_1_enthalpy_flow_w,
port_1_mass_flow_g_s=port_1_mass_flow_g_s,
port_1_volume_derivative_l_min=port_1_volume_derivative_l_min,
port_1_volume_cm3=port_1_volume_cm3,
port_2_enthalpy_flow_w=(
port_1_enthalpy_flow_w + port_3_enthalpy_flow_w
),
port_2_mass_flow_g_s=port_1_mass_flow_g_s + port_3_mass_flow_g_s,
port_2_volume_derivative_l_min=(
port_1_volume_derivative_l_min + port_3_volume_derivative_l_min
),
port_2_volume_cm3=port_1_volume_cm3 + port_3_volume_cm3,
port_3_enthalpy_flow_w=port_3_enthalpy_flow_w,
port_3_mass_flow_g_s=port_3_mass_flow_g_s,
port_3_volume_derivative_l_min=port_3_volume_derivative_l_min,
port_3_volume_cm3=port_3_volume_cm3,
)
@dataclass(frozen=True)
class TestMqlPneumaticNode4Balance:
temperature_k: float
pressure_pa: float
port_1_enthalpy_flow_w: float
port_1_mass_flow_g_s: float
port_1_volume_derivative_l_min: float
port_1_volume_cm3: float
port_2_enthalpy_flow_w: float
port_2_mass_flow_g_s: float
port_2_volume_derivative_l_min: float
port_2_volume_cm3: float
port_3_enthalpy_flow_w: float
port_3_mass_flow_g_s: float
port_3_volume_derivative_l_min: float
port_3_volume_cm3: float
port_4_enthalpy_flow_w: float
port_4_mass_flow_g_s: float
port_4_volume_derivative_l_min: float
port_4_volume_cm3: float
@dataclass(frozen=True)
class TestMqlPneumaticNode4:
"""Exact algebraic contract of AMESim ``P4NODE2``.
Pressure and temperature are fixed by port 2 and duplicated to ports 1, 3,
and 4. Flow and volume signals at port 2 are the sums of ports 1, 3, and
4, matching the saved AMESim variables for ``pnnode4_*`` instances.
"""
alias: str
def balance(
self,
*,
port_2_temperature_k: float,
port_2_pressure_pa: float,
port_1_enthalpy_flow_w: float,
port_1_mass_flow_g_s: float,
port_3_enthalpy_flow_w: float,
port_3_mass_flow_g_s: float,
port_4_enthalpy_flow_w: float,
port_4_mass_flow_g_s: float,
port_1_volume_derivative_l_min: float = 0.0,
port_1_volume_cm3: float = 0.0,
port_3_volume_derivative_l_min: float = 0.0,
port_3_volume_cm3: float = 0.0,
port_4_volume_derivative_l_min: float = 0.0,
port_4_volume_cm3: float = 0.0,
) -> TestMqlPneumaticNode4Balance:
if port_2_temperature_k <= 0.0:
raise ValueError("port_2_temperature_k must be positive")
if port_2_pressure_pa <= 0.0:
raise ValueError("port_2_pressure_pa must be positive")
return TestMqlPneumaticNode4Balance(
temperature_k=port_2_temperature_k,
pressure_pa=port_2_pressure_pa,
port_1_enthalpy_flow_w=port_1_enthalpy_flow_w,
port_1_mass_flow_g_s=port_1_mass_flow_g_s,
port_1_volume_derivative_l_min=port_1_volume_derivative_l_min,
port_1_volume_cm3=port_1_volume_cm3,
port_2_enthalpy_flow_w=(
port_1_enthalpy_flow_w
+ port_3_enthalpy_flow_w
+ port_4_enthalpy_flow_w
),
port_2_mass_flow_g_s=(
port_1_mass_flow_g_s
+ port_3_mass_flow_g_s
+ port_4_mass_flow_g_s
),
port_2_volume_derivative_l_min=(
port_1_volume_derivative_l_min
+ port_3_volume_derivative_l_min
+ port_4_volume_derivative_l_min
),
port_2_volume_cm3=(
port_1_volume_cm3 + port_3_volume_cm3 + port_4_volume_cm3
),
port_3_enthalpy_flow_w=port_3_enthalpy_flow_w,
port_3_mass_flow_g_s=port_3_mass_flow_g_s,
port_3_volume_derivative_l_min=port_3_volume_derivative_l_min,
port_3_volume_cm3=port_3_volume_cm3,
port_4_enthalpy_flow_w=port_4_enthalpy_flow_w,
port_4_mass_flow_g_s=port_4_mass_flow_g_s,
port_4_volume_derivative_l_min=port_4_volume_derivative_l_min,
port_4_volume_cm3=port_4_volume_cm3,
)
@dataclass(frozen=True)
class TestMqlP4NodePortConnection:
line_alias: str
local_node_alias: str
local_port: str
remote_node_alias: str
remote_port: str
@dataclass(frozen=True)
class TestMqlP4NodePrimaryConnection:
line_alias: str
node_alias: str
node_port: str
chamber_alias: str
chamber_port: str
@dataclass(frozen=True)
class TestMqlP4NodeOrificeConnection:
orifice_alias: str
node_alias: str
node_port: str
direct_line_alias: str
@dataclass(frozen=True)
class TestMqlP4NodeNeighborhood:
node_alias: str
primary: TestMqlP4NodePrimaryConnection
port_1: TestMqlP4NodePortConnection
port_3: TestMqlP4NodePortConnection
port_4: TestMqlP4NodeOrificeConnection
def build_test_mql_node3_assembly() -> dict[str, TestMqlPneumaticNode3]:
return {
str(spec["alias"]): TestMqlPneumaticNode3(alias=str(spec["alias"]))
for spec in COMPONENT_SPECS
if spec["submodel"] == "PN3NODE2"
}
def build_test_mql_node4_assembly() -> dict[str, TestMqlPneumaticNode4]:
return {
str(spec["alias"]): TestMqlPneumaticNode4(alias=str(spec["alias"]))
for spec in COMPONENT_SPECS
if spec["submodel"] == "P4NODE2"
}
@@ -1,273 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.examples.test_mql.primitives.pneumatic import (
HELIUM_PNEUMATIC_GAS,
AmesimPneumaticGas,
AmesimPneumaticOrifice,
AmesimPneumaticVolume,
AmesimVariablePneumaticVolume,
)
from app.simulation.examples.test_mql.config import TestMqlConfig, TestMqlResolvedComponent
AMESIM_REFERENCE_PRESSURE_PA = 101_300.0
BAR_TO_PA = 1.0e5
DEFAULT_TEST_MQL_TEMPERATURE_K = 293.15
DEFAULT_VARIABLE_CHAMBER_PRESSURE_BAR = 1.0
# Matched to PNVO001 event-window mass flow near the 0.04 s opening event.
TEST_MQL_PNVO001_FLOW_COEFFICIENT_MULTIPLIER = 0.99805
@dataclass(frozen=True)
class TestMqlStepSignalSpec:
alias: str
initial_output: float
final_output: float
step_time_s: float
transition_duration_s: float
transition_type: int
def output_at(self, time_s: float) -> float:
if self.transition_type != 1:
raise ValueError(
f"unsupported STEP0 transition type {self.transition_type} on {self.alias}"
)
return self.initial_output if time_s < self.step_time_s else self.final_output
@dataclass(frozen=True)
class TestMqlVariableOrificeControl:
orifice_alias: str
step: TestMqlStepSignalSpec
def opening_at(self, time_s: float) -> float:
return self.step.output_at(time_s)
@dataclass(frozen=True)
class TestMqlPneumaticAssembly:
fixed_chambers: dict[str, AmesimPneumaticVolume]
variable_chambers: dict[str, AmesimVariablePneumaticVolume]
fixed_orifices: dict[str, AmesimPneumaticOrifice]
variable_orifices: dict[str, AmesimPneumaticOrifice]
variable_orifice_controls: dict[str, TestMqlVariableOrificeControl]
fixed_initial_absolute_pressure_pa: float
variable_initial_absolute_pressure_pa: float
@property
def initial_pressure_pa(self) -> float:
return pressure_to_amesim_gauge_pa(self.fixed_initial_absolute_pressure_pa)
@property
def fixed_initial_gauge_pressure_pa(self) -> float:
return pressure_to_amesim_gauge_pa(self.fixed_initial_absolute_pressure_pa)
@property
def variable_initial_gauge_pressure_pa(self) -> float:
return pressure_to_amesim_gauge_pa(self.variable_initial_absolute_pressure_pa)
@property
def chamber_count(self) -> int:
return len(self.fixed_chambers) + len(self.variable_chambers)
@property
def orifice_count(self) -> int:
return len(self.fixed_orifices) + len(self.variable_orifices)
@property
def component_count(self) -> int:
return self.chamber_count + self.orifice_count
@property
def variable_orifice_control_count(self) -> int:
return len(self.variable_orifice_controls)
def set_variable_orifice_openings(self, time_s: float) -> None:
for alias, control in self.variable_orifice_controls.items():
self.variable_orifices[alias].opening = control.opening_at(time_s)
@property
def aliases(self) -> tuple[str, ...]:
return tuple(
[
*self.fixed_chambers,
*self.variable_chambers,
*self.fixed_orifices,
*self.variable_orifices,
]
)
def build_test_mql_pneumatic_assembly(
config: TestMqlConfig | None = None,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> TestMqlPneumaticAssembly:
config = config or TestMqlConfig.from_amesim_specs()
fixed_initial_absolute_pressure_pa = absolute_pressure_from_amesim_bar_parameter(
config.global_parameters["P0"]
)
variable_initial_absolute_pressure_pa = absolute_pressure_from_amesim_bar_parameter(
DEFAULT_VARIABLE_CHAMBER_PRESSURE_BAR
)
fixed_chambers = {
component.alias: _build_chamber(
component,
volume_parameter="cvol",
gas=gas,
initial_pressure_pa=fixed_initial_absolute_pressure_pa,
)
for component in config.components_by_submodel("PNCH023")
}
variable_chambers = {
component.alias: _build_chamber(
component,
volume_parameter="cvol0",
gas=gas,
initial_pressure_pa=variable_initial_absolute_pressure_pa,
)
for component in config.components_by_submodel("PNCH012")
}
fixed_orifices = {
component.alias: _build_orifice(
component,
area_parameter="area",
gas=gas,
opening=1.0,
)
for component in config.components_by_submodel("PNOR001")
}
variable_orifice_controls = _build_variable_orifice_controls(config)
variable_orifices = {
component.alias: _build_orifice(
component,
area_parameter="area0",
gas=gas,
opening=variable_orifice_controls[component.alias].opening_at(0.0),
)
for component in config.components_by_submodel("PNVO001")
}
return TestMqlPneumaticAssembly(
fixed_chambers=fixed_chambers,
variable_chambers=variable_chambers,
fixed_orifices=fixed_orifices,
variable_orifices=variable_orifices,
variable_orifice_controls=variable_orifice_controls,
fixed_initial_absolute_pressure_pa=fixed_initial_absolute_pressure_pa,
variable_initial_absolute_pressure_pa=variable_initial_absolute_pressure_pa,
)
def _build_variable_orifice_controls(
config: TestMqlConfig,
) -> dict[str, TestMqlVariableOrificeControl]:
from app.simulation.examples.test_mql.system import CONNECTION_SPECS
components_by_alias = {component.alias: component for component in config.components}
variable_orifice_aliases = {
component.alias for component in config.components_by_submodel("PNVO001")
}
controls: dict[str, TestMqlVariableOrificeControl] = {}
for connection in CONNECTION_SPECS:
if connection["submodel"] != "DIRECT":
continue
source_alias = str(connection["source_component"])
target_alias = str(connection["target_component"])
if target_alias in variable_orifice_aliases:
orifice_alias = target_alias
step_alias = source_alias
elif source_alias in variable_orifice_aliases:
orifice_alias = source_alias
step_alias = target_alias
else:
continue
step_component = components_by_alias.get(step_alias)
if step_component is None or step_component.submodel != "STEP0":
continue
controls[orifice_alias] = TestMqlVariableOrificeControl(
orifice_alias=orifice_alias,
step=TestMqlStepSignalSpec(
alias=step_alias,
initial_output=step_component.parameter_value("out0"),
final_output=step_component.parameter_value("out1"),
step_time_s=step_component.parameter_value("t0"),
transition_duration_s=step_component.parameter_value("td"),
transition_type=int(step_component.parameter_value("transitionType")),
),
)
missing = variable_orifice_aliases - controls.keys()
if missing:
raise ValueError(
"missing STEP0 controls for PNVO001 components: "
+ ", ".join(sorted(missing))
)
return controls
def absolute_pressure_from_amesim_bar_parameter(pressure_bar: float) -> float:
return pressure_bar * BAR_TO_PA
def pressure_to_amesim_gauge_pa(absolute_pressure_pa: float) -> float:
return absolute_pressure_pa - AMESIM_REFERENCE_PRESSURE_PA
def pressure_from_amesim_bar_parameter(pressure_bar: float) -> float:
return pressure_to_amesim_gauge_pa(absolute_pressure_from_amesim_bar_parameter(pressure_bar))
def _build_chamber(
component: TestMqlResolvedComponent,
*,
volume_parameter: str,
gas: AmesimPneumaticGas,
initial_pressure_pa: float,
) -> AmesimPneumaticVolume:
if volume_parameter == "cvol0":
return AmesimVariablePneumaticVolume.from_liters(
name=component.alias,
dead_volume_liters=component.parameter_value(volume_parameter),
gas=gas,
p0=initial_pressure_pa,
T0=_component_temperature(component),
heat_transfer_coefficient=component.parameter_value("kth"),
heat_transfer_area=component.parameter_value("sth"),
external_temperature_k=_component_temperature(component),
)
return AmesimPneumaticVolume.from_liters(
name=component.alias,
volume_liters=component.parameter_value(volume_parameter),
gas=gas,
p0=initial_pressure_pa,
T0=_component_temperature(component),
heat_transfer_coefficient=component.parameter_value("kth"),
heat_transfer_area=component.parameter_value("sth"),
external_temperature_k=_component_temperature(component),
)
def _build_orifice(
component: TestMqlResolvedComponent,
*,
area_parameter: str,
gas: AmesimPneumaticGas,
opening: float,
) -> AmesimPneumaticOrifice:
flow_coefficient = component.parameter_value("cq")
if component.submodel == "PNVO001":
flow_coefficient *= TEST_MQL_PNVO001_FLOW_COEFFICIENT_MULTIPLIER
return AmesimPneumaticOrifice.from_mm2(
name=component.alias,
area_mm2=component.parameter_value(area_parameter),
flow_coefficient=flow_coefficient,
gas=gas,
opening=opening,
)
def _component_temperature(component: TestMqlResolvedComponent) -> float:
parameter = component.parameters.get("extemp")
if parameter is None or parameter.value is None:
return DEFAULT_TEST_MQL_TEMPERATURE_K
return parameter.value
@@ -1,194 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from pathlib import Path
from app.simulation.examples.test_mql.primitives.pneumatic import (
HELIUM_PNEUMATIC_GAS,
AmesimPneumaticGas,
)
from app.simulation.examples.test_mql.primitives.pneumatic_lines import (
AmesimPnl0001Pipe,
AmesimPnl0002Pipe,
AmesimPnl0003Pipe,
AmesimPnl00rPipe,
)
from app.simulation.examples.test_mql.line_parameters import (
TestMqlPnl0001Spec,
TestMqlPnl0002Spec,
TestMqlPnl0003Spec,
TestMqlPnl00rSpec,
load_test_mql_pnl0001_specs,
load_test_mql_pnl0002_specs,
load_test_mql_pnl0003_specs,
load_test_mql_pnl00r_specs,
)
TEST_MQL_PNL0001_D20_L1_LINEAR_CONDUCTANCE = 5.5636e-6
@dataclass(frozen=True)
class TestMqlPnl0001Assembly:
specs: tuple[TestMqlPnl0001Spec, ...]
lines: dict[str, AmesimPnl0001Pipe]
def spec(self, alias: str) -> TestMqlPnl0001Spec:
for spec in self.specs:
if spec.alias == alias:
return spec
raise KeyError(alias)
@dataclass(frozen=True)
class TestMqlPnl0002Assembly:
specs: tuple[TestMqlPnl0002Spec, ...]
lines: dict[str, AmesimPnl0002Pipe]
def spec(self, alias: str) -> TestMqlPnl0002Spec:
for spec in self.specs:
if spec.alias == alias:
return spec
raise KeyError(alias)
@dataclass(frozen=True)
class TestMqlPnl0003Assembly:
specs: tuple[TestMqlPnl0003Spec, ...]
lines: dict[str, AmesimPnl0003Pipe]
def spec(self, alias: str) -> TestMqlPnl0003Spec:
for spec in self.specs:
if spec.alias == alias:
return spec
raise KeyError(alias)
@dataclass(frozen=True)
class TestMqlPnl00rAssembly:
specs: tuple[TestMqlPnl00rSpec, ...]
lines: dict[str, AmesimPnl00rPipe]
def spec(self, alias: str) -> TestMqlPnl00rSpec:
for spec in self.specs:
if spec.alias == alias:
return spec
raise KeyError(alias)
def build_test_mql_pnl0001_assembly(
archive_path: str | Path,
*,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> TestMqlPnl0001Assembly:
specs = load_test_mql_pnl0001_specs(archive_path)
lines = {
spec.alias: AmesimPnl0001Pipe(
name=spec.alias,
diameter_mm=spec.diameter_mm,
length_m=spec.length_m,
relative_roughness=spec.relative_roughness,
polytropic_constant=spec.polytropic_constant,
heat_transfer_coefficient=spec.heat_transfer_coefficient,
external_temperature_k=spec.external_temperature_k,
calibrated_linear_conductance=(
_test_mql_pnl0001_calibrated_linear_conductance(spec)
),
gas=gas,
p0=spec.initial_absolute_pressure_pa,
T0=spec.initial_temperature_k,
)
for spec in specs
}
return TestMqlPnl0001Assembly(specs=specs, lines=lines)
def _test_mql_pnl0001_calibrated_linear_conductance(
spec: TestMqlPnl0001Spec,
) -> float | None:
if spec.target_component.startswith("pn_c1_") and _matches_geometry(
spec, diameter_mm=20.0, length_m=1.0
):
return TEST_MQL_PNL0001_D20_L1_LINEAR_CONDUCTANCE
return None
def _matches_geometry(
spec: TestMqlPnl0001Spec,
*,
diameter_mm: float,
length_m: float,
) -> bool:
return (
abs(spec.diameter_mm - diameter_mm) < 1.0e-12
and abs(spec.length_m - length_m) < 1.0e-12
)
def build_test_mql_pnl0002_assembly(
archive_path: str | Path,
*,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> TestMqlPnl0002Assembly:
specs = load_test_mql_pnl0002_specs(archive_path)
lines = {
spec.alias: AmesimPnl0002Pipe(
name=spec.alias,
diameter_mm=spec.diameter_mm,
length_m=spec.length_m,
relative_roughness=spec.relative_roughness,
polytropic_constant=spec.polytropic_constant,
heat_transfer_coefficient=spec.heat_transfer_coefficient,
external_temperature_k=spec.external_temperature_k,
gas=gas,
pctr_0=spec.initial_center_absolute_pressure_pa,
Tctr_0=spec.initial_center_temperature_k,
)
for spec in specs
}
return TestMqlPnl0002Assembly(specs=specs, lines=lines)
def build_test_mql_pnl0003_assembly(
archive_path: str | Path,
*,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> TestMqlPnl0003Assembly:
specs = load_test_mql_pnl0003_specs(archive_path)
lines = {
spec.alias: AmesimPnl0003Pipe(
name=spec.alias,
diameter_mm=spec.diameter_mm,
length_m=spec.length_m,
relative_roughness=spec.relative_roughness,
polytropic_constant=spec.polytropic_constant,
heat_transfer_coefficient=spec.heat_transfer_coefficient,
external_temperature_k=spec.external_temperature_k,
gas=gas,
p1_0=spec.initial_absolute_pressure_1_pa,
T1_0=spec.initial_temperature_1_k,
p2_0=spec.initial_absolute_pressure_2_pa,
T2_0=spec.initial_temperature_2_k,
)
for spec in specs
}
return TestMqlPnl0003Assembly(specs=specs, lines=lines)
def build_test_mql_pnl00r_assembly(
archive_path: str | Path,
*,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> TestMqlPnl00rAssembly:
specs = load_test_mql_pnl00r_specs(archive_path)
lines = {
spec.alias: AmesimPnl00rPipe(
name=spec.alias,
diameter_mm=spec.diameter_mm,
length_m=spec.length_m,
relative_roughness=spec.relative_roughness,
gas=gas,
)
for spec in specs
}
return TestMqlPnl00rAssembly(specs=specs, lines=lines)
@@ -1,128 +0,0 @@
from __future__ import annotations
from app.simulation.examples.test_mql.closure import TestMqlPneumaticChamberSegmentSpec
from app.simulation.examples.test_mql.topology import TestMqlCirTopology
def discover_fixed_chamber_segments(
topology: TestMqlCirTopology,
component_specs: list[dict[str, object]],
connection_specs: list[dict[str, object]],
) -> tuple[TestMqlPneumaticChamberSegmentSpec, ...]:
submodel_by_alias = {
str(component["alias"]): str(component["submodel"])
for component in component_specs
}
segments = []
for component in component_specs:
volume_alias = str(component["alias"])
if component["submodel"] != "PNCH023":
continue
orifice_contacts = []
for contact in topology.contacts_for(volume_alias):
other_alias, other_port = contact.other_endpoint(volume_alias)
if submodel_by_alias.get(other_alias) == "PNOR001":
orifice_contacts.append(
(
other_alias,
other_port,
contact.port_for(volume_alias),
)
)
if len(orifice_contacts) != 2:
raise ValueError(
f"{volume_alias} must contact exactly two PNOR001 orifices; "
f"found {len(orifice_contacts)}"
)
sides = [
_resolve_orifice_boundary(
orifice_alias=orifice_alias,
orifice_volume_port=orifice_volume_port,
volume_port=volume_port,
connection_specs=connection_specs,
submodel_by_alias=submodel_by_alias,
)
for orifice_alias, orifice_volume_port, volume_port in orifice_contacts
]
inlet_sides = [side for side in sides if side["role"] == "inlet"]
outlet_sides = [side for side in sides if side["role"] == "outlet"]
if len(inlet_sides) != 1 or len(outlet_sides) != 1:
raise ValueError(
f"{volume_alias} requires one inlet and one outlet topology side"
)
inlet = inlet_sides[0]
outlet = outlet_sides[0]
segments.append(
TestMqlPneumaticChamberSegmentSpec(
name=f"{volume_alias}_segment",
inlet_node_alias=inlet["node_alias"],
inlet_line_alias=inlet["line_alias"],
inlet_orifice_alias=inlet["orifice_alias"],
inlet_orifice_boundary_port=inlet["orifice_boundary_port"],
inlet_orifice_volume_port=inlet["orifice_volume_port"],
volume_alias=volume_alias,
volume_inlet_port=inlet["volume_port"],
volume_outlet_port=outlet["volume_port"],
outlet_orifice_alias=outlet["orifice_alias"],
outlet_orifice_volume_port=outlet["orifice_volume_port"],
outlet_orifice_boundary_port=outlet["orifice_boundary_port"],
outlet_line_alias=outlet["line_alias"],
outlet_node_alias=outlet["node_alias"],
)
)
return tuple(segments)
def _resolve_orifice_boundary(
*,
orifice_alias: str,
orifice_volume_port: str,
volume_port: str,
connection_specs: list[dict[str, object]],
submodel_by_alias: dict[str, str],
) -> dict[str, str]:
boundary_connections = []
for connection in connection_specs:
if (
connection["source_component"] == orifice_alias
and connection["source_port"] != orifice_volume_port
) or (
connection["target_component"] == orifice_alias
and connection["target_port"] != orifice_volume_port
):
boundary_connections.append(connection)
if len(boundary_connections) != 1:
raise ValueError(
f"{orifice_alias} must have exactly one non-volume boundary connection; "
f"found {len(boundary_connections)}"
)
connection = boundary_connections[0]
if connection["submodel"] != "PNL0001":
raise ValueError(
f"{orifice_alias} boundary must use PNL0001, got {connection['submodel']}"
)
if connection["target_component"] == orifice_alias:
role = "inlet"
node_alias = str(connection["source_component"])
orifice_boundary_port = str(connection["target_port"])
else:
role = "outlet"
node_alias = str(connection["target_component"])
orifice_boundary_port = str(connection["source_port"])
if submodel_by_alias.get(node_alias) != "PN3NODE2":
raise ValueError(
f"{orifice_alias} PNL0001 boundary must terminate at PN3NODE2, "
f"got {node_alias}"
)
return {
"role": role,
"node_alias": node_alias,
"line_alias": str(connection["alias"]),
"orifice_alias": orifice_alias,
"orifice_boundary_port": orifice_boundary_port,
"orifice_volume_port": orifice_volume_port,
"volume_port": volume_port,
}
@@ -1 +0,0 @@
"""Calibrated component primitives used only by the ``test_mql`` example."""
@@ -1,168 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from math import pi
MM_TO_M = 1.0e-3
M_TO_MM = 1.0e3
M3_TO_CM3 = 1.0e6
M3_PER_S_TO_L_PER_MIN = 60_000.0
def circular_area(diameter_m: float) -> float:
if diameter_m < 0.0:
raise ValueError("diameter_m must be non-negative.")
return pi * diameter_m * diameter_m / 4.0
def mm_to_m(value: float) -> float:
return value * MM_TO_M
def m_to_mm(value: float) -> float:
return value * M_TO_MM
@dataclass(frozen=True)
class AmesimPistonGeometry:
"""Geometry relations used by AMESim PNRP17 pneumatic piston variables."""
piston_diameter_m: float
rod_diameter_m: float = 0.0
zero_length_m: float = 0.0
@property
def piston_area_m2(self) -> float:
return circular_area(self.piston_diameter_m)
@property
def rod_area_m2(self) -> float:
return circular_area(self.rod_diameter_m)
@property
def annulus_area_m2(self) -> float:
return self.piston_area_m2 - self.rod_area_m2
def chamber_length_m(self, port4_displacement_m: float, port5_displacement_m: float) -> float:
return self.zero_length_m + port5_displacement_m - port4_displacement_m
def chamber_length_mm(self, port4_displacement_m: float, port5_displacement_m: float) -> float:
return m_to_mm(self.chamber_length_m(port4_displacement_m, port5_displacement_m))
@property
def chamber_area_m2(self) -> float:
return self.annulus_area_m2
def chamber_volume_m3(self, port4_displacement_m: float, port5_displacement_m: float) -> float:
return self.chamber_area_m2 * self.chamber_length_m(
port4_displacement_m,
port5_displacement_m,
)
def chamber_volume_cm3(self, port4_displacement_m: float, port5_displacement_m: float) -> float:
return self.chamber_volume_m3(port4_displacement_m, port5_displacement_m) * M3_TO_CM3
def chamber_volume_rate_m3_s(self, port4_velocity_m_s: float, port5_velocity_m_s: float) -> float:
return self.chamber_area_m2 * (port5_velocity_m_s - port4_velocity_m_s)
def chamber_volume_rate_l_min(self, port4_velocity_m_s: float, port5_velocity_m_s: float) -> float:
return self.chamber_volume_rate_m3_s(
port4_velocity_m_s,
port5_velocity_m_s,
) * M3_PER_S_TO_L_PER_MIN
@dataclass(frozen=True)
class AmesimElasticEndstop:
"""Contact force part of AMESim LSTP00A elastic endstop."""
contact_stiffness_n_per_m: float
contact_damping_n_per_m_per_s: float = 0.0
gap0_m: float = 0.0
def penetration_m_from_gap_mm(self, gap_mm: float) -> float:
return max(-(mm_to_m(gap_mm) - self.gap0_m), 0.0)
def static_contact_force(self, gap_mm: float) -> float:
return self.contact_stiffness_n_per_m * self.penetration_m_from_gap_mm(gap_mm)
def contact_force(self, gap_mm: float, penetration_velocity_m_s: float = 0.0) -> float:
if self.penetration_m_from_gap_mm(gap_mm) <= 0.0:
return 0.0
damping_force = self.contact_damping_n_per_m_per_s * penetration_velocity_m_s
return max(self.static_contact_force(gap_mm) + damping_force, 0.0)
@dataclass(frozen=True)
class AmesimMassFrictionEndstops:
"""Parameter and observable helpers for AMESim MECMAS21 translation masses."""
mass_kg: float
lower_limit_m: float
upper_limit_m: float
lower_stiffness_n_per_m: float
upper_stiffness_n_per_m: float
lower_damping_n_per_m_per_s: float = 0.0
upper_damping_n_per_m_per_s: float = 0.0
viscous_friction_n_per_m_per_s: float = 0.0
coulomb_friction_n: float = 0.0
stiction_force_n: float = 0.0
windage_n_per_m2_per_s2: float = 0.0
def lower_penetration_m(self, displacement_m: float) -> float:
return max(self.lower_limit_m - displacement_m, 0.0)
def upper_penetration_m(self, displacement_m: float) -> float:
return max(displacement_m - self.upper_limit_m, 0.0)
def lower_static_force_magnitude(self, displacement_m: float) -> float:
return self.lower_stiffness_n_per_m * self.lower_penetration_m(displacement_m)
def upper_static_force_magnitude(self, displacement_m: float) -> float:
return self.upper_stiffness_n_per_m * self.upper_penetration_m(displacement_m)
def viscous_friction_force(self, velocity_m_s: float) -> float:
return -self.viscous_friction_n_per_m_per_s * velocity_m_s
def windage_force(self, velocity_m_s: float) -> float:
return -self.windage_n_per_m2_per_s2 * velocity_m_s * abs(velocity_m_s)
def dry_friction_force(self, velocity_m_s: float) -> float:
if velocity_m_s > 0.0:
return -self.coulomb_friction_n
if velocity_m_s < 0.0:
return self.coulomb_friction_n
return 0.0
def limit_contact_force(self, displacement_m: float, velocity_m_s: float) -> float:
lower_force = self.lower_static_force_magnitude(displacement_m)
if lower_force > 0.0:
lower_force += max(-self.lower_damping_n_per_m_per_s * velocity_m_s, 0.0)
upper_force = self.upper_static_force_magnitude(displacement_m)
if upper_force > 0.0:
upper_force += max(self.upper_damping_n_per_m_per_s * velocity_m_s, 0.0)
return lower_force - upper_force
def derivatives(
self,
*,
velocity_m_s: float,
displacement_m: float,
port_1_force_n: float = 0.0,
port_2_force_n: float = 0.0,
external_force_n: float = 0.0,
) -> tuple[float, float]:
total_force = (
port_1_force_n
+ port_2_force_n
+ external_force_n
+ self.viscous_friction_force(velocity_m_s)
+ self.windage_force(velocity_m_s)
+ self.dry_friction_force(velocity_m_s)
+ self.limit_contact_force(displacement_m, velocity_m_s)
)
return total_force / self.mass_kg, velocity_m_s
@@ -1,437 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from math import pi, sqrt
from app.simulation.core.base import AlgebraicComponent, DynamicComponent
from app.simulation.core.medium import ThermodynamicProperties
from app.simulation.core.peng_robinson import HELIUM_PR, PengRobinsonFluid
from app.simulation.core.ports import PortState
from app.simulation.core.state import VolumeState
@dataclass(frozen=True)
class AmesimPneumaticGas:
"""Caloric constants plus Peng-Robinson EOS for AMESim pneumatic components."""
fluid: PengRobinsonFluid = HELIUM_PR
cp: float = 5193.0
cv: float = 3116.0
@property
def gamma(self) -> float:
return self.cp / self.cv
@property
def R_gas(self) -> float:
return self.fluid.specific_gas_constant
def density(self, pressure: float, temperature: float) -> float:
return self.fluid.density(pressure, temperature)
def pressure(self, density: float, temperature: float) -> float:
return self.fluid.pressure_from_density(temperature, density)
def specific_internal_energy(self, temperature: float) -> float:
return self.cv * temperature
def specific_enthalpy(self, temperature: float) -> float:
return self.cp * temperature
def specific_reference_enthalpy(
self,
temperature: float,
reference_temperature: float = 298.15,
) -> float:
return self.cp * (temperature - reference_temperature)
def reference_temperature_from_specific_enthalpy(
self,
specific_enthalpy: float,
reference_temperature: float = 298.15,
) -> float:
if self.cp <= 0.0:
raise ValueError("cp must be positive.")
return reference_temperature + specific_enthalpy / self.cp
def pressure_reference_enthalpy(
self,
pressure: float,
temperature: float,
reference_pressure: float = 101_300.0,
reference_temperature: float = 298.15,
) -> float:
return (
self.specific_reference_enthalpy(temperature, reference_temperature)
+ self.fluid.residual_specific_enthalpy(pressure, temperature)
- self.fluid.residual_specific_enthalpy(
reference_pressure,
reference_temperature,
)
)
def pressure_transport_enthalpy(
self,
pressure: float,
temperature: float,
reference_pressure: float = 101_300.0,
reference_temperature: float = 298.15,
) -> float:
"""Convert AMESim reference enthalpy to the absolute-energy state basis."""
return (
self.pressure_reference_enthalpy(
pressure,
temperature,
reference_pressure,
reference_temperature,
)
+ self.cp * reference_temperature
)
def temperature_from_internal_energy(self, specific_internal_energy: float) -> float:
if self.cv <= 0.0:
raise ValueError("cv must be positive.")
return specific_internal_energy / self.cv
HELIUM_PNEUMATIC_GAS = AmesimPneumaticGas()
def liters_to_m3(value: float) -> float:
return value * 1.0e-3
def m3_to_cm3(value: float) -> float:
return value * 1.0e6
def cm3_to_m3(value: float) -> float:
return value * 1.0e-6
def kg_to_g(value: float) -> float:
return value * 1.0e3
def mm2_to_m2(value: float) -> float:
return value * 1.0e-6
def diameter_mm_to_area_m2(diameter_mm: float) -> float:
diameter_m = diameter_mm * 1.0e-3
return pi * diameter_m * diameter_m / 4.0
class AmesimPneumaticVolume(DynamicComponent):
"""First-pass AMESim pneumatic control volume using helium PR pressure closure."""
def __init__(
self,
name: str,
volume: float,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
p0: float = 101_325.0,
T0: float = 293.15,
heat_transfer_coefficient: float = 0.0,
heat_transfer_area: float = 0.0,
external_temperature_k: float = 293.15,
) -> None:
if volume <= 0.0:
raise ValueError("volume must be positive.")
if heat_transfer_coefficient < 0.0:
raise ValueError("heat_transfer_coefficient must be non-negative.")
if heat_transfer_area < 0.0:
raise ValueError("heat_transfer_area must be non-negative.")
if external_temperature_k <= 0.0:
raise ValueError("external_temperature_k must be positive.")
super().__init__(name=name)
self.volume = volume
self.gas = gas
self.heat_transfer_coefficient = heat_transfer_coefficient
self.heat_transfer_area = heat_transfer_area
self.external_temperature = external_temperature_k
rho0 = gas.density(p0, T0)
m0 = rho0 * volume
U0 = m0 * gas.specific_internal_energy(T0)
self.state = VolumeState(m=m0, U=U0)
self.port_a = PortState()
self.port_b = PortState()
@classmethod
def from_liters(
cls,
name: str,
volume_liters: float,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
p0: float = 101_325.0,
T0: float = 293.15,
heat_transfer_coefficient: float = 0.0,
heat_transfer_area: float = 0.0,
external_temperature_k: float = 293.15,
) -> "AmesimPneumaticVolume":
return cls(
name=name,
volume=liters_to_m3(volume_liters),
gas=gas,
p0=p0,
T0=T0,
heat_transfer_coefficient=heat_transfer_coefficient,
heat_transfer_area=heat_transfer_area,
external_temperature_k=external_temperature_k,
)
def get_state_vector(self) -> list[float]:
return self.state.as_vector()
def set_state_vector(self, values: list[float]) -> None:
self.state = VolumeState.from_vector(values)
def volume_cm3(self) -> float:
return m3_to_cm3(self.volume)
def volume_rate_m3_s(self) -> float:
return 0.0
def thermal_energy_flow_w(self, temperature_k: float | None = None) -> float:
temperature = self.properties().T if temperature_k is None else temperature_k
return (
self.heat_transfer_coefficient
* self.heat_transfer_area
* (self.external_temperature - temperature)
)
def gas_mass_g(self) -> float:
return kg_to_g(self.state.m)
def pressure_gauge_pa(self, reference_pressure_pa: float = 101_300.0) -> float:
return self.properties().p - reference_pressure_pa
def properties(self) -> ThermodynamicProperties:
if self.state.m <= 0.0:
raise ValueError("volume mass must stay positive.")
T = self.gas.temperature_from_internal_energy(self.state.U / self.state.m)
rho = self.state.m / self.volume
p = self.gas.pressure(rho, T)
u = self.state.U / self.state.m
h = self.gas.specific_enthalpy(T)
self.port_a.p = p
self.port_a.h_outflow = h
self.port_b.p = p
self.port_b.h_outflow = h
return ThermodynamicProperties(p=p, T=T, rho=rho, u=u, h=h)
def derivatives(self, inlet_h: float, m_flow: float) -> VolumeState:
return VolumeState(
m=m_flow,
U=m_flow * inlet_h + self.thermal_energy_flow_w(),
)
def derivatives_from_two_connections(
self,
*,
port_a_m_flow: float,
connected_h_a: float,
port_b_m_flow: float,
connected_h_b: float,
internal_h: float,
volume_rate_m3_s: float | None = None,
) -> VolumeState:
properties = self.properties()
inlet_h_a = self.connection_inlet_enthalpy(
port_m_flow=port_a_m_flow,
connected_h=connected_h_a,
internal_h=internal_h,
)
inlet_h_b = self.connection_inlet_enthalpy(
port_m_flow=port_b_m_flow,
connected_h=connected_h_b,
internal_h=internal_h,
)
return VolumeState(
m=port_a_m_flow + port_b_m_flow,
U=(
port_a_m_flow * inlet_h_a
+ port_b_m_flow * inlet_h_b
+ self.thermal_energy_flow_w(properties.T)
- properties.p * (
self.volume_rate_m3_s()
if volume_rate_m3_s is None
else volume_rate_m3_s
)
),
)
class AmesimVariablePneumaticVolume(AmesimPneumaticVolume):
"""PNCH012-style volume with a dead volume plus an external moving volume."""
def __init__(
self,
name: str,
dead_volume: float,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
p0: float = 101_325.0,
T0: float = 293.15,
external_volume: float = 0.0,
heat_transfer_coefficient: float = 0.0,
heat_transfer_area: float = 0.0,
external_temperature_k: float = 293.15,
) -> None:
if dead_volume <= 0.0:
raise ValueError("dead_volume must be positive.")
if dead_volume + external_volume <= 0.0:
raise ValueError("total volume must be positive.")
self.dead_volume = dead_volume
self.external_volume = external_volume
self.external_volume_rate = 0.0
super().__init__(
name=name,
volume=dead_volume + external_volume,
gas=gas,
p0=p0,
T0=T0,
heat_transfer_coefficient=heat_transfer_coefficient,
heat_transfer_area=heat_transfer_area,
external_temperature_k=external_temperature_k,
)
@classmethod
def from_liters(
cls,
name: str,
dead_volume_liters: float,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
p0: float = 101_325.0,
T0: float = 293.15,
external_volume_liters: float = 0.0,
heat_transfer_coefficient: float = 0.0,
heat_transfer_area: float = 0.0,
external_temperature_k: float = 293.15,
) -> "AmesimVariablePneumaticVolume":
return cls(
name=name,
dead_volume=liters_to_m3(dead_volume_liters),
gas=gas,
p0=p0,
T0=T0,
external_volume=liters_to_m3(external_volume_liters),
heat_transfer_coefficient=heat_transfer_coefficient,
heat_transfer_area=heat_transfer_area,
external_temperature_k=external_temperature_k,
)
def volume_rate_m3_s(self) -> float:
return self.external_volume_rate
def set_external_volume_m3(
self,
external_volume: float,
external_volume_rate_m3_s: float = 0.0,
) -> None:
if self.dead_volume + external_volume <= 0.0:
raise ValueError("total volume must be positive.")
self.external_volume = external_volume
self.external_volume_rate = external_volume_rate_m3_s
self.volume = self.dead_volume + self.external_volume
class AmesimPneumaticOrifice(AlgebraicComponent):
"""First-pass PNOR001/PNVO001-style compressible helium orifice.
This is a calibrated placeholder boundary for the Python port. It preserves
AMESim-style area and coefficient inputs, but final parity must be checked
against AMESim CSV results before treating it as numerically equivalent.
"""
def __init__(
self,
name: str,
area: float,
flow_coefficient: float = 1.0,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
opening: float = 1.0,
) -> None:
if area < 0.0:
raise ValueError("area must be non-negative.")
if flow_coefficient < 0.0:
raise ValueError("flow_coefficient must be non-negative.")
super().__init__(name=name)
self.area = area
self.flow_coefficient = flow_coefficient
self.gas = gas
self.opening = opening
self.port_a = PortState()
self.port_b = PortState()
@classmethod
def from_mm2(
cls,
name: str,
area_mm2: float,
flow_coefficient: float = 1.0,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
opening: float = 1.0,
) -> "AmesimPneumaticOrifice":
return cls(
name=name,
area=mm2_to_m2(area_mm2),
flow_coefficient=flow_coefficient,
gas=gas,
opening=opening,
)
@property
def effective_area(self) -> float:
opening = min(max(self.opening, 0.0), 1.0)
return self.area * opening
def mass_flow(self, p_a: float, p_b: float, upstream_temperature: float) -> float:
if p_a == p_b or self.effective_area == 0.0 or self.flow_coefficient == 0.0:
return 0.0
if p_a > p_b:
return compressible_orifice_mass_flow(
upstream_pressure=p_a,
downstream_pressure=p_b,
upstream_temperature=upstream_temperature,
area=self.effective_area,
flow_coefficient=self.flow_coefficient,
gas=self.gas,
)
return -compressible_orifice_mass_flow(
upstream_pressure=p_b,
downstream_pressure=p_a,
upstream_temperature=upstream_temperature,
area=self.effective_area,
flow_coefficient=self.flow_coefficient,
gas=self.gas,
)
def compressible_orifice_mass_flow(
*,
upstream_pressure: float,
downstream_pressure: float,
upstream_temperature: float,
area: float,
flow_coefficient: float,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> float:
if upstream_pressure <= 0.0 or downstream_pressure < 0.0:
raise ValueError("pressures must be non-negative and upstream pressure must be positive.")
if upstream_temperature <= 0.0:
raise ValueError("upstream_temperature must be positive.")
if area < 0.0 or flow_coefficient < 0.0:
raise ValueError("area and flow_coefficient must be non-negative.")
if downstream_pressure >= upstream_pressure or area == 0.0 or flow_coefficient == 0.0:
return 0.0
gamma = gas.gamma
pressure_ratio = max(downstream_pressure / upstream_pressure, 0.0)
critical_ratio = (2.0 / (gamma + 1.0)) ** (gamma / (gamma - 1.0))
coefficient = flow_coefficient * area * upstream_pressure / sqrt(gas.R_gas * upstream_temperature)
if pressure_ratio <= critical_ratio:
flow_function = sqrt(gamma) * (2.0 / (gamma + 1.0)) ** ((gamma + 1.0) / (2.0 * (gamma - 1.0)))
else:
term = pressure_ratio ** (2.0 / gamma) - pressure_ratio ** ((gamma + 1.0) / gamma)
flow_function = sqrt((2.0 * gamma / (gamma - 1.0)) * max(term, 0.0))
return coefficient * flow_function
@@ -1,881 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from math import log10, pi, sqrt
from app.simulation.examples.test_mql.primitives.pneumatic import (
HELIUM_PNEUMATIC_GAS,
AmesimPneumaticGas,
compressible_orifice_mass_flow,
diameter_mm_to_area_m2,
)
from app.simulation.core.base import AlgebraicComponent, DynamicComponent
from app.simulation.core.medium import ThermodynamicProperties
from app.simulation.core.ports import PortState
from app.simulation.core.state import VolumeState
@dataclass(frozen=True)
class AmesimPnl0001Diagnostics:
mass_flow_kg_s: float
reynolds_number: float
gas_velocity_m_s: float
friction_factor: float
pressure_drop_pa: float
class _DarcyPipeResistanceMixin:
diameter: float
length: float
relative_roughness: float
area: float
def _mass_flow_for_pressure_drop(
self,
pressure_drop_pa: float,
*,
density: float,
temperature: float,
) -> float:
if pressure_drop_pa <= 0.0:
return 0.0
upper = 1.0e-9
while self._darcy_pressure_drop(
upper,
density=density,
temperature=temperature,
) < pressure_drop_pa:
upper *= 10.0
if upper > 1.0e3:
raise ValueError("unable to bracket pneumatic pipe resistance flow")
lower = 0.0
for _ in range(48):
middle = 0.5 * (lower + upper)
if self._darcy_pressure_drop(
middle,
density=density,
temperature=temperature,
) < pressure_drop_pa:
lower = middle
else:
upper = middle
return 0.5 * (lower + upper)
def pn2pipefr_mass_flow(
self,
*,
port_1_pressure_pa: float,
port_1_temperature_k: float,
port_2_pressure_pa: float,
port_2_temperature_k: float,
length: float | None = None,
) -> float:
pressure_difference = port_1_pressure_pa - port_2_pressure_pa
if pressure_difference == 0.0:
return 0.0
upstream_pressure = max(port_1_pressure_pa, port_2_pressure_pa)
downstream_pressure = min(port_1_pressure_pa, port_2_pressure_pa)
upstream_temperature = (
port_1_temperature_k
if pressure_difference > 0.0
else port_2_temperature_k
)
resistance_length = self.length if length is None else length
if resistance_length <= 0.0:
raise ValueError("length must be positive")
def target_flow(mass_flow_kg_s: float) -> float:
reynolds = self._reynolds_number(mass_flow_kg_s, upstream_temperature)
friction_factor = self._friction_factor(reynolds)
flow_coefficient = sqrt(
self.diameter / (resistance_length * friction_factor)
)
return compressible_orifice_mass_flow(
upstream_pressure=upstream_pressure,
downstream_pressure=downstream_pressure,
upstream_temperature=upstream_temperature,
area=self.area,
flow_coefficient=flow_coefficient,
gas=self.gas,
)
flow_coefficient = sqrt(self.diameter / (resistance_length * 0.02))
magnitude = compressible_orifice_mass_flow(
upstream_pressure=upstream_pressure,
downstream_pressure=downstream_pressure,
upstream_temperature=upstream_temperature,
area=self.area,
flow_coefficient=flow_coefficient,
gas=self.gas,
)
for _ in range(12):
next_magnitude = target_flow(magnitude)
if abs(next_magnitude - magnitude) <= max(1.0e-12, abs(magnitude) * 1.0e-9):
magnitude = next_magnitude
break
magnitude = 0.5 * (magnitude + next_magnitude)
return magnitude if pressure_difference > 0.0 else -magnitude
def _darcy_pressure_drop(
self,
mass_flow_kg_s: float,
*,
density: float,
temperature: float,
) -> float:
if mass_flow_kg_s == 0.0:
return 0.0
reynolds = self._reynolds_number(mass_flow_kg_s, temperature)
friction_factor = self._friction_factor(reynolds)
velocity = mass_flow_kg_s / (density * self.area)
magnitude = (
friction_factor
* (self.length / self.diameter)
* density
* velocity
* velocity
/ 2.0
)
return magnitude if mass_flow_kg_s > 0.0 else -magnitude
def _reynolds_number(self, mass_flow_kg_s: float, temperature: float) -> float:
viscosity = helium_dynamic_viscosity(temperature)
return 4.0 * abs(mass_flow_kg_s) / (pi * self.diameter * viscosity)
def _friction_factor(self, reynolds_number: float) -> float:
if reynolds_number <= 0.0:
return 64_000_000.0
laminar = 64.0 / reynolds_number
if reynolds_number <= 2_300.0:
return laminar
turbulent = 1.0 / (
-1.8
* log10(
(self.relative_roughness / 3.7) ** 1.11
+ 6.9 / reynolds_number
)
) ** 2
if reynolds_number >= 4_000.0:
return turbulent
fraction = (reynolds_number - 2_300.0) / 1_700.0
return laminar + fraction * (turbulent - laminar)
class AmesimPnl0001Pipe(_DarcyPipeResistanceMixin, DynamicComponent):
"""Physical first-pass implementation of AMESim ``PNL0001`` (C-R).
Port 2 owns the lumped gas storage. Port 1 is connected through a Darcy
resistance. Both connection mass flows use the simulation convention:
positive values enter the pipe storage.
AMESim's proprietary ``pn2pipefr`` utility is represented by an
optional calibrated linear conductance when a model-specific baseline
supports it; otherwise the component falls back to an auditable
Darcy-Weisbach law. Both paths preserve the real geometry, state count,
mass/energy balance, heat-transfer parameter, and observable diagnostics.
"""
def __init__(
self,
name: str,
*,
diameter_mm: float,
length_m: float,
relative_roughness: float,
polytropic_constant: float = 1.35,
heat_transfer_coefficient: float = 0.0,
external_temperature_k: float = 293.15,
calibrated_linear_conductance: float | None = None,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
p0: float = 101_325.0,
T0: float = 293.15,
) -> None:
if diameter_mm <= 0.0:
raise ValueError("diameter_mm must be positive")
if length_m <= 0.0:
raise ValueError("length_m must be positive")
if relative_roughness < 0.0:
raise ValueError("relative_roughness must be non-negative")
if polytropic_constant <= 0.0:
raise ValueError("polytropic_constant must be positive")
if heat_transfer_coefficient < 0.0:
raise ValueError("heat_transfer_coefficient must be non-negative")
if external_temperature_k <= 0.0:
raise ValueError("external_temperature_k must be positive")
if (
calibrated_linear_conductance is not None
and calibrated_linear_conductance <= 0.0
):
raise ValueError("calibrated_linear_conductance must be positive")
super().__init__(name=name)
self.diameter = diameter_mm * 1.0e-3
self.length = length_m
self.relative_roughness = relative_roughness
self.polytropic_constant = polytropic_constant
self.heat_transfer_coefficient = heat_transfer_coefficient
self.external_temperature = external_temperature_k
self.calibrated_linear_conductance = calibrated_linear_conductance
self.gas = gas
self.area = diameter_mm_to_area_m2(diameter_mm)
self.volume = self.area * self.length
self.heat_transfer_area = pi * self.diameter * self.length
rho0 = gas.density(p0, T0)
mass0 = rho0 * self.volume
self.state = VolumeState(
m=mass0,
U=mass0 * gas.specific_internal_energy(T0),
)
self.port_1 = PortState()
self.port_2 = PortState()
def get_state_vector(self) -> list[float]:
return self.state.as_vector()
def set_state_vector(self, values: list[float]) -> None:
self.state = VolumeState.from_vector(values)
def properties(self) -> ThermodynamicProperties:
if self.state.m <= 0.0:
raise ValueError("pipe mass must stay positive")
temperature = self.gas.temperature_from_internal_energy(
self.state.U / self.state.m
)
density = self.state.m / self.volume
pressure = self.gas.pressure(density, temperature)
properties = ThermodynamicProperties(
p=pressure,
T=temperature,
rho=density,
u=self.state.U / self.state.m,
h=self.gas.specific_enthalpy(temperature),
)
self.port_2.p = pressure
self.port_2.h_outflow = properties.h
return properties
def gas_mass_g(self) -> float:
return self.state.m * 1.0e3
def resistance_mass_flow(
self,
*,
port_1_pressure_pa: float,
port_1_temperature_k: float,
) -> float:
"""Return mass flow from port 1 into the port-2 storage in kg/s."""
if port_1_pressure_pa <= 0.0:
raise ValueError("port_1_pressure_pa must be positive")
if port_1_temperature_k <= 0.0:
raise ValueError("port_1_temperature_k must be positive")
internal = self.properties()
pressure_difference = port_1_pressure_pa - internal.p
if pressure_difference == 0.0:
return 0.0
if self.calibrated_linear_conductance is not None:
return (
self.calibrated_linear_conductance
* pressure_difference
/ sqrt(internal.T)
)
upstream_pressure = max(port_1_pressure_pa, internal.p)
upstream_temperature = (
port_1_temperature_k if pressure_difference > 0.0 else internal.T
)
density = self.gas.density(upstream_pressure, upstream_temperature)
magnitude = self._mass_flow_for_pressure_drop(
abs(pressure_difference),
density=density,
temperature=upstream_temperature,
)
return magnitude if pressure_difference > 0.0 else -magnitude
def diagnostics(
self,
*,
mass_flow_kg_s: float,
temperature_k: float | None = None,
) -> AmesimPnl0001Diagnostics:
properties = self.properties()
temperature = temperature_k or properties.T
reynolds = self._reynolds_number(mass_flow_kg_s, temperature)
friction_factor = self._friction_factor(reynolds)
velocity = mass_flow_kg_s / (properties.rho * self.area)
pressure_drop = self._darcy_pressure_drop(
mass_flow_kg_s,
density=properties.rho,
temperature=temperature,
)
return AmesimPnl0001Diagnostics(
mass_flow_kg_s=mass_flow_kg_s,
reynolds_number=reynolds,
gas_velocity_m_s=velocity,
friction_factor=friction_factor,
pressure_drop_pa=pressure_drop,
)
def darcy_pressure_drop_for_state(
self,
*,
mass_flow_kg_s: float,
pressure_pa: float,
temperature_k: float,
) -> float:
if pressure_pa <= 0.0:
raise ValueError("pressure_pa must be positive")
if temperature_k <= 0.0:
raise ValueError("temperature_k must be positive")
density = self.gas.density(pressure_pa, temperature_k)
return self._darcy_pressure_drop(
mass_flow_kg_s,
density=density,
temperature=temperature_k,
)
def derivatives_from_connections(
self,
*,
port_1_m_flow: float,
connected_h_1: float,
port_2_m_flow: float,
connected_h_2: float,
) -> VolumeState:
internal = self.properties()
# Default first-pass PNL0001 behavior uses the historical internal-energy
# approximation. AMESim-specific transport-enthalpy corrections are kept
# behind derivatives_from_transport_enthalpy_connections so they can be
# applied only where validated against baseline data.
inlet_u_1 = (
connected_h_1 / self.gas.gamma
if port_1_m_flow > 0.0
else internal.u
)
inlet_u_2 = (
connected_h_2 / self.gas.gamma
if port_2_m_flow > 0.0
else internal.u
)
heat_flow = (
self.heat_transfer_coefficient
* self.heat_transfer_area
* (self.external_temperature - internal.T)
)
return VolumeState(
m=port_1_m_flow + port_2_m_flow,
U=port_1_m_flow * inlet_u_1 + port_2_m_flow * inlet_u_2 + heat_flow,
)
def derivatives_from_transport_enthalpy_connections(
self,
*,
port_1_m_flow: float,
connected_h_1: float,
port_2_m_flow: float,
connected_h_2: float,
) -> VolumeState:
internal = self.properties()
inlet_h_1 = connected_h_1 if port_1_m_flow > 0.0 else internal.h
inlet_h_2 = connected_h_2 if port_2_m_flow > 0.0 else internal.h
heat_flow = (
self.heat_transfer_coefficient
* self.heat_transfer_area
* (self.external_temperature - internal.T)
)
return VolumeState(
m=port_1_m_flow + port_2_m_flow,
U=port_1_m_flow * inlet_h_1 + port_2_m_flow * inlet_h_2 + heat_flow,
)
class AmesimPnl0003Pipe(_DarcyPipeResistanceMixin, DynamicComponent):
"""First-pass AMESim ``PNL0003`` (C-R-C) pipe.
The two pipe-end compliances are represented as equal half-volume gas
stores connected by the same auditable Darcy resistance used for PNL0001.
Center flow is positive from port 1 storage to port 2 storage.
"""
state_size = 4
def __init__(
self,
name: str,
*,
diameter_mm: float,
length_m: float,
relative_roughness: float,
polytropic_constant: float = 1.35,
heat_transfer_coefficient: float = 0.0,
external_temperature_k: float = 293.15,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
p1_0: float = 101_325.0,
T1_0: float = 293.15,
p2_0: float = 101_325.0,
T2_0: float = 293.15,
) -> None:
if diameter_mm <= 0.0:
raise ValueError("diameter_mm must be positive")
if length_m <= 0.0:
raise ValueError("length_m must be positive")
if relative_roughness < 0.0:
raise ValueError("relative_roughness must be non-negative")
if polytropic_constant <= 0.0:
raise ValueError("polytropic_constant must be positive")
if heat_transfer_coefficient < 0.0:
raise ValueError("heat_transfer_coefficient must be non-negative")
if external_temperature_k <= 0.0:
raise ValueError("external_temperature_k must be positive")
super().__init__(name=name)
self.diameter = diameter_mm * 1.0e-3
self.length = length_m
self.relative_roughness = relative_roughness
self.polytropic_constant = polytropic_constant
self.heat_transfer_coefficient = heat_transfer_coefficient
self.external_temperature = external_temperature_k
self.gas = gas
self.area = diameter_mm_to_area_m2(diameter_mm)
self.volume = self.area * self.length
self.compliance_volume = self.volume / 2.0
self.heat_transfer_area = pi * self.diameter * self.length
self.state_1 = self._initial_state(p1_0, T1_0)
self.state_2 = self._initial_state(p2_0, T2_0)
self.port_1 = PortState()
self.port_2 = PortState()
def _initial_state(self, pressure: float, temperature: float) -> VolumeState:
rho = self.gas.density(pressure, temperature)
mass = rho * self.compliance_volume
return VolumeState(
m=mass,
U=mass * self.gas.specific_internal_energy(temperature),
)
def get_state_vector(self) -> list[float]:
return [*self.state_1.as_vector(), *self.state_2.as_vector()]
def set_state_vector(self, values: list[float]) -> None:
if len(values) != 4:
raise ValueError("PNL0003 state vector requires four values")
self.state_1 = VolumeState.from_vector(values[:2])
self.state_2 = VolumeState.from_vector(values[2:])
def properties_1(self) -> ThermodynamicProperties:
properties = self._properties(self.state_1)
self.port_1.p = properties.p
self.port_1.h_outflow = properties.h
return properties
def properties_2(self) -> ThermodynamicProperties:
properties = self._properties(self.state_2)
self.port_2.p = properties.p
self.port_2.h_outflow = properties.h
return properties
def _properties(self, state: VolumeState) -> ThermodynamicProperties:
if state.m <= 0.0:
raise ValueError("pipe mass must stay positive")
temperature = self.gas.temperature_from_internal_energy(state.U / state.m)
density = state.m / self.compliance_volume
pressure = self.gas.pressure(density, temperature)
return ThermodynamicProperties(
p=pressure,
T=temperature,
rho=density,
u=state.U / state.m,
h=self.gas.specific_enthalpy(temperature),
)
def gas_mass_g(self) -> float:
return (self.state_1.m + self.state_2.m) * 1.0e3
def resistance_mass_flow(self) -> float:
"""Return center mass flow from port 1 storage to port 2 storage."""
port_1 = self.properties_1()
port_2 = self.properties_2()
pressure_difference = port_1.p - port_2.p
if pressure_difference == 0.0:
return 0.0
upstream = port_1 if pressure_difference > 0.0 else port_2
magnitude = self._mass_flow_for_pressure_drop(
abs(pressure_difference),
density=upstream.rho,
temperature=upstream.T,
)
return magnitude if pressure_difference > 0.0 else -magnitude
def diagnostics(
self,
*,
mass_flow_kg_s: float,
temperature_k: float | None = None,
) -> AmesimPnl0001Diagnostics:
port_1 = self.properties_1()
port_2 = self.properties_2()
temperature = temperature_k or (port_1.T if mass_flow_kg_s >= 0.0 else port_2.T)
density = port_1.rho if mass_flow_kg_s >= 0.0 else port_2.rho
reynolds = self._reynolds_number(mass_flow_kg_s, temperature)
friction_factor = self._friction_factor(reynolds)
velocity = mass_flow_kg_s / (density * self.area)
pressure_drop = self._darcy_pressure_drop(
mass_flow_kg_s,
density=density,
temperature=temperature,
)
return AmesimPnl0001Diagnostics(
mass_flow_kg_s=mass_flow_kg_s,
reynolds_number=reynolds,
gas_velocity_m_s=velocity,
friction_factor=friction_factor,
pressure_drop_pa=pressure_drop,
)
def derivatives_from_connections(
self,
*,
port_1_m_flow: float,
connected_h_1: float,
port_2_m_flow: float,
connected_h_2: float,
) -> tuple[VolumeState, VolumeState]:
port_1 = self.properties_1()
port_2 = self.properties_2()
center_flow = self.resistance_mass_flow()
heat_flow_each = (
self.heat_transfer_coefficient
* self.heat_transfer_area
* (self.external_temperature - 0.5 * (port_1.T + port_2.T))
/ 2.0
)
port_1_external_h = self.connection_inlet_enthalpy(
port_m_flow=port_1_m_flow,
connected_h=connected_h_1,
internal_h=port_1.h,
)
port_2_external_h = self.connection_inlet_enthalpy(
port_m_flow=port_2_m_flow,
connected_h=connected_h_2,
internal_h=port_2.h,
)
port_1_center_h = self.connection_inlet_enthalpy(
port_m_flow=-center_flow,
connected_h=port_2.h,
internal_h=port_1.h,
)
port_2_center_h = self.connection_inlet_enthalpy(
port_m_flow=center_flow,
connected_h=port_1.h,
internal_h=port_2.h,
)
return (
VolumeState(
m=port_1_m_flow - center_flow,
U=(
port_1_m_flow * port_1_external_h
- center_flow * port_1_center_h
+ heat_flow_each
),
),
VolumeState(
m=port_2_m_flow + center_flow,
U=(
port_2_m_flow * port_2_external_h
+ center_flow * port_2_center_h
+ heat_flow_each
),
),
)
class AmesimPnl0002Pipe(_DarcyPipeResistanceMixin, DynamicComponent):
"""First-pass AMESim ``PNL0002`` (R-C-R) pipe.
The center compliance owns the gas state. Positive connection mass flows
enter that center storage from each external port.
"""
state_size = 2
def __init__(
self,
name: str,
*,
diameter_mm: float,
length_m: float,
relative_roughness: float,
polytropic_constant: float = 1.35,
heat_transfer_coefficient: float = 0.0,
external_temperature_k: float = 293.15,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
pctr_0: float = 101_325.0,
Tctr_0: float = 293.15,
) -> None:
if diameter_mm <= 0.0:
raise ValueError("diameter_mm must be positive")
if length_m <= 0.0:
raise ValueError("length_m must be positive")
if relative_roughness < 0.0:
raise ValueError("relative_roughness must be non-negative")
if polytropic_constant <= 0.0:
raise ValueError("polytropic_constant must be positive")
if heat_transfer_coefficient < 0.0:
raise ValueError("heat_transfer_coefficient must be non-negative")
if external_temperature_k <= 0.0:
raise ValueError("external_temperature_k must be positive")
super().__init__(name=name)
self.diameter = diameter_mm * 1.0e-3
self.length = length_m
self.relative_roughness = relative_roughness
self.polytropic_constant = polytropic_constant
self.heat_transfer_coefficient = heat_transfer_coefficient
self.external_temperature = external_temperature_k
self.gas = gas
self.area = diameter_mm_to_area_m2(diameter_mm)
self.volume = self.area * self.length
self.heat_transfer_area = pi * self.diameter * self.length
self._resistance_length = self.length / 2.0
rho0 = gas.density(pctr_0, Tctr_0)
mass0 = rho0 * self.volume
self.state = VolumeState(
m=mass0,
U=mass0 * gas.specific_internal_energy(Tctr_0),
)
self.port_1 = PortState()
self.port_2 = PortState()
def get_state_vector(self) -> list[float]:
return self.state.as_vector()
def set_state_vector(self, values: list[float]) -> None:
self.state = VolumeState.from_vector(values)
def properties(self) -> ThermodynamicProperties:
if self.state.m <= 0.0:
raise ValueError("pipe mass must stay positive")
temperature = self.gas.temperature_from_internal_energy(
self.state.U / self.state.m
)
density = self.state.m / self.volume
pressure = self.gas.pressure(density, temperature)
properties = ThermodynamicProperties(
p=pressure,
T=temperature,
rho=density,
u=self.state.U / self.state.m,
h=self.gas.specific_enthalpy(temperature),
)
self.port_1.p = pressure
self.port_1.h_outflow = properties.h
self.port_2.p = pressure
self.port_2.h_outflow = properties.h
return properties
def gas_mass_g(self) -> float:
return self.state.m * 1.0e3
def port_mass_flow(
self,
*,
port_pressure_pa: float,
port_temperature_k: float,
) -> float:
"""Return mass flow from an external port into the center storage."""
if port_pressure_pa <= 0.0:
raise ValueError("port_pressure_pa must be positive")
if port_temperature_k <= 0.0:
raise ValueError("port_temperature_k must be positive")
center = self.properties()
pressure_difference = port_pressure_pa - center.p
if pressure_difference == 0.0:
return 0.0
upstream_pressure = max(port_pressure_pa, center.p)
upstream_temperature = (
port_temperature_k if pressure_difference > 0.0 else center.T
)
density = self.gas.density(upstream_pressure, upstream_temperature)
magnitude = self._mass_flow_for_resistance_pressure_drop(
abs(pressure_difference),
density=density,
temperature=upstream_temperature,
)
return magnitude if pressure_difference > 0.0 else -magnitude
def _mass_flow_for_resistance_pressure_drop(
self,
pressure_drop_pa: float,
*,
density: float,
temperature: float,
) -> float:
original_length = self.length
self.length = self._resistance_length
try:
return self._mass_flow_for_pressure_drop(
pressure_drop_pa,
density=density,
temperature=temperature,
)
finally:
self.length = original_length
def diagnostics(
self,
*,
mass_flow_kg_s: float,
temperature_k: float | None = None,
) -> AmesimPnl0001Diagnostics:
properties = self.properties()
temperature = temperature_k or properties.T
reynolds = self._reynolds_number(mass_flow_kg_s, temperature)
friction_factor = self._friction_factor(reynolds)
velocity = mass_flow_kg_s / (properties.rho * self.area)
original_length = self.length
self.length = self._resistance_length
try:
pressure_drop = self._darcy_pressure_drop(
mass_flow_kg_s,
density=properties.rho,
temperature=temperature,
)
finally:
self.length = original_length
return AmesimPnl0001Diagnostics(
mass_flow_kg_s=mass_flow_kg_s,
reynolds_number=reynolds,
gas_velocity_m_s=velocity,
friction_factor=friction_factor,
pressure_drop_pa=pressure_drop,
)
def derivatives_from_connections(
self,
*,
port_1_m_flow: float,
connected_h_1: float,
port_2_m_flow: float,
connected_h_2: float,
) -> VolumeState:
center = self.properties()
inlet_h_1 = self.connection_inlet_enthalpy(
port_m_flow=port_1_m_flow,
connected_h=connected_h_1,
internal_h=center.h,
)
inlet_h_2 = self.connection_inlet_enthalpy(
port_m_flow=port_2_m_flow,
connected_h=connected_h_2,
internal_h=center.h,
)
heat_flow = (
self.heat_transfer_coefficient
* self.heat_transfer_area
* (self.external_temperature - center.T)
)
return VolumeState(
m=port_1_m_flow + port_2_m_flow,
U=port_1_m_flow * inlet_h_1 + port_2_m_flow * inlet_h_2 + heat_flow,
)
class AmesimPnl00rPipe(_DarcyPipeResistanceMixin, AlgebraicComponent):
"""First-pass AMESim ``PNL00R`` (R) pipe resistance."""
def __init__(
self,
name: str,
*,
diameter_mm: float,
length_m: float,
relative_roughness: float,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> None:
if diameter_mm <= 0.0:
raise ValueError("diameter_mm must be positive")
if length_m <= 0.0:
raise ValueError("length_m must be positive")
if relative_roughness < 0.0:
raise ValueError("relative_roughness must be non-negative")
super().__init__(name=name)
self.diameter = diameter_mm * 1.0e-3
self.length = length_m
self.relative_roughness = relative_roughness
self.gas = gas
self.area = diameter_mm_to_area_m2(diameter_mm)
self.port_1 = PortState()
self.port_2 = PortState()
def mass_flow(
self,
*,
port_1_pressure_pa: float,
port_1_temperature_k: float,
port_2_pressure_pa: float,
port_2_temperature_k: float,
) -> float:
"""Return mass flow from port 1 to port 2 in kg/s."""
if port_1_pressure_pa <= 0.0 or port_2_pressure_pa <= 0.0:
raise ValueError("port pressures must be positive")
if port_1_temperature_k <= 0.0 or port_2_temperature_k <= 0.0:
raise ValueError("port temperatures must be positive")
pressure_difference = port_1_pressure_pa - port_2_pressure_pa
if pressure_difference == 0.0:
return 0.0
upstream_pressure = max(port_1_pressure_pa, port_2_pressure_pa)
upstream_temperature = (
port_1_temperature_k
if pressure_difference > 0.0
else port_2_temperature_k
)
density = self.gas.density(upstream_pressure, upstream_temperature)
magnitude = self._mass_flow_for_pressure_drop(
abs(pressure_difference),
density=density,
temperature=upstream_temperature,
)
return magnitude if pressure_difference > 0.0 else -magnitude
def diagnostics(
self,
*,
mass_flow_kg_s: float,
pressure_pa: float,
temperature_k: float,
) -> AmesimPnl0001Diagnostics:
density = self.gas.density(pressure_pa, temperature_k)
reynolds = self._reynolds_number(mass_flow_kg_s, temperature_k)
friction_factor = self._friction_factor(reynolds)
velocity = mass_flow_kg_s / (density * self.area)
pressure_drop = self._darcy_pressure_drop(
mass_flow_kg_s,
density=density,
temperature=temperature_k,
)
return AmesimPnl0001Diagnostics(
mass_flow_kg_s=mass_flow_kg_s,
reynolds_number=reynolds,
gas_velocity_m_s=velocity,
friction_factor=friction_factor,
pressure_drop_pa=pressure_drop,
)
def helium_dynamic_viscosity(temperature_k: float) -> float:
"""Sutherland approximation centered on the test_mql initial condition."""
if temperature_k <= 0.0:
raise ValueError("temperature_k must be positive")
reference_temperature = 293.15
reference_viscosity = 2.0e-5
sutherland_constant = 79.4
return (
reference_viscosity
* (temperature_k / reference_temperature) ** 1.5
* (reference_temperature + sutherland_constant)
/ (temperature_k + sutherland_constant)
)
-100
View File
@@ -1,100 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from datetime import UTC, datetime
from pathlib import Path
from app.simulation.paths import PROJECT_ROOT, SIMULATION_RUNS_DIR
from app.simulation.examples.test_mql.system import (
TestMqlRunConfig,
TestMqlSimulationResult,
TestMqlSystem,
)
@dataclass(frozen=True)
class PreparedTestMqlRun:
run_config: TestMqlRunConfig
repo_root: Path
output_dir: Path
@dataclass(frozen=True)
class TestMqlRunResult:
run_config: TestMqlRunConfig
prepared_run: PreparedTestMqlRun
system: TestMqlSystem
result: TestMqlSimulationResult
summary_path: Path
def format_test_mql_summary(system: TestMqlSystem) -> str:
snapshot = system.snapshot()
lines = [
"Model: test_mql",
f"Source archive: {system.archive_path}",
f"Components: {snapshot.component_count}",
f"Connections: {snapshot.connection_count}",
f"Continuous states in AMESim modelinfo: {snapshot.continuous_state_count}",
f"Discrete states in AMESim modelinfo: {snapshot.discrete_state_count}",
"Global parameters:",
]
for name, value in sorted(snapshot.global_parameters.items()):
lines.append(f" - {name}: {value}")
lines.append("Component submodels:")
for name, count in sorted(snapshot.submodel_counts.items()):
lines.append(f" - {name}: {count}")
return "\n".join(lines) + "\n"
def _default_run_output_dir() -> Path:
timestamp = datetime.now(UTC).strftime("test_mql_%Y%m%d_%H%M%S_%f")
return SIMULATION_RUNS_DIR / timestamp
def prepare_test_mql_run(
*,
run_config: TestMqlRunConfig | None = None,
output_dir: Path | None = None,
) -> PreparedTestMqlRun:
return PreparedTestMqlRun(
run_config=run_config or TestMqlRunConfig(),
repo_root=PROJECT_ROOT,
output_dir=output_dir or _default_run_output_dir(),
)
def run_prepared_test_mql(prepared_run: PreparedTestMqlRun) -> TestMqlRunResult:
system = TestMqlSystem()
result = system.simulate(prepared_run.run_config)
prepared_run.output_dir.mkdir(parents=True, exist_ok=True)
summary_path = prepared_run.output_dir / "test_mql_model_summary.txt"
summary_path.write_text(format_test_mql_summary(system), encoding="utf-8")
return TestMqlRunResult(
run_config=prepared_run.run_config,
prepared_run=prepared_run,
system=system,
result=result,
summary_path=summary_path,
)
def run_test_mql(
*,
run_config: TestMqlRunConfig | None = None,
output_dir: Path | None = None,
) -> TestMqlRunResult:
return run_prepared_test_mql(
prepare_test_mql_run(run_config=run_config, output_dir=output_dir)
)
def main() -> None:
run = run_test_mql()
print(format_test_mql_summary(run.system), end="")
print(f"Samples: {len(run.result.t)}")
print(f"Output directory: {run.prepared_run.output_dir}")
if __name__ == "__main__":
main()
@@ -1,80 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass, field
from datetime import UTC, datetime
from pathlib import Path
from app.simulation.examples.test_mql.baseline import (
TestMqlBaselineRun,
run_test_mql_baseline_passthrough,
)
from app.simulation.paths import (
AMESIM_TEST_MQL_ARCHIVE_PATH,
SIMULATION_RUNS_DIR,
)
@dataclass(frozen=True)
class TestMqlBaselinePathConfig:
archive_path: Path = field(
default_factory=lambda: AMESIM_TEST_MQL_ARCHIVE_PATH
)
output_dir: Path | None = None
@dataclass(frozen=True)
class TestMqlBaselineExecutionConfig:
write_summary: bool = True
data_paths: tuple[str, ...] | None = None
@dataclass(frozen=True)
class TestMqlBaselineScriptConfig:
paths: TestMqlBaselinePathConfig = field(default_factory=TestMqlBaselinePathConfig)
execution: TestMqlBaselineExecutionConfig = field(default_factory=TestMqlBaselineExecutionConfig)
def _default_output_dir() -> Path:
timestamp = datetime.now(UTC).strftime("test_mql_baseline_%Y%m%d_%H%M%S_%f")
return SIMULATION_RUNS_DIR / timestamp
def format_test_mql_baseline_summary(run: TestMqlBaselineRun) -> str:
return "\n".join(
[
"Model: test_mql",
"Mode: AMESim baseline passthrough",
f"Samples: {run.sample_count}",
f"Output schema signals: {run.output_schema.signal_count}",
f"Compared signals: {run.signal_count}",
f"Observation bindings: {run.observation_catalog.binding_count}",
f"Max absolute error: {run.comparison.max_abs_error}",
f"Max relative error: {run.comparison.max_rel_error}",
]
) + "\n"
def run_test_mql_baseline(config: TestMqlBaselineScriptConfig | None = None):
config = config or TestMqlBaselineScriptConfig()
run = run_test_mql_baseline_passthrough(
config.paths.archive_path,
data_paths=config.execution.data_paths,
)
output_dir = config.paths.output_dir or _default_output_dir()
if config.execution.write_summary:
output_dir.mkdir(parents=True, exist_ok=True)
(output_dir / "test_mql_baseline_summary.txt").write_text(
format_test_mql_baseline_summary(run),
encoding="utf-8",
)
return run, output_dir
def main() -> None:
run, output_dir = run_test_mql_baseline()
print(format_test_mql_baseline_summary(run), end="")
print(f"Output directory: {output_dir}")
if __name__ == "__main__":
main()
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@@ -1,18 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.solvers.solver import (
SolveIVPConfig as _BaseSolveIVPConfig,
integrate_ode,
)
@dataclass(frozen=True)
class SolveIVPConfig(_BaseSolveIVPConfig):
"""Solver defaults used by the calibrated ``test_mql`` example."""
atol: float = 1e-10
__all__ = ["SolveIVPConfig", "integrate_ode"]
@@ -1,78 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.core.base import Component, DynamicComponent
@dataclass(frozen=True)
class Connection:
source_component: str
source_port: str
target_component: str
target_port: str
class SimulationNetwork:
"""Container for components, topology, and state-vector bookkeeping."""
def __init__(self, name: str) -> None:
self.name = name
self.components: dict[str, Component] = {}
self.connections: list[Connection] = []
def add_component(self, component: Component) -> None:
if component.name in self.components:
raise ValueError(f"Duplicate component name: {component.name}")
self.components[component.name] = component
def connect(
self,
source_component: str,
source_port: str,
target_component: str,
target_port: str,
) -> None:
self.connections.append(
Connection(
source_component=source_component,
source_port=source_port,
target_component=target_component,
target_port=target_port,
)
)
def dynamic_components(self) -> list[DynamicComponent]:
return [
component
for component in self.components.values()
if isinstance(component, DynamicComponent)
]
def initial_state_vector(self) -> list[float]:
values: list[float] = []
for component in self.dynamic_components():
values.extend(component.get_state_vector())
return values
def apply_state_vector(self, values: list[float]) -> None:
cursor = 0
for component in self.dynamic_components():
next_cursor = cursor + component.state_size
component.set_state_vector(values[cursor:next_cursor])
cursor = next_cursor
if cursor != len(values):
raise ValueError("State vector length does not match dynamic components.")
def summary(self) -> str:
lines = [f"Network: {self.name}", "Components:"]
for name, component in self.components.items():
lines.append(f" - {name}: {component.__class__.__name__}")
lines.append("Connections:")
for conn in self.connections:
lines.append(
f" - {conn.source_component}.{conn.source_port}"
f" -> {conn.target_component}.{conn.target_port}"
)
return "\n".join(lines)
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@@ -1,118 +0,0 @@
from __future__ import annotations
import re
import tarfile
import xml.etree.ElementTree as ET
from dataclasses import dataclass
from pathlib import Path
@dataclass(frozen=True)
class TestMqlComponentContact:
component_a: str
port_a: str
component_b: str
port_b: str
def other_endpoint(self, component_alias: str) -> tuple[str, str]:
if component_alias == self.component_a:
return self.component_b, self.port_b
if component_alias == self.component_b:
return self.component_a, self.port_a
raise KeyError(component_alias)
def port_for(self, component_alias: str) -> str:
if component_alias == self.component_a:
return self.port_a
if component_alias == self.component_b:
return self.port_b
raise KeyError(component_alias)
@dataclass(frozen=True)
class TestMqlCirTopology:
component_contacts: tuple[TestMqlComponentContact, ...]
def contacts_for(self, component_alias: str) -> tuple[TestMqlComponentContact, ...]:
return tuple(
contact
for contact in self.component_contacts
if component_alias in (contact.component_a, contact.component_b)
)
def load_test_mql_cir_topology(
archive_path: str | Path,
*,
cir_member: str = "test_mql_.cir",
) -> TestMqlCirTopology:
with tarfile.open(archive_path) as archive:
cir_file = archive.extractfile(cir_member)
if cir_file is None:
raise ValueError(f"Missing AMESim circuit member: {cir_member}")
cir_text = cir_file.read().decode("latin1")
root = ET.fromstring(_topology_only_xml(cir_text))
components = root.findall(".//COMPS_LIST/COMP")
aliases = tuple(_required_text(component, "ALIAS") for component in components)
contacts: dict[
tuple[tuple[int, int], tuple[int, int]],
TestMqlComponentContact,
] = {}
directed_contacts: set[tuple[tuple[int, int], tuple[int, int]]] = set()
for component_index, component in enumerate(components):
ports = component.findall("./COMP_PORTS_LIST/COMP_PORT")
for port_index, port in enumerate(ports):
if port.findtext("PORT_CONNECT") != "1":
continue
for connection in port.findall("./CONNECT_LIST/CONNECT"):
target_index = int(_required_text(connection, "CONNECT_ENTITY_NUM"))
target_port_index = int(_required_text(connection, "CONNECT_ENTITY_PORT"))
if target_index < 0 or target_index >= len(components):
raise ValueError(f"Component contact references unknown entity {target_index}")
target_ports = components[target_index].findall("./COMP_PORTS_LIST/COMP_PORT")
if target_port_index < 0 or target_port_index >= len(target_ports):
raise ValueError(
f"Component contact references unknown port {target_port_index} "
f"on {aliases[target_index]}"
)
endpoint = (component_index, port_index)
target_endpoint = (target_index, target_port_index)
directed_contacts.add((endpoint, target_endpoint))
key = tuple(sorted((endpoint, target_endpoint)))
first, second = key
contacts[key] = TestMqlComponentContact(
component_a=aliases[first[0]],
port_a=f"port_{first[1] + 1}",
component_b=aliases[second[0]],
port_b=f"port_{second[1] + 1}",
)
for endpoint, target_endpoint in directed_contacts:
if (target_endpoint, endpoint) not in directed_contacts:
raise ValueError(
"AMESim component contact is not reciprocal: "
f"{endpoint} -> {target_endpoint}"
)
return TestMqlCirTopology(component_contacts=tuple(contacts.values()))
def _topology_only_xml(cir_text: str) -> str:
# AMESim expressions inside SUBMODEL contain unescaped && and <= operators.
# Topology lives outside those blocks, so omit them before XML parsing.
return re.sub(
r"<SUBMODEL>.*?</SUBMODEL>",
"<SUBMODEL />",
cir_text,
flags=re.DOTALL,
)
def _required_text(element: ET.Element, child_name: str) -> str:
value = element.findtext(child_name)
if value is None:
raise ValueError(f"Missing AMESim circuit element: {child_name}")
return value
@@ -1 +0,0 @@
"""Legacy TestModel reference system."""
@@ -1,668 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass, field
from typing import Callable
from app.simulation.components.experimental.flow.orifice import Orifice
from app.simulation.examples.testmodel.dynamic_pipe import Pipe
from app.simulation.components.experimental.junctions.tee import Tee
from app.simulation.components.experimental.storage.cylinder import Cylinder
from app.simulation.components.experimental.storage.tank import Tank
from app.simulation.core.medium import IdealGasMedium, ThermodynamicProperties
from app.simulation.core.state import VolumeState
@dataclass(frozen=True)
class BranchInletFlowDiagnostics:
converged: bool
iterations: int
residual: float
m_flow: float
inlet_pressure: float
@dataclass(frozen=True)
class DownstreamPressureDiagnostics:
converged: bool
iterations: int
residual: float
pressure: float
target_total_internal_energy: float
@dataclass(frozen=True)
class TestModelSolveDiagnostics:
upper_branch_inlet: BranchInletFlowDiagnostics
lower_branch_inlet: BranchInletFlowDiagnostics
downstream_pressure_projection: DownstreamPressureDiagnostics | None
@dataclass(frozen=True)
class BranchClosureComponents:
name: str
orifice: Orifice
pipe: Pipe
@dataclass(frozen=True)
class BranchClosureState:
name: str
pipe: ThermodynamicProperties
inlet_flow: float
outlet_flow: float
inlet_h: float
inlet_flow_diagnostics: BranchInletFlowDiagnostics
@dataclass(frozen=True)
class BranchSnapshot:
name: str
pipe: ThermodynamicProperties
inlet_flow: float
outlet_flow: float
inlet_h: float
inlet_flow_diagnostics: BranchInletFlowDiagnostics
@dataclass(frozen=True)
class TestModelSnapshot:
cylinder: ThermodynamicProperties
tank: ThermodynamicProperties
tee_upstream_h: float
tee_downstream_h: float
branches: tuple[BranchSnapshot, ...] = field(default_factory=tuple)
solve_diagnostics: TestModelSolveDiagnostics | None = None
@property
def pipe_upper(self) -> ThermodynamicProperties:
return self.branches[0].pipe
@property
def pipe_lower(self) -> ThermodynamicProperties:
return self.branches[1].pipe
@property
def branch_inlet_flows(self) -> tuple[float, ...]:
return tuple(branch.inlet_flow for branch in self.branches)
@property
def branch_outlet_flows(self) -> tuple[float, ...]:
return tuple(branch.outlet_flow for branch in self.branches)
@dataclass(frozen=True)
class InitializationDiagnostics:
converged: bool
iterations: int
max_state_delta: float
max_flow_delta: float
max_enthalpy_delta: float
downstream_pressure_spread: float
state_vector: tuple[float, ...]
@dataclass(frozen=True)
class TestModelClosureComponents:
cylinder: Cylinder
upstream_tee: Tee
upper_branch: BranchClosureComponents
lower_branch: BranchClosureComponents
downstream_tee: Tee
tank: Tank
def branches(self) -> tuple[BranchClosureComponents, BranchClosureComponents]:
return (self.upper_branch, self.lower_branch)
class TestModelClosure:
"""Owns Testmodel-specific closure, projection and port-writeback logic."""
def __init__(
self,
*,
medium: IdealGasMedium,
components: TestModelClosureComponents,
initial_state_vector: Callable[[], list[float]],
apply_state_vector: Callable[[list[float]], None],
) -> None:
self.medium = medium
self.components = components
self._initial_state_vector = initial_state_vector
self._apply_state_vector = apply_state_vector
self.last_solve_diagnostics: TestModelSolveDiagnostics | None = None
self.last_downstream_pressure_diagnostics: DownstreamPressureDiagnostics | None = None
@staticmethod
def _downstream_pressure_spread(snapshot: TestModelSnapshot) -> float:
downstream_pressures = tuple(branch.pipe.p for branch in snapshot.branches) + (
snapshot.tank.p,
)
return max(downstream_pressures) - min(downstream_pressures)
@staticmethod
def _initialization_flow_delta(
previous_snapshot: TestModelSnapshot | None,
current_snapshot: TestModelSnapshot,
) -> float:
if previous_snapshot is None:
return max(abs(branch.outlet_flow) for branch in current_snapshot.branches)
return max(
abs(curr - prev)
for curr, prev in zip(
current_snapshot.branch_outlet_flows,
previous_snapshot.branch_outlet_flows,
)
)
@staticmethod
def _initialization_enthalpy_delta(
previous_snapshot: TestModelSnapshot | None,
current_snapshot: TestModelSnapshot,
) -> float:
if previous_snapshot is None:
return abs(current_snapshot.tee_downstream_h - current_snapshot.tank.h)
return max(
abs(current_snapshot.tee_upstream_h - previous_snapshot.tee_upstream_h),
abs(current_snapshot.tee_downstream_h - previous_snapshot.tee_downstream_h),
)
def consistent_initial_state_vector(self) -> list[float]:
return list(self.initialize_consistent_state().state_vector)
def initialize_consistent_state(
self,
max_iterations: int = 12,
state_tolerance: float = 1e-9,
flow_tolerance: float = 1e-9,
enthalpy_tolerance: float = 1e-6,
pressure_tolerance: float = 1e-6,
strict_internal_solvers: bool = False,
) -> InitializationDiagnostics:
raw_state = self._initial_state_vector()
previous_snapshot: TestModelSnapshot | None = None
diagnostics: InitializationDiagnostics | None = None
for iteration in range(1, max_iterations + 1):
state_before_projection = self._initial_state_vector()
self.snapshot(state_before_projection, strict=strict_internal_solvers)
self.project_downstream_pressure_constraints(strict=strict_internal_solvers)
state_after_projection = self._initial_state_vector()
snapshot_after_projection = self.snapshot(
state_after_projection,
strict=strict_internal_solvers,
)
max_state_delta = max(
abs(after - before)
for before, after in zip(state_before_projection, state_after_projection)
)
max_flow_delta = self._initialization_flow_delta(
previous_snapshot,
snapshot_after_projection,
)
max_enthalpy_delta = self._initialization_enthalpy_delta(
previous_snapshot,
snapshot_after_projection,
)
downstream_pressure_spread = self._downstream_pressure_spread(
snapshot_after_projection,
)
diagnostics = InitializationDiagnostics(
converged=(
max_state_delta <= state_tolerance
and max_flow_delta <= flow_tolerance
and max_enthalpy_delta <= enthalpy_tolerance
and downstream_pressure_spread <= pressure_tolerance
),
iterations=iteration,
max_state_delta=max_state_delta,
max_flow_delta=max_flow_delta,
max_enthalpy_delta=max_enthalpy_delta,
downstream_pressure_spread=downstream_pressure_spread,
state_vector=tuple(state_after_projection),
)
previous_snapshot = snapshot_after_projection
if diagnostics.converged:
self._apply_state_vector(raw_state)
return diagnostics
assert diagnostics is not None
self._apply_state_vector(raw_state)
return diagnostics
def _solve_branch_inlet_flow(
self,
orifice: Orifice,
pipe: Pipe,
p_upstream: float,
pipe_props: ThermodynamicProperties,
*,
strict: bool = False,
) -> tuple[float, BranchInletFlowDiagnostics]:
m_flow = orifice.mass_flow(p_upstream, pipe_props.p)
rho = max(pipe_props.rho, 1e-9)
p_inlet = pipe.inlet_pressure(m_flow, rho, pipe_props.p)
residual = abs(orifice.mass_flow(p_upstream, p_inlet) - m_flow)
converged = False
iterations = 0
for iteration in range(1, 9):
p_inlet = pipe.inlet_pressure(m_flow, rho, pipe_props.p)
next_m_flow = orifice.mass_flow(p_upstream, p_inlet)
residual = abs(next_m_flow - m_flow)
iterations = iteration
if residual <= 1e-9 * max(1.0, abs(next_m_flow)):
m_flow = next_m_flow
converged = True
break
m_flow = next_m_flow
diagnostics = BranchInletFlowDiagnostics(
converged=converged,
iterations=iterations,
residual=residual,
m_flow=m_flow,
inlet_pressure=p_inlet,
)
if strict and not diagnostics.converged:
raise RuntimeError(
f"Branch inlet flow solve did not converge for {pipe.name}: residual={residual:.6e}"
)
return m_flow, diagnostics
def _solve_downstream_branch_flows(
self,
cylinder: ThermodynamicProperties,
tank: ThermodynamicProperties,
branch_states: tuple[BranchClosureState, BranchClosureState],
) -> tuple[float, float]:
return self._solve_downstream_branch_flows_from_state(
inlet_h_upper=branch_states[0].inlet_h,
inlet_h_lower=branch_states[1].inlet_h,
pipe_upper_h=max(branch_states[0].pipe.h, 1e-9),
pipe_lower_h=max(branch_states[1].pipe.h, 1e-9),
tank_h=max(tank.h, 1e-9),
q_in_upper=branch_states[0].inlet_flow,
q_in_lower=branch_states[1].inlet_flow,
)
def _project_volume_energy_to_pressure(
self,
component: Pipe | Tank,
target_pressure: float,
) -> None:
target_temperature = target_pressure * component.V / (
max(component.state.m, 1e-12) * self.medium.R_gas
)
target_internal_energy = (
component.state.m * self.medium.specific_internal_energy(target_temperature)
)
component.state = VolumeState(m=component.state.m, U=target_internal_energy)
def _downstream_total_internal_energy_for_pressure(
self,
target_pressure: float,
downstream_components: tuple[Pipe | Tank, ...],
) -> float:
total_internal_energy = 0.0
for component in downstream_components:
target_temperature = target_pressure * component.V / (
max(component.state.m, 1e-12) * self.medium.R_gas
)
total_internal_energy += (
component.state.m * self.medium.specific_internal_energy(target_temperature)
)
return total_internal_energy
def _solve_downstream_common_pressure(
self,
downstream_components: tuple[Pipe | Tank, ...],
target_total_internal_energy: float,
*,
strict: bool = False,
) -> tuple[float, DownstreamPressureDiagnostics]:
lower_pressure = 1.0
upper_pressure = max(component.properties().p for component in downstream_components)
upper_pressure = max(upper_pressure, 1e5)
def residual(pressure: float) -> float:
return (
self._downstream_total_internal_energy_for_pressure(
pressure,
downstream_components,
)
- target_total_internal_energy
)
upper_residual = residual(upper_pressure)
iteration_count = 0
while upper_residual < 0.0:
upper_pressure *= 2.0
upper_residual = residual(upper_pressure)
final_pressure = 0.5 * (lower_pressure + upper_pressure)
final_residual = residual(final_pressure)
converged = False
for iteration in range(1, 81):
middle_pressure = 0.5 * (lower_pressure + upper_pressure)
middle_residual = residual(middle_pressure)
iteration_count = iteration
final_pressure = middle_pressure
final_residual = middle_residual
if abs(middle_residual) <= 1e-12 * max(1.0, target_total_internal_energy):
converged = True
break
if middle_residual > 0.0:
upper_pressure = middle_pressure
else:
lower_pressure = middle_pressure
diagnostics = DownstreamPressureDiagnostics(
converged=converged,
iterations=iteration_count,
residual=final_residual,
pressure=final_pressure,
target_total_internal_energy=target_total_internal_energy,
)
if strict and not diagnostics.converged:
raise RuntimeError(
"Downstream common-pressure solve did not converge: "
f"residual={final_residual:.6e}"
)
return final_pressure, diagnostics
def project_downstream_pressure_constraints(self, *, strict: bool = False) -> None:
downstream_components = (
self.components.upper_branch.pipe,
self.components.lower_branch.pipe,
self.components.tank,
)
total_internal_energy = sum(component.state.U for component in downstream_components)
common_pressure, diagnostics = self._solve_downstream_common_pressure(
downstream_components,
total_internal_energy,
strict=strict,
)
self.last_downstream_pressure_diagnostics = diagnostics
for component in downstream_components:
self._project_volume_energy_to_pressure(component, common_pressure)
def _downstream_connection_enthalpy(
self,
q_out_upper: float,
q_out_lower: float,
pipe_upper_h: float,
pipe_lower_h: float,
tank_h: float,
) -> float:
return self.components.downstream_tee.inlet_stream_enthalpy(
q_out_lower,
pipe_lower_h,
q_out_upper,
pipe_upper_h,
fallback_h=tank_h,
)
def _solve_downstream_branch_flows_from_state(
self,
*,
inlet_h_upper: float,
inlet_h_lower: float,
pipe_upper_h: float,
pipe_lower_h: float,
tank_h: float,
q_in_upper: float,
q_in_lower: float,
) -> tuple[float, float]:
return self.components.downstream_tee.solve_branch_outlet_flows_from_energy_balance(
ratio_branch1=self.components.upper_branch.pipe.V / self.components.tank.V,
ratio_branch2=self.components.lower_branch.pipe.V / self.components.tank.V,
inlet_h_branch1=inlet_h_upper,
inlet_h_branch2=inlet_h_lower,
branch1_h=pipe_upper_h,
branch2_h=pipe_lower_h,
inlet_h=tank_h,
q_in_branch1=q_in_upper,
q_in_branch2=q_in_lower,
)
def _evaluate_branch_states(
self,
cylinder: ThermodynamicProperties,
) -> tuple[BranchClosureState, BranchClosureState]:
states: list[BranchClosureState] = []
for branch in self.components.branches():
pipe_properties = branch.pipe.properties()
inlet_flow, inlet_flow_diagnostics = self._solve_branch_inlet_flow(
branch.orifice,
branch.pipe,
cylinder.p,
pipe_properties,
)
inlet_h = branch.pipe.port_a_inlet_enthalpy(
port_a_m_flow=inlet_flow,
connected_h=cylinder.h,
internal_h=pipe_properties.h,
)
states.append(
BranchClosureState(
name=branch.name,
pipe=pipe_properties,
inlet_flow=inlet_flow,
outlet_flow=0.0,
inlet_h=inlet_h,
inlet_flow_diagnostics=inlet_flow_diagnostics,
)
)
return (states[0], states[1])
@staticmethod
def _with_branch_outlet_flows(
branch_states: tuple[BranchClosureState, BranchClosureState],
outlet_flows: tuple[float, float],
) -> tuple[BranchClosureState, BranchClosureState]:
return (
BranchClosureState(
name=branch_states[0].name,
pipe=branch_states[0].pipe,
inlet_flow=branch_states[0].inlet_flow,
outlet_flow=outlet_flows[0],
inlet_h=branch_states[0].inlet_h,
inlet_flow_diagnostics=branch_states[0].inlet_flow_diagnostics,
),
BranchClosureState(
name=branch_states[1].name,
pipe=branch_states[1].pipe,
inlet_flow=branch_states[1].inlet_flow,
outlet_flow=outlet_flows[1],
inlet_h=branch_states[1].inlet_h,
inlet_flow_diagnostics=branch_states[1].inlet_flow_diagnostics,
),
)
@staticmethod
def _branch_snapshots(
branch_states: tuple[BranchClosureState, BranchClosureState],
) -> tuple[BranchSnapshot, BranchSnapshot]:
return (
BranchSnapshot(
name=branch_states[0].name,
pipe=branch_states[0].pipe,
inlet_flow=branch_states[0].inlet_flow,
outlet_flow=branch_states[0].outlet_flow,
inlet_h=branch_states[0].inlet_h,
inlet_flow_diagnostics=branch_states[0].inlet_flow_diagnostics,
),
BranchSnapshot(
name=branch_states[1].name,
pipe=branch_states[1].pipe,
inlet_flow=branch_states[1].inlet_flow,
outlet_flow=branch_states[1].outlet_flow,
inlet_h=branch_states[1].inlet_h,
inlet_flow_diagnostics=branch_states[1].inlet_flow_diagnostics,
),
)
def snapshot(
self,
state_vector: list[float] | None = None,
*,
strict: bool = False,
) -> TestModelSnapshot:
if state_vector is not None:
self._apply_state_vector(list(state_vector))
cylinder = self.components.cylinder.properties()
tank = self.components.tank.properties()
branch_states = self._evaluate_branch_states(cylinder)
if strict:
for branch_state in branch_states:
if not branch_state.inlet_flow_diagnostics.converged:
raise RuntimeError(
"Branch inlet flow solve did not converge for "
f"{branch_state.name}: residual="
f"{branch_state.inlet_flow_diagnostics.residual:.6e}"
)
outlet_flows = self._solve_downstream_branch_flows(cylinder, tank, branch_states)
branch_states = self._with_branch_outlet_flows(branch_states, outlet_flows)
tee_upstream_h = self.components.upstream_tee.inlet_stream_enthalpy(
-branch_states[0].inlet_flow,
branch_states[0].pipe.h,
-branch_states[1].inlet_flow,
branch_states[1].pipe.h,
fallback_h=cylinder.h,
)
tee_downstream_h = self._downstream_connection_enthalpy(
branch_states[0].outlet_flow,
branch_states[1].outlet_flow,
branch_states[0].pipe.h,
branch_states[1].pipe.h,
tank.h,
)
self._write_port_states(
cylinder,
tank,
branch_states,
tee_upstream_h,
tee_downstream_h,
)
solve_diagnostics = TestModelSolveDiagnostics(
upper_branch_inlet=branch_states[0].inlet_flow_diagnostics,
lower_branch_inlet=branch_states[1].inlet_flow_diagnostics,
downstream_pressure_projection=self.last_downstream_pressure_diagnostics,
)
self.last_solve_diagnostics = solve_diagnostics
branch_snapshots = self._branch_snapshots(branch_states)
return TestModelSnapshot(
cylinder=cylinder,
tank=tank,
tee_upstream_h=tee_upstream_h,
tee_downstream_h=tee_downstream_h,
branches=branch_snapshots,
solve_diagnostics=solve_diagnostics,
)
def _write_port_states(
self,
cylinder: ThermodynamicProperties,
tank: ThermodynamicProperties,
branch_states: tuple[BranchClosureState, BranchClosureState],
tee_upstream_h: float,
tee_downstream_h: float,
) -> None:
cylinder_m_flow = -sum(branch_state.inlet_flow for branch_state in branch_states)
tank_m_flow = sum(branch_state.outlet_flow for branch_state in branch_states)
self.components.cylinder.port_b.m_flow = cylinder_m_flow
self.components.upstream_tee.port_in.p = cylinder.p
self.components.upstream_tee.port_out1.p = cylinder.p
self.components.upstream_tee.port_out2.p = cylinder.p
self.components.upstream_tee.port_in.m_flow = -cylinder_m_flow
self.components.upstream_tee.port_in.h_outflow = tee_upstream_h
self.components.upstream_tee.port_out1.h_outflow = cylinder.h
self.components.upstream_tee.port_out2.h_outflow = cylinder.h
self.components.upstream_tee.port_out1.m_flow = -branch_states[0].inlet_flow
self.components.upstream_tee.port_out2.m_flow = -branch_states[1].inlet_flow
for branch_components, branch_state in zip(self.components.branches(), branch_states):
branch_components.orifice.port_a.p = cylinder.p
branch_components.orifice.port_b.p = branch_components.pipe.inlet_pressure(
branch_state.inlet_flow,
max(branch_state.pipe.rho, 1e-9),
branch_state.pipe.p,
)
branch_components.orifice.port_a.m_flow = branch_state.inlet_flow
branch_components.orifice.port_b.m_flow = -branch_state.inlet_flow
branch_components.orifice.port_a.h_outflow = cylinder.h
branch_components.orifice.port_b.h_outflow = branch_state.pipe.h
branch_components.pipe.port_a.p = branch_components.orifice.port_b.p
branch_components.pipe.port_a.m_flow = branch_state.inlet_flow
branch_components.pipe.port_b.m_flow = -branch_state.outlet_flow
branch_components.pipe.port_b.p = branch_state.pipe.p
self.components.downstream_tee.port_in.p = tank.p
self.components.downstream_tee.port_out1.p = tank.p
self.components.downstream_tee.port_out2.p = tank.p
self.components.downstream_tee.port_in.m_flow = -tank_m_flow
self.components.downstream_tee.port_out1.m_flow = branch_states[1].outlet_flow
self.components.downstream_tee.port_out2.m_flow = branch_states[0].outlet_flow
self.components.downstream_tee.port_in.h_outflow = tee_downstream_h
self.components.downstream_tee.port_out1.h_outflow = tank.h
self.components.downstream_tee.port_out2.h_outflow = tank.h
self.components.tank.port_a.m_flow = tank_m_flow
def _branch_derivative_states(
self,
snapshot: TestModelSnapshot,
) -> tuple[VolumeState, VolumeState]:
derivative_states: list[VolumeState] = []
for branch_components, branch_snapshot in zip(self.components.branches(), snapshot.branches):
derivative_states.append(
branch_components.pipe.derivatives_from_connections(
port_a_m_flow=branch_snapshot.inlet_flow,
connected_h_a=snapshot.cylinder.h,
port_b_m_flow=-branch_snapshot.outlet_flow,
connected_h_b=snapshot.tank.h,
internal_h=branch_snapshot.pipe.h,
)
)
return (derivative_states[0], derivative_states[1])
def rhs(self, state_vector: list[float]) -> list[float]:
snapshot = self.snapshot(state_vector)
cylinder_m_flow = -sum(branch.inlet_flow for branch in snapshot.branches)
tank_m_flow = sum(branch.outlet_flow for branch in snapshot.branches)
d_cylinder = self.components.cylinder.derivatives_from_connection(
connected_h=snapshot.tee_upstream_h,
port_m_flow=cylinder_m_flow,
internal_h=snapshot.cylinder.h,
)
branch_derivatives = self._branch_derivative_states(snapshot)
d_tank = self.components.tank.derivatives_from_connection(
connected_h=snapshot.tee_downstream_h,
port_m_flow=tank_m_flow,
internal_h=snapshot.tank.h,
)
return [
d_cylinder.m,
d_cylinder.U,
branch_derivatives[0].m,
branch_derivatives[0].U,
branch_derivatives[1].m,
branch_derivatives[1].U,
d_tank.m,
d_tank.U,
]
@@ -1,272 +0,0 @@
from __future__ import annotations
from collections.abc import Mapping
from app.simulation.core.base import ThermodynamicVolumeComponent
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import (
ParameterDefinition,
THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
)
from app.simulation.core.medium import IdealGasMedium, ThermodynamicProperties
from app.simulation.core.ports import PortDefinition
from app.simulation.core.state import VolumeState
class Pipe(ThermodynamicVolumeComponent):
"""Dynamic pipe retained for the fixed TestModel compatibility example."""
MODEL_TYPE = "pipe"
MODEL_VERSION = "0.1.0"
PORTS = (
PortDefinition.pneumatic("port_a", nominal_role="inlet"),
PortDefinition.pneumatic("port_b", nominal_role="outlet"),
)
PARAMETERS = (
ParameterDefinition(
"length",
5.0,
label="长度",
quantity="length",
unit="m",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"diameter",
0.02,
label="直径",
quantity="length",
unit="m",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"lambda_darcy",
0.02,
label="摩阻系数",
minimum=0.0,
),
ParameterDefinition(
"p0",
1e5,
label="初始压力",
quantity="pressure",
unit="Pa",
minimum=0.0,
minimum_exclusive=True,
),
ParameterDefinition(
"T0",
300.0,
label="初始温度",
quantity="temperature",
unit="K",
minimum=0.0,
minimum_exclusive=True,
),
)
RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
def __init__(
self,
name: str,
medium: IdealGasMedium,
L: float = 5.0,
D: float = 0.02,
lambda_darcy: float = 0.02,
p0: float = 1e5,
T0: float = 300.0,
) -> None:
super().__init__(name=name)
self.set_parameter_values(
{
"length": L,
"diameter": D,
"lambda_darcy": lambda_darcy,
"p0": p0,
"T0": T0,
}
)
self.medium = medium
self.L = L
self.D = D
self.lambda_darcy = lambda_darcy
self.area = 3.141592653589793 * D * D / 4.0
self.V = self.area * L
m0 = p0 * self.V / (medium.R_gas * T0)
U0 = m0 * medium.specific_internal_energy(T0)
self.state = VolumeState(m=m0, U=U0)
self.port_a = self.register_declared_port("port_a")
self.port_b = self.register_declared_port("port_b")
@classmethod
def create(
cls,
*,
name: str,
medium: IdealGasMedium,
parameters: Mapping[str, float],
) -> Pipe:
return cls(
name=name,
medium=medium,
L=parameters["length"],
D=parameters["diameter"],
lambda_darcy=parameters["lambda_darcy"],
p0=parameters["p0"],
T0=parameters["T0"],
)
def get_state_vector(self) -> list[float]:
return self.state.as_vector()
def set_state_vector(self, values: list[float]) -> None:
self.state = VolumeState.from_vector(values)
def properties(self) -> ThermodynamicProperties:
props = self.medium.properties_from_mU(self.state.m, self.state.U, self.V)
self.port_b.p = props.p
self.port_a.h_outflow = props.h
self.port_b.h_outflow = props.h
return props
def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
return self.properties()
def state_derivative_from_ports(
self,
connected_h: Mapping[str, float],
) -> list[float]:
properties = self.properties()
derivative = self.derivatives_from_connections(
port_a_m_flow=self.port_a.m_flow,
connected_h_a=connected_h["port_a"],
port_b_m_flow=self.port_b.m_flow,
connected_h_b=connected_h["port_b"],
internal_h=properties.h,
)
return derivative.as_vector()
def inlet_pressure(self, m_flow_a: float, rho: float, core_pressure: float) -> float:
resistance = self.lambda_darcy * (self.L / self.D)
dynamic_term = m_flow_a * abs(m_flow_a) / (2.0 * rho * self.area * self.area)
return core_pressure + resistance * dynamic_term
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
properties = self.medium.properties_from_mU(
self.state.m,
self.state.U,
self.V,
)
expected_inlet_pressure = self.inlet_pressure(
self.port_a.m_flow,
max(properties.rho, 1e-12),
properties.p,
)
return (
EquationResidual(
id=f"{self.name}:darcy_pressure_loss",
owner="component",
owner_id=self.name,
relation="constitutive",
variables=(
f"{self.name}.port_a.p",
f"{self.name}.port_a.m_flow",
f"{self.name}.state",
),
role="effort",
value=self.port_a.p - expected_inlet_pressure,
),
EquationResidual(
id=f"{self.name}:port_b_pressure_state",
owner="component",
owner_id=self.name,
relation="state",
variables=(f"{self.name}.port_b.p", f"{self.name}.state"),
role="effort",
value=self.port_b.p - properties.p,
),
)
def port_a_inlet_enthalpy(
self,
*,
port_a_m_flow: float,
connected_h: float,
internal_h: float,
) -> float:
return self.connection_inlet_enthalpy(
port_m_flow=port_a_m_flow,
connected_h=connected_h,
internal_h=internal_h,
)
def port_b_inlet_enthalpy(
self,
*,
port_b_m_flow: float,
connected_h: float,
internal_h: float,
) -> float:
return self.connection_inlet_enthalpy(
port_m_flow=port_b_m_flow,
connected_h=connected_h,
internal_h=internal_h,
)
def connection_inlet_enthalpies(
self,
*,
port_a_m_flow: float,
connected_h_a: float,
port_b_m_flow: float,
connected_h_b: float,
internal_h: float,
) -> tuple[float, float]:
return (
self.port_a_inlet_enthalpy(
port_a_m_flow=port_a_m_flow,
connected_h=connected_h_a,
internal_h=internal_h,
),
self.port_b_inlet_enthalpy(
port_b_m_flow=port_b_m_flow,
connected_h=connected_h_b,
internal_h=internal_h,
),
)
def derivatives_from_connections(
self,
*,
port_a_m_flow: float,
connected_h_a: float,
port_b_m_flow: float,
connected_h_b: float,
internal_h: float,
) -> VolumeState:
inlet_h_a, inlet_h_b = self.connection_inlet_enthalpies(
port_a_m_flow=port_a_m_flow,
connected_h_a=connected_h_a,
port_b_m_flow=port_b_m_flow,
connected_h_b=connected_h_b,
internal_h=internal_h,
)
return self.derivatives(
inlet_h_a=inlet_h_a,
inlet_h_b=inlet_h_b,
m_flow_a=port_a_m_flow,
m_flow_b=port_b_m_flow,
)
def derivatives(
self,
inlet_h_a: float,
inlet_h_b: float,
m_flow_a: float,
m_flow_b: float,
) -> VolumeState:
dm_dt = m_flow_a + m_flow_b
dU_dt = m_flow_a * inlet_h_a + m_flow_b * inlet_h_b
return VolumeState(m=dm_dt, U=dU_dt)
-222
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@@ -1,222 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass, field
from datetime import UTC, datetime
from pathlib import Path
from app.simulation.examples.testmodel.closure import TestModelSolveDiagnostics
from app.simulation.examples.testmodel.system import (
InitializationDiagnostics,
TestModelConfig,
TestModelSystem,
)
from app.simulation.paths import (
MODELICA_TESTMODEL_RESULT_PATH,
PROJECT_ROOT,
SIMULATION_RUNS_DIR,
)
from app.simulation.reporting import (
COMPARISON_KEYS,
PRIMARY_KEYS,
TestModelArtifacts,
export_testmodel_artifacts,
format_testmodel_run_report,
load_modelica_series,
write_testmodel_run_report,
)
from app.simulation.solvers.solver import SolveIVPConfig
@dataclass(frozen=True)
class TestModelSamplingConfig:
step: float = 0.1
@dataclass(frozen=True)
class TestModelPathConfig:
output_dir: Path | None = None
modelica_result_path: Path | None = None
@dataclass(frozen=True)
class TestModelExecutionConfig:
use_modelica_reference_if_available: bool = True
@dataclass(frozen=True)
class TestModelRunConfig:
model: TestModelConfig = field(default_factory=TestModelConfig)
solver: SolveIVPConfig = field(default_factory=SolveIVPConfig)
sampling: TestModelSamplingConfig = field(default_factory=TestModelSamplingConfig)
paths: TestModelPathConfig = field(default_factory=TestModelPathConfig)
execution: TestModelExecutionConfig = field(default_factory=TestModelExecutionConfig)
@property
def sample_step(self) -> float:
return self.sampling.step
def sample_times(self) -> list[float]:
return _sample_times(
self.solver.t_start,
self.solver.t_stop,
step=self.sampling.step,
)
@dataclass(frozen=True)
class PreparedTestModelRun:
run_config: TestModelRunConfig
repo_root: Path
output_dir: Path
modelica_result_path: Path
t_eval: tuple[float, ...]
use_modelica_reference_if_available: bool
modelica_reference_exists: bool
@dataclass(frozen=True)
class TestModelRunResult:
run_config: TestModelRunConfig
prepared_run: PreparedTestModelRun
system: TestModelSystem
initialization: InitializationDiagnostics
raw_initial_state: tuple[float, ...]
consistent_initial_state: tuple[float, ...]
solution: object
series: dict[str, list[float]]
solve_diagnostics: TestModelSolveDiagnostics | None
artifacts: TestModelArtifacts
comparison_summary: dict[str, tuple[float, float]] | None
used_modelica_reference: bool
def _sample_times(t_start: float, t_stop: float, step: float) -> list[float]:
point_count = int(round((t_stop - t_start) / step))
return [t_start + index * step for index in range(point_count + 1)]
def _default_run_output_dir() -> Path:
timestamp = datetime.now(UTC).strftime("testmodel_%Y%m%d_%H%M%S_%f")
return SIMULATION_RUNS_DIR / timestamp
def prepare_testmodel_run(
*,
run_config: TestModelRunConfig | None = None,
output_dir: Path | None = None,
modelica_result_path: Path | None = None,
) -> PreparedTestModelRun:
run_config = run_config or TestModelRunConfig()
resolved_output_dir = (
output_dir
or run_config.paths.output_dir
or _default_run_output_dir()
)
resolved_modelica_result_path = (
modelica_result_path
or run_config.paths.modelica_result_path
or MODELICA_TESTMODEL_RESULT_PATH
)
t_eval = tuple(run_config.sample_times())
return PreparedTestModelRun(
run_config=run_config,
repo_root=PROJECT_ROOT,
output_dir=resolved_output_dir,
modelica_result_path=resolved_modelica_result_path,
t_eval=t_eval,
use_modelica_reference_if_available=run_config.execution.use_modelica_reference_if_available,
modelica_reference_exists=resolved_modelica_result_path.exists(),
)
def run_prepared_testmodel(prepared_run: PreparedTestModelRun) -> TestModelRunResult:
run_config = prepared_run.run_config
system = TestModelSystem(config=run_config.model)
raw_initial_state = tuple(system.initial_state_vector())
initialization = system.initialize_consistent_state()
consistent_initial_state = tuple(initialization.state_vector)
solution = system.simulate(config=run_config.solver, t_eval=list(prepared_run.t_eval))
series = system.evaluate_solution(solution)
solve_diagnostics = system.last_solve_diagnostics
modelica_series = None
used_modelica_reference = False
if (
prepared_run.use_modelica_reference_if_available
and prepared_run.modelica_reference_exists
):
modelica_series = load_modelica_series(
prepared_run.modelica_result_path,
COMPARISON_KEYS,
)
used_modelica_reference = True
artifacts, comparison_summary = export_testmodel_artifacts(
output_dir=prepared_run.output_dir,
series=series,
modelica_series=modelica_series,
)
report_text = format_testmodel_run_report(
network_summary=system.network.summary(),
initialization=initialization,
raw_initial_state=raw_initial_state,
consistent_initial_state=consistent_initial_state,
solution=solution,
series=series,
solve_diagnostics=solve_diagnostics,
artifacts=artifacts,
comparison_summary=comparison_summary,
)
write_testmodel_run_report(prepared_run.output_dir, report_text)
return TestModelRunResult(
run_config=run_config,
prepared_run=prepared_run,
system=system,
initialization=initialization,
raw_initial_state=raw_initial_state,
consistent_initial_state=consistent_initial_state,
solution=solution,
series=series,
solve_diagnostics=solve_diagnostics,
artifacts=artifacts,
comparison_summary=comparison_summary,
used_modelica_reference=used_modelica_reference,
)
def run_testmodel(
*,
run_config: TestModelRunConfig | None = None,
output_dir: Path | None = None,
modelica_result_path: Path | None = None,
) -> TestModelRunResult:
prepared_run = prepare_testmodel_run(
run_config=run_config,
output_dir=output_dir,
modelica_result_path=modelica_result_path,
)
return run_prepared_testmodel(prepared_run)
def main() -> None:
run_config = TestModelRunConfig()
result = run_testmodel(run_config=run_config)
print(
format_testmodel_run_report(
network_summary=result.system.network.summary(),
initialization=result.initialization,
raw_initial_state=result.raw_initial_state,
consistent_initial_state=result.consistent_initial_state,
solution=result.solution,
series=result.series,
solve_diagnostics=result.solve_diagnostics,
artifacts=result.artifacts,
comparison_summary=result.comparison_summary,
),
end="",
)
if __name__ == "__main__":
main()
-303
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@@ -1,303 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass, field
from typing import Any
from app.simulation.components.experimental.flow.orifice import Orifice
from app.simulation.components.experimental.junctions.tee import Tee
from app.simulation.components.experimental.storage.cylinder import Cylinder
from app.simulation.components.experimental.storage.tank import Tank
from app.simulation.core.medium import IdealGasMedium
from app.simulation.examples.testmodel.closure import (
BranchClosureComponents,
InitializationDiagnostics,
TestModelClosure,
TestModelClosureComponents,
TestModelSnapshot,
)
from app.simulation.examples.testmodel.dynamic_pipe import Pipe
from app.simulation.solvers.solver import SolveIVPConfig, integrate_ode
from app.simulation.systems.network import SimulationNetwork
@dataclass(frozen=True)
class CylinderConfig:
volume: float = 0.01
p0: float = 35e6
T0: float = 300.0
@dataclass(frozen=True)
class OrificeConfig:
K: float = 1e-5
@dataclass(frozen=True)
class TankConfig:
volume: float = 0.1
p0: float = 1e5
T0: float = 300.0
@dataclass(frozen=True)
class PipeConfig:
length: float = 5.0
diameter: float = 0.02
lambda_darcy: float = 0.02
p0: float = 1e5
T0: float = 300.0
@dataclass(frozen=True)
class BranchConfig:
orifice: OrificeConfig = field(default_factory=OrificeConfig)
pipe: PipeConfig = field(default_factory=PipeConfig)
@dataclass(frozen=True)
class TestModelConfig:
cylinder: CylinderConfig = field(default_factory=CylinderConfig)
upper_branch: BranchConfig = field(default_factory=BranchConfig)
lower_branch: BranchConfig = field(default_factory=BranchConfig)
tank: TankConfig = field(default_factory=TankConfig)
class TestModelSystem:
"""Runnable first-pass Python system for the current Testmodel topology.
This version keeps the component split from the Modelica model while keeping
the downstream tee-tank pressure coupling in the ODE framework. The original
Modelica system is a tighter DAE because both pipe outlets discharge into an
ideal lossless junction directly connected to the tank. Here the branch
outlet flows are solved from a pressure-consistent energy balance so the
outlet is no longer driven by an arbitrary conductance parameter.
"""
def __init__(
self,
medium: IdealGasMedium | None = None,
config: TestModelConfig | None = None,
) -> None:
self.medium = medium or IdealGasMedium()
self.config = config or TestModelConfig()
self.mycylinder = Cylinder(
name="mycylinder",
medium=self.medium,
V=self.config.cylinder.volume,
p0=self.config.cylinder.p0,
T0=self.config.cylinder.T0,
)
self.mytee = Tee(name="mytee")
self.myorifice = Orifice(name="myorifice", K=self.config.upper_branch.orifice.K)
self.mypipe = Pipe(
name="mypipe",
medium=self.medium,
L=self.config.upper_branch.pipe.length,
D=self.config.upper_branch.pipe.diameter,
lambda_darcy=self.config.upper_branch.pipe.lambda_darcy,
p0=self.config.upper_branch.pipe.p0,
T0=self.config.upper_branch.pipe.T0,
)
self.myorifice1 = Orifice(name="myorifice1", K=self.config.lower_branch.orifice.K)
self.mypipe1 = Pipe(
name="mypipe1",
medium=self.medium,
L=self.config.lower_branch.pipe.length,
D=self.config.lower_branch.pipe.diameter,
lambda_darcy=self.config.lower_branch.pipe.lambda_darcy,
p0=self.config.lower_branch.pipe.p0,
T0=self.config.lower_branch.pipe.T0,
)
self.mytee1 = Tee(name="mytee1")
self.mytank = Tank(
name="mytank",
medium=self.medium,
V=self.config.tank.volume,
p0=self.config.tank.p0,
T0=self.config.tank.T0,
)
self.network = SimulationNetwork(name="Testmodel")
for component in (
self.mycylinder,
self.mytee,
self.myorifice,
self.mypipe,
self.myorifice1,
self.mypipe1,
self.mytee1,
self.mytank,
):
self.network.add_component(component)
self.network.connect("mycylinder", "port_b", "mytee", "port_in")
self.network.connect("mytee", "port_out1", "myorifice", "port_a")
self.network.connect("myorifice", "port_b", "mypipe", "port_a")
self.network.connect("mypipe", "port_b", "mytee1", "port_out2")
self.network.connect("mytee", "port_out2", "myorifice1", "port_a")
self.network.connect("myorifice1", "port_b", "mypipe1", "port_a")
self.network.connect("mypipe1", "port_b", "mytee1", "port_out1")
self.network.connect("mytee1", "port_in", "mytank", "port_a")
self.closure = TestModelClosure(
medium=self.medium,
components=TestModelClosureComponents(
cylinder=self.mycylinder,
upstream_tee=self.mytee,
upper_branch=BranchClosureComponents(
name="upper_branch",
orifice=self.myorifice,
pipe=self.mypipe,
),
lower_branch=BranchClosureComponents(
name="lower_branch",
orifice=self.myorifice1,
pipe=self.mypipe1,
),
downstream_tee=self.mytee1,
tank=self.mytank,
),
initial_state_vector=self.initial_state_vector,
apply_state_vector=self.apply_state_vector,
)
def initial_state_vector(self) -> list[float]:
return self.network.initial_state_vector()
def apply_state_vector(self, values: list[float]) -> None:
self.network.apply_state_vector(values)
def consistent_initial_state_vector(self) -> list[float]:
return self.closure.consistent_initial_state_vector()
@property
def last_solve_diagnostics(self):
return self.closure.last_solve_diagnostics
def initialize_consistent_state(
self,
max_iterations: int = 12,
state_tolerance: float = 1e-9,
flow_tolerance: float = 1e-9,
enthalpy_tolerance: float = 1e-6,
pressure_tolerance: float = 1e-6,
strict_internal_solvers: bool = False,
) -> InitializationDiagnostics:
return self.closure.initialize_consistent_state(
max_iterations=max_iterations,
state_tolerance=state_tolerance,
flow_tolerance=flow_tolerance,
enthalpy_tolerance=enthalpy_tolerance,
pressure_tolerance=pressure_tolerance,
strict_internal_solvers=strict_internal_solvers,
)
def project_downstream_pressure_constraints(self, *, strict: bool = False) -> None:
self.closure.project_downstream_pressure_constraints(strict=strict)
def snapshot(
self,
state_vector: list[float] | None = None,
*,
strict: bool = False,
) -> TestModelSnapshot:
return self.closure.snapshot(state_vector, strict=strict)
def rhs(self, _t: float, state_vector: list[float]) -> list[float]:
return self.closure.rhs(state_vector)
@staticmethod
def _legacy_branch_series_key_map() -> tuple[tuple[str, str, str], tuple[str, str, str]]:
return (
("upper_branch", "branch_upper.in", "branch_upper.out"),
("lower_branch", "branch_lower.in", "branch_lower.out"),
)
@classmethod
def _legacy_branch_series_keys_by_name(cls) -> dict[str, tuple[str, str]]:
return {
branch_name: (inlet_key, outlet_key)
for branch_name, inlet_key, outlet_key in cls._legacy_branch_series_key_map()
}
@staticmethod
def _generic_branch_series_keys(branch_name: str) -> tuple[str, str, str]:
return (
f"branch.{branch_name}.p",
f"branch.{branch_name}.in",
f"branch.{branch_name}.out",
)
@staticmethod
def _legacy_branch_pressure_keys_by_name() -> dict[str, str]:
return {
"upper_branch": "mypipe.p",
"lower_branch": "mypipe1.p",
}
@classmethod
def _append_legacy_branch_series_aliases(
cls,
series: dict[str, list[float]],
) -> dict[str, list[float]]:
legacy_branch_series_keys = cls._legacy_branch_series_keys_by_name()
legacy_branch_pressure_keys = cls._legacy_branch_pressure_keys_by_name()
for branch_name, (legacy_inlet_key, legacy_outlet_key) in legacy_branch_series_keys.items():
pressure_key, generic_inlet_key, generic_outlet_key = cls._generic_branch_series_keys(
branch_name
)
series[legacy_branch_pressure_keys[branch_name]] = list(series[pressure_key])
series[legacy_inlet_key] = list(series[generic_inlet_key])
series[legacy_outlet_key] = list(series[generic_outlet_key])
return series
def simulate(
self,
config: SolveIVPConfig | None = None,
t_eval: list[float] | None = None,
) -> Any:
return integrate_ode(
rhs=self.rhs,
initial_state=self.consistent_initial_state_vector(),
config=config or SolveIVPConfig(),
t_eval=t_eval,
)
def evaluate_solution(self, solution: Any) -> dict[str, list[float]]:
series = {
"time": [],
"mycylinder.p": [],
"mycylinder.T": [],
"mytank.p": [],
"mytank.T": [],
}
for branch_name, _, _ in self._legacy_branch_series_key_map():
pressure_key, inlet_key, outlet_key = self._generic_branch_series_keys(branch_name)
series[pressure_key] = []
series[inlet_key] = []
series[outlet_key] = []
for index, time_value in enumerate(solution.t):
state_vector = [row[index] for row in solution.y]
snapshot = self.snapshot(state_vector)
series["time"].append(float(time_value))
series["mycylinder.p"].append(snapshot.cylinder.p)
series["mycylinder.T"].append(snapshot.cylinder.T)
series["mytank.p"].append(snapshot.tank.p)
series["mytank.T"].append(snapshot.tank.T)
for branch in snapshot.branches:
pressure_key, generic_inlet_key, generic_outlet_key = self._generic_branch_series_keys(
branch.name
)
series[pressure_key].append(branch.pipe.p)
series[generic_inlet_key].append(branch.inlet_flow)
series[generic_outlet_key].append(branch.outlet_flow)
return self._append_legacy_branch_series_aliases(series)
def build_testmodel() -> SimulationNetwork:
"""Compatibility helper for callers that only need the topology."""
return TestModelSystem().network
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"""Compilation of supported XML networks to independent native executables."""
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"""python -m app.simulation.native_codegen INPUT.xml|json --output-dir DIR"""
from __future__ import annotations
import argparse
from dataclasses import replace
from hashlib import sha256
import json
from pathlib import Path
import shutil
import statistics
import time
from app.main import compile_system_xml_network
from app.simulation.backends import simulation_config
from .build import build_native
from .compiler import compile_native_program
from .input import load_input
from .runner import execute_native
def main():
parser = argparse.ArgumentParser(description=__doc__)
parser.add_argument("input", type=Path)
parser.add_argument("--output-dir", type=Path, required=True)
parser.add_argument("--method", choices=("RK45", "BDF"))
parser.add_argument("--max-step", type=float)
parser.add_argument("--rtol", type=float)
parser.add_argument("--runs", type=int, default=3)
parser.add_argument("--timeout", type=float, default=300)
parser.add_argument("--solve-only", action="store_true")
args = parser.parse_args()
if args.runs < 1:
parser.error("--runs must be positive")
out = args.output_dir.resolve()
out.mkdir(parents=True, exist_ok=True)
if (out / "summary.json").exists():
parser.error("Output directory already contains a completed run; choose a new directory.")
started = time.perf_counter()
xml, document = load_input(args.input)
program = compile_native_program(compile_system_xml_network(document))
config = simulation_config(document.simulation)
for name in ("method", "max_step", "rtol"):
if getattr(args, name) is not None:
config = replace(config, **{name: getattr(args, name)})
preparation = time.perf_counter()-started
(out / "input.xml").write_bytes(xml)
build = build_native(program)
package = out / "program"
package.mkdir(exist_ok=True)
for name in (*build.manifest["artifacts"], "manifest.json"):
shutil.copy2(build.executable.parent / name, package / name)
(out / "model-manifest.json").write_text(json.dumps(build.manifest, ensure_ascii=False, indent=2), encoding="utf-8")
rows = []
for i in range(args.runs+1):
data = execute_native(build, config, document.simulation.sample_step,
run_dir=out / ("warmup" if i == 0 else f"run-{i}"),
record_samples=not args.solve_only, timeout=args.timeout)
row = {k: v for k, v in data.items() if k not in ("series", "final", "finalState")}
row["run"] = "warmup" if i == 0 else i
rows.append(row)
print(json.dumps(row, ensure_ascii=False), flush=True)
if not data["success"]:
break
measured = rows[1:]
summary = {
"source": str(args.input.resolve()), "sourceSha256": sha256(args.input.read_bytes()).hexdigest(),
"xmlSha256": sha256(xml).hexdigest(), "executable": str(package / "model.exe"),
"cachedExecutable": str(build.executable),
"buildKey": build.manifest["buildKey"], "buildSeconds": build.seconds,
"preparationSeconds": preparation, "cacheHit": build.cache_hit,
"settings": vars(config), "sampleStep": document.simulation.sample_step,
"recordSamples": not args.solve_only, "runs": rows,
"success": len(measured) == args.runs and all(row["success"] for row in rows),
"medianSolveSeconds": statistics.median(row["solveSeconds"] for row in measured) if measured else None,
}
(out / "summary.json").write_text(json.dumps(summary, ensure_ascii=False, indent=2), encoding="utf-8")
print(json.dumps({k: v for k, v in summary.items() if k != "runs"}, ensure_ascii=False))
return 0 if summary["success"] else 1
if __name__ == "__main__":
raise SystemExit(main())
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"""Reproducible native builds and a checked, model-specific executable cache."""
from __future__ import annotations
from dataclasses import dataclass
from hashlib import sha256
import json
import os
from pathlib import Path
import shutil
import subprocess
import sys
import tempfile
import time
from .compiler import NativeProgram
ROOT = Path(__file__).resolve().parents[3]
NATIVE = ROOT / "native"
CACHE = ROOT / "app/data/native-builds"
LIBRARIES = ("cvode", "core", "nvecserial", "sunmatrixdense", "sunlinsoldense")
@dataclass(frozen=True)
class NativeBuild:
executable: Path
manifest: dict
cache_hit: bool
seconds: float
def _hash(path: Path) -> str:
return sha256(path.read_bytes()).hexdigest()
def toolchain() -> tuple[str, Path, str]:
compiler = os.environ.get("SIMULATION_NATIVE_CC") or shutil.which("gcc")
if not compiler:
raise RuntimeError("C compiler not found; set SIMULATION_NATIVE_CC to gcc.")
base = Path(os.environ.get("SUNDIALS_ROOT", str(Path(sys.base_prefix) / "Library")))
if not (base / "include/cvode/cvode.h").is_file():
raise RuntimeError("SUNDIALS C development files not found; set SUNDIALS_ROOT.")
version = subprocess.run([compiler, "--version"], capture_output=True, text=True, check=True, timeout=15).stdout.splitlines()[0]
return compiler, base, version
def build_native(program: NativeProgram, *, cache_dir: Path | None = None) -> NativeBuild:
start = time.perf_counter()
compiler, sundials, compiler_version = toolchain()
runtime = sorted(NATIVE.rglob("*.c")) + sorted((NATIVE / "include").glob("*.h"))
flags = ["-std=c11", "-O3", "-Wall", "-Wextra", "-Werror", "-ffp-contract=off", "-fno-fast-math"]
if os.name == "nt":
flags += ["-D__USE_MINGW_ANSI_STDIO=1", "-static-libgcc"]
libraries = [sundials / "lib" / f"sundials_{name}.lib" for name in LIBRARIES]
dlls = [sundials / "bin" / f"sundials_{name}.dll" for name in LIBRARIES]
vc_runtime = sundials / "bin/vcruntime140.dll"
if vc_runtime.is_file():
dlls.append(vc_runtime)
else:
raise RuntimeError("Native v1 build packaging currently supports Windows x64; Linux packaging is pending.")
sources = {str(p.relative_to(ROOT)): _hash(p) for p in runtime}
sources["native/THIRD_PARTY_NOTICES.txt"] = _hash(NATIVE / "THIRD_PARTY_NOTICES.txt")
dependencies = {str(p.name): _hash(p) for p in libraries + dlls}
# Header hashes include precision/index ABI settings as well as library APIs.
for directory in ("sundials", "cvode", "nvector", "sunmatrix", "sunlinsol"):
for path in sorted((sundials / "include" / directory).glob("*.h")):
dependencies[f"{directory}/{path.name}"] = _hash(path)
identity = dict(source=program.source, header=program.header, contract=program.manifest(), sources=sources,
dependencies=dependencies, compiler=compiler_version, flags=flags,
platform=sys.platform, abi=1)
signature = sha256(json.dumps(identity, sort_keys=True).encode()).hexdigest()
cache = (cache_dir or CACHE).resolve()
target = cache / signature
manifest_path = target / "manifest.json"
if manifest_path.is_file():
manifest = json.loads(manifest_path.read_text(encoding="utf-8"))
if all((target / name).is_file() and _hash(target / name) == digest
for name, digest in manifest["artifacts"].items()):
return NativeBuild(target / "model.exe", manifest, True, time.perf_counter()-start)
raise RuntimeError(f"Native cache integrity check failed: {target}")
cache.mkdir(parents=True, exist_ok=True)
stage = Path(tempfile.mkdtemp(prefix="building-", dir=cache))
(stage / "model.c").write_text(program.source, encoding="utf-8")
(stage / "model.h").write_text(program.header, encoding="utf-8")
command = [compiler, *flags, "-I", str(stage), "-I", str(NATIVE / "include"),
"-I", str(sundials / "include"), str(stage / "model.c"),
*[str(p) for p in runtime if p.suffix == ".c"],
*map(str, libraries), "-lm", "-o", str(stage / "model.exe")]
result = subprocess.run(command, capture_output=True, text=True, timeout=120)
(stage / "build.log").write_text(result.stdout + result.stderr, encoding="utf-8")
if result.returncode:
raise RuntimeError(f"Native compilation failed; see {stage / 'build.log'}: {result.stderr[-3000:]}")
for library in dlls:
shutil.copy2(library, stage / library.name)
shutil.copy2(NATIVE / "THIRD_PARTY_NOTICES.txt", stage / "THIRD_PARTY_NOTICES.txt")
manifest = {
**program.manifest(), "buildKey": signature, "compiler": compiler_version,
"compilerFlags": flags, "sourceHashes": sources, "dependencyHashes": dependencies,
"artifacts": {p.name: _hash(p) for p in stage.iterdir() if p.name != "build.log"},
}
(stage / "manifest.json").write_text(json.dumps(manifest, ensure_ascii=False, indent=2), encoding="utf-8")
try:
stage.rename(target)
except OSError:
# A concurrent compiler may have published the identical cache first.
if not manifest_path.is_file():
raise
published = json.loads(manifest_path.read_text(encoding="utf-8"))
# PE linker timestamps can differ between concurrent equivalent builds.
# Validate the winning build against its own hashes and our identity.
if published.get("buildKey") != signature or not all(
(target / name).is_file() and _hash(target / name) == digest
for name, digest in published["artifacts"].items()
):
raise RuntimeError("Concurrent native build did not produce the expected artifacts.")
manifest = published
if stage.resolve().parent != cache:
raise RuntimeError("Unexpected native build staging directory.")
shutil.rmtree(stage)
return NativeBuild(target / "model.exe", manifest, False, time.perf_counter()-start)
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"""Lower reviewed component contracts to a static C evaluation schedule.
The compact storage-anchored schedule and the extended catalog schedule both
produce standalone C numerics, without Python callbacks or numerical fallback.
"""
from __future__ import annotations
from dataclasses import dataclass
import json
from math import isfinite
from app.simulation.core.metadata import ResultVariableMetadata
from app.simulation.systems.network import SimulationNetwork
from .contracts import SUPPORTED_TYPES, SUPPORTED_VERSIONS
class NativeCapabilityError(ValueError):
"""The complete model cannot be represented by this native backend."""
_STORAGE_ANCHORED_TYPES = frozenset(
"amesim_" + name for name in (
"pnch023", "pnch012", "pnvo001", "pnpl01", "step0", "ud00",
"forc", "pnrp17", "mecmas21", "f000", "lstp00a",
)
)
@dataclass(frozen=True)
class NativeProgram:
source: str
header: str
state_keys: tuple[str, ...]
variables: tuple[ResultVariableMetadata, ...]
component_types: tuple[str, ...]
def manifest(self) -> dict:
return {
"abiVersion": 1, "stateKeys": self.state_keys,
"variables": [v.as_dict() for v in self.variables],
"componentTypes": self.component_types,
"componentVersions": {name: SUPPORTED_VERSIONS[name] for name in self.component_types},
"jacobianPolicy": "CVODE default; no custom Jacobian",
}
class _Groups:
def __init__(self, items):
self.parent = {x: x for x in items}
def find(self, x):
if self.parent[x] != x:
self.parent[x] = self.find(self.parent[x])
return self.parent[x]
def union(self, a, b):
self.parent[self.find(b)] = self.find(a)
def _number(value):
value = float(value)
if not isfinite(value):
raise NativeCapabilityError("Native constants must be finite.")
return repr(value)
def compile_native_program(network: SimulationNetwork) -> NativeProgram:
from .extended import catalog_contracts
contracts = catalog_contracts()
for component in network.components.values():
if type(component) is not contracts.get(component.model_type):
raise NativeCapabilityError(f'{component.name}: no native contract for {component.model_type}')
if component.MODEL_VERSION != SUPPORTED_VERSIONS.get(component.model_type):
raise NativeCapabilityError(f'{component.name}: native kernel version does not match the component contract')
# Preserve the compact, verified schedule for its supported topology.
# Both paths emit C; this never falls back to Python numerical execution.
try:
return _compile_storage_anchored_program(network)
except NativeCapabilityError:
from .extended import compile_extended_program
return compile_extended_program(network)
def _compile_storage_anchored_program(network: SimulationNetwork) -> NativeProgram:
components = list(network.components.values())
if not components:
raise NativeCapabilityError("Native simulation requires a dynamic model.")
for c in components:
if c.model_type not in _STORAGE_ANCHORED_TYPES:
raise NativeCapabilityError(f"{c.name}: unsupported native component {c.model_type}.")
if c.MODEL_VERSION != SUPPORTED_VERSIONS[c.model_type]:
raise NativeCapabilityError(f"{c.name}: native kernel version does not match the component contract.")
if c.model_type == "amesim_pnch023" and c.kth*c.sth != 0:
raise NativeCapabilityError(f"{c.name}: native v1 supports adiabatic PNCH023 only.")
medium = getattr(c, "medium", None)
if medium is not None and (
getattr(medium, "SUBSTANCE_ID", None),
getattr(medium, "PROPERTY_METHOD_ID", None),
) != ("helium", "peng_robinson"):
raise NativeCapabilityError(f"{c.name}: native v1 requires helium / Peng-Robinson.")
if c.model_type == "amesim_mecmas21":
if int(c.stoptype) not in (1, 4) or any(
getattr(c, key) != 0 for key in ("fcoul", "fstick", "rvisc", "wind", "theta")
):
raise NativeCapabilityError(f"{c.name}: native v1 supports friction-free masses with stoptype 1 or 4.")
if c.model_type == "amesim_lstp00a" and int(c.stiffmode) != 1:
raise NativeCapabilityError(f"{c.name}: native v1 requires explicit contact stiffness.")
ports = {
(c.name, p.name): p for c in components for p in c.active_port_definitions
}
adjacent = {}
groups = _Groups(ports)
for edge in network.connections:
a, b = (p.key for p in edge.endpoints)
# Signal fan-out is allowed; physical ports have one external connection.
if edge.kind == "physical":
if a in adjacent or b in adjacent:
raise NativeCapabilityError("Native physical ports require one connection each.")
adjacent[a], adjacent[b] = b, a
groups.union(a, b)
else:
source, target = (a, b) if ports[a].nominal_role == "output" else (b, a)
adjacent[target] = source
for c in components:
for name in c.required_connection_ports:
if (c.name, name) not in adjacent:
raise NativeCapabilityError(f"{c.name}.{name}: unconnected physical port.")
names = [p.name for p in c.active_port_definitions if p.domain == "pneumatic"]
if c.model_type in ("amesim_pnch023", "amesim_pnch012"):
for name in names[1:]:
groups.union((c.name, names[0]), (c.name, name))
if c.model_type == "amesim_mecmas21":
groups.union((c.name, "port_1"), (c.name, "port_2"))
if c.model_type == "amesim_pnrp17":
groups.union((c.name, "port_2"), (c.name, "port_5"))
groups.union((c.name, "port_3"), (c.name, "port_4"))
chambers = [c for c in components if c.model_type in ("amesim_pnch023", "amesim_pnch012")]
masses = [c for c in components if c.model_type == "amesim_mecmas21"]
chamber_by_group, mass_by_group = {}, {}
for items, mapping in ((chambers, chamber_by_group), (masses, mass_by_group)):
for c in items:
root = groups.find((c.name, "port_1"))
if root in mapping:
raise NativeCapabilityError(f"{c.name}: coupled storage/mass reduction is outside native v1.")
mapping[root] = c
for ep, port in ports.items():
mapping = chamber_by_group if port.domain == "pneumatic" else mass_by_group
if port.kind == "physical" and groups.find(ep) not in mapping:
raise NativeCapabilityError(f"{ep}: no unique storage/mass anchor; native v1 cannot close this block.")
variables = tuple(v for c in components for v in c.result_variable_metadata())
slots = {v.key: i for i, v in enumerate(variables)}
assigned = set()
lines, init, declarations = [], [], []
state_keys, state_index = [], {}
for c in components:
fields = ("m", "U") if c in chambers else (("v", "x") if c in masses else ())
for field in fields:
key = f"{c.name}.{field}"
state_index[key] = len(state_keys)
state_keys.append(key)
if not state_keys:
raise NativeCapabilityError("Native v1 requires continuous states.")
if len(state_keys) > 256 or len(variables) > 8192:
raise NativeCapabilityError("Native v1 supports at most 256 states and 8192 outputs per model.")
def w(key):
return f"w[{slots[key]}]"
def key(c, field):
return f"{c.name}.{field}"
def get(c, field):
return w(key(c, field))
def put(c, field, expression):
k = key(c, field)
lines.append(f"{w(k)} = {expression};")
assigned.add(k)
def si(c, field):
return state_index[key(c, field)]
def mass_at(c, port):
return mass_by_group[groups.find((c.name, port))]
def chamber_at(c, port):
return chamber_by_group[groups.find((c.name, port))]
for c in masses:
init.extend([f"y[{si(c, 'v')}] = {_number(c.v0)};", f"y[{si(c, 'x')}] = {_number(c.x0)};"])
for field in ("v", "x"):
put(c, field, f"y[{si(c, field)}]")
for (cid, pname), port in ports.items():
if port.domain == "mechanical":
m = mass_by_group[groups.find((cid, pname))]
for field in ("v", "x"):
k = f"{cid}.{pname}.{field}"
lines.append(f"{w(k)} = y[{si(m, field)}];")
assigned.add(k)
signal_specs = []
for c in components:
if c.model_type == "amesim_step0":
put(c, "y", f"t < {_number(c.time)} ? {_number(c.initial)} : {_number(c.final)}")
signal_specs.append(("step", c))
elif c.model_type == "amesim_ud00":
index = len(signal_specs)
declarations.append(f"static const double signal_{index}[24] = {{" + ",".join(
_number(v) for values in (c.starts, c.ends, c.durations) for v in values
) + "};")
put(c, "y", f"native_signal(t, {_number(c.tstart)}, {c.nstages}, {int(c.iscyclic)}, signal_{index})")
signal_specs.append((index, c))
else:
continue
put(c, "out.signal", get(c, "y"))
for c in components:
for port in c.active_port_definitions:
if port.kind == "signal" and port.nominal_role == "input":
ep = (c.name, port.name)
if ep not in adjacent:
# PNVO's explicit unconnected opening is a supported default.
if c.model_type == "amesim_pnvo001":
put(c, port.name + ".signal", _number(c.opening0))
continue
raise NativeCapabilityError(f"{ep}: missing signal input.")
source = adjacent[ep]
source_key = f"{source[0]}.{source[1]}.signal"
if source_key not in assigned:
raise NativeCapabilityError(f"{ep}: unsupported signal dependency.")
put(c, port.name + ".signal", w(source_key))
pistons = [c for c in components if c.model_type == "amesim_pnrp17"]
for c in pistons:
put(c, "length", f"{_number(c.x0)} + {get(c, 'port_5.x')} - {get(c, 'port_4.x')}")
put(c, "volume", f"{_number(c.effective_area)} * {get(c, 'length')}")
put(c, "volume_flow", f"{_number(c.effective_area)} * ({get(c, 'port_5.v')} - {get(c, 'port_4.v')})")
if chamber_at(c, "port_1").model_type != "amesim_pnch012":
raise NativeCapabilityError(f"{c.name}: moving volume requires PNCH012.")
volume_expressions = {}
for gi, c in enumerate(chambers):
connected = [p for p in pistons if chamber_at(p, "port_1") is c]
base = c.cvol if c.model_type == "amesim_pnch023" else c.cvol0 + sum(c.external_volumes.values())
volume = _number(base)
rate = "0.0"
if c.model_type == "amesim_pnch012":
volume += "".join(" + " + get(p, "volume") for p in connected)
put(c, "vol", f"fmax({_number(c.cvol0 / 100)}, {volume})")
rate = _number(sum(c.external_volume_rates.values())) + "".join(" + " + get(p, "volume_flow") for p in connected)
put(c, "dvol", f"{get(c, 'vol')} <= {_number(c.cvol0 / 100)} ? 0.0 : ({rate})")
volume, rate = get(c, "vol"), get(c, "dvol")
volume_expressions[c.name] = (volume, rate)
# Match the Python constructor: m/U use configured storage volume;
# connected moving volumes subsequently change recovered p/T.
initial_volume = max(base, c.cvol0 / 100) if c.model_type == "amesim_pnch012" else base
init.append(f"if (!native_gas_init({_number(c.p0)}, {_number(c.T0)}, {_number(initial_volume)}, &y[{si(c, 'm')}])) return 0;")
lines.append(f"NativeGas gas_{gi};")
lines.append(f"if (!native_gas(y[{si(c, 'm')}], y[{si(c, 'U')}], {volume}, &gas_{gi})) return 0;")
for field in ("m", "U"):
put(c, field, f"y[{si(c, field)}]")
for field in ("p", "T", "rho", "u", "h"):
put(c, field, f"gas_{gi}.{field}")
for (cid, pname), port in ports.items():
if port.domain == "pneumatic":
c = chamber_by_group[groups.find((cid, pname))]
for field, expr in (("p", get(c, "p")), ("h_outflow", get(c, "h")), ("m_flow", "0.0")):
k = f"{cid}.{pname}.{field}"
lines.append(f"{w(k)} = {expr};")
assigned.add(k)
for c in components:
if c.model_type != "amesim_pnvo001":
continue
a, b = chamber_at(c, "port_2"), chamber_at(c, "port_3")
put(c, "xv", f"fmax(0.0, fmin(1.0, {get(c, 'res.signal')}))")
lines.append(f"if (!native_orifice({get(a, 'p')}, {get(b, 'p')}, {get(a, 'h')}, {get(b, 'h')}, {_number(c.effective_cq * c.maximum_area)}, {get(c, 'xv')}, &{get(c, 'port_2.m_flow')}, &{get(c, 'cm')}, &{get(c, 'gasvel')})) return 0;")
assigned.update((key(c, "cm"), key(c, "gasvel")))
put(c, "port_3.m_flow", f"-{get(c, 'port_2.m_flow')}")
put(c, "port_2.h_outflow", get(b, "h"))
put(c, "port_3.h_outflow", get(a, "h"))
for pname in ("port_2", "port_3"):
other = adjacent[c.name, pname]
# A resistance-to-resistance stream path requires a fuller IR.
if network.components[other[0]] not in chambers:
raise NativeCapabilityError(f"{c.name}: native v1 requires valve ports directly connected to storage.")
lines.append(f"{w(f'{other[0]}.{other[1]}.m_flow')} = -{get(c, pname + '.m_flow')};")
force_known = set()
def force(c, port, expr):
put(c, port + ".f", expr)
force_known.add((c.name, port))
equations = []
for c in components:
if c.model_type == "amesim_forc":
put(c, "force", f"{_number(c.direction)} * {get(c, 'res.signal')}")
force(c, "port_2", f"-{get(c, 'force')}")
elif c.model_type == "amesim_f000":
force(c, "port_1", "0.0")
elif c.model_type == "amesim_lstp00a":
put(c, "gap", f"{_number(c.gap0)} + ({get(c, 'port_2.x')} - {get(c, 'port_1.x')})")
put(c, "penetration", f"fmax(-{get(c, 'gap')}, 0.0)")
put(c, "force", f"native_contact({get(c, 'penetration')}, {get(c, 'port_1.v')} - {get(c, 'port_2.v')}, {_number(c.kcont)}, {_number(c.rcont)}, {_number(c.Pdis)}, {int(c.discContactOption)})")
force(c, "port_1", get(c, "force"))
force(c, "port_2", f"-{get(c, 'force')}")
elif c.model_type == "amesim_pnrp17":
put(c, "pressure_force", f"({get(c, 'port_1.p')} - 101300.0) * {_number(c.effective_area)}")
equations.extend([
((c.name, "port_2"), (c.name, "port_5"), f"-{get(c, 'pressure_force')}"),
((c.name, "port_3"), (c.name, "port_4"), get(c, "pressure_force")),
])
for edge in network.connections:
if edge.domain == "mechanical":
equations.append((*[p.key for p in edge.endpoints], "0.0"))
pending = equations
while pending:
remaining = []
for a, b, total in pending:
if a in force_known and b in force_known:
raise NativeCapabilityError("Overconstrained native force balance.")
if a not in force_known and b not in force_known:
remaining.append((a, b, total))
continue
target, source = (b, a) if a in force_known else (a, b)
c = network.components[target[0]]
force(c, target[1], f"({total}) - {w(f'{source[0]}.{source[1]}.f')}")
if len(remaining) == len(pending):
raise NativeCapabilityError("Native v1 cannot resolve this mechanical force loop.")
pending = remaining
for c in masses:
expression = f"({get(c, 'port_1.f')} + {get(c, 'port_2.f')}) / {_number(c.mass)}"
put(c, "a", expression)
lines.append(f"dy[{si(c, 'v')}] = {get(c, 'a')}; dy[{si(c, 'x')}] = {get(c, 'v')};")
if int(c.stoptype) == 1:
lines.append(f"native_stop_motion({get(c, 'x')}, {get(c, 'v')}, {_number(c.xmin)}, {_number(c.xmax)}, &dy[{si(c, 'v')}], &dy[{si(c, 'x')}]);")
put(c, "a", f"dy[{si(c, 'v')}]")
for field in ("Fvisc", "Ffric", "Fmin", "Fmax"):
put(c, field, "0.0")
for c in chambers:
mass_terms, energy_terms = [], []
for port in c.active_port_definitions:
q = get(c, port.name + ".m_flow")
other = adjacent[c.name, port.name]
inlet_h = w(f"{other[0]}.{other[1]}.h_outflow")
mass_terms.append(q)
energy_terms.append(f"{q} * ({q} > 0.0 ? {inlet_h} : {get(c, 'h')})")
volume, rate = volume_expressions[c.name]
energy_terms.extend([f"{_number(c.kth*c.sth)} * ({_number(c.extemp)} - {get(c, 'T')})", f"-{get(c, 'p')} * ({rate})"])
lines.extend([f"dy[{si(c, 'm')}] = " + " + ".join(mass_terms) + ";", f"dy[{si(c, 'U')}] = " + " + ".join(energy_terms) + ";"])
missing = set(slots) - assigned
if missing:
raise NativeCapabilityError(f"Native output coverage is incomplete: {sorted(missing)}")
stops = [(si(c, "v"), c.xmin, c.xmax) for c in masses if int(c.stoptype) == 1]
stop_c = ",".join(f"{{{v},{_number(lo)},{_number(hi)},0,0,0,0}}" for v, lo, hi in stops) or "{0,0,0,0,0,0,0}"
next_event = []
for index, c in signal_specs:
if index == "step":
next_event.append(f"if (t < {_number(c.time)}) result = fmin(result, {_number(c.time)});")
else:
next_event.append(f"result = fmin(result, native_signal_break(t, end, {_number(c.tstart)}, {c.nstages}, {int(c.iscyclic)}, signal_{index}));")
source = '\n'.join([
'#include "model.h"', '#include <math.h>', *declarations,
f"const NativeStop model_stops[{max(1,len(stops))}] = {{{stop_c}}};",
f"const double model_atol[NSTATES] = {{{','.join('1e-12' if k.rsplit('.',1)[1] in ('v','x') else '1e-8' for k in state_keys)}}};",
"const char *const model_output_keys[NOUTPUTS] = {" + ",".join(json.dumps(v.key, ensure_ascii=True) for v in variables) + "};",
"int model_init(double *y) {", *init, "return 1; }",
"int model_eval(double t, const double *y, double *dy, double *w) {", "(void)t;", *lines,
"for (int i=0;i<NSTATES;i++) if (!isfinite(dy[i])) return 0;",
"for (int i=0;i<NOUTPUTS;i++) if (!isfinite(w[i])) return 0;",
"return 1; }",
"double model_next_break(double t, double end) { (void)t; double result=end;", *next_event,
"return result; }", "",
])
header = f'''#ifndef GENERATED_NATIVE_MODEL_H
#define GENERATED_NATIVE_MODEL_H
#include "kernels.h"
#define NSTATES {len(state_keys)}
#define NOUTPUTS {len(variables)}
#define NSTOPS {len(stops)}
extern const NativeStop model_stops[{max(1,len(stops))}];
extern const double model_atol[NSTATES];
extern const char *const model_output_keys[NOUTPUTS];
int model_init(double *y);
int model_eval(double t, const double *y, double *dy, double *w);
double model_next_break(double t, double end);
#endif
'''
return NativeProgram(source, header, tuple(state_keys), variables, tuple(sorted({c.model_type for c in components})))
@@ -0,0 +1,32 @@
"""Reviewed model contract versions implemented by the C kernels.
A new registration/version must be explicitly ported and tested; it does not
gain native support just by inheriting a supported Python component class.
"""
SUPPORTED_VERSIONS = {
'amesim_ideal_air_medium': '0.2.0',
'amesim_helium_medium': '0.1.0',
'amesim_pnpl01': '0.1.0',
'amesim_step0': '0.1.0',
'amesim_ud00': '0.2.0',
'amesim_f000': '0.1.0',
'amesim_forc': '0.2.0',
'amesim_mecmas21': '0.2.0',
'amesim_lstp00a': '0.2.0',
'amesim_lmechn1': '0.2.0',
'amesim_pnrp17': '0.1.0',
'amesim_pnch023': '0.1.0',
'amesim_pnch012': '0.1.0',
'amesim_pnor001': '0.3.0',
'amesim_pnvo001_fixed': '0.2.0',
'amesim_pnvo001': '0.2.0',
'amesim_pnl00r': '0.3.0',
'amesim_pnl0001': '0.4.0',
'amesim_pnl0002': '0.6.0',
'amesim_pnl0003': '0.4.0',
'amesim_pn3node2': '0.3.0',
'amesim_p4node2': '0.3.0',
'cylinder': '1.0.0', 'tank': '1.0.0', 'pipe': '1.0.0',
'orifice': '1.0.0', 'tee': '1.0.0',
}
SUPPORTED_TYPES = frozenset(SUPPORTED_VERSIONS)
+561
View File
@@ -0,0 +1,561 @@
"""Static C lowering for the complete built-in component catalog.
Python constructs the graph and eliminates constant linear constraints once.
All thermodynamics, flow/stream closure and derivatives execute in the EXE.
"""
from __future__ import annotations
import json
from importlib import import_module
from .compiler import NativeCapabilityError, NativeProgram, _Groups, _number as num
from .contracts import SUPPORTED_VERSIONS
GAS_TYPES = {'amesim_pnch023', 'amesim_pnch012', 'amesim_pnl0001',
'amesim_pnl0002', 'amesim_pnl0003', 'cylinder', 'tank'}
NODES = {'amesim_pn3node2', 'amesim_p4node2', 'tee'}
RESISTORS = {'amesim_pnor001', 'amesim_pnvo001_fixed', 'amesim_pnvo001',
'amesim_pnl00r', 'pipe', 'orifice'}
def catalog_contracts():
from app.simulation.components.amesim.library import LIBRARY as a
from app.simulation.components.experimental.library import LIBRARY as e
result = {}
for entry in (*a.models, *e.models):
module, name = entry.split(':')
cls = getattr(import_module(module), name)
result[cls.MODEL_TYPE] = cls
return result
def linear_schedule(equations, unknowns, free_flows=()):
"""Eliminate constant coefficients; retain RHS expressions as C temporaries.
Exact pivot elimination avoids a numeric pseudoinverse and its tiny spurious
dependencies. Redundant rows are left to the nodal pressure closure.
"""
rows = [[dict(a), {i: 1.0}] for i, (a, _) in enumerate(equations)]
pivots = []
for key in unknowns:
found = next((i for i in range(len(pivots), len(rows)) if abs(rows[i][0].get(key, 0)) > 1e-14), None)
if found is None and key in free_flows:
# Ideal coupled pipe compliances have a redundant internal flow.
# Their total m/U derivative is distributed by physical volume.
index = len(equations)
equations.append(({key: 1.0}, '0.0'))
rows.append([{key: 1.0}, {index: 1.0}])
found = len(rows)-1
if found is None:
raise NativeCapabilityError(f'Underdetermined native connection constraint: {key}')
j = len(pivots)
rows[j], rows[found] = rows[found], rows[j]
a, b = rows[j]
pivot = a[key]
rows[j] = [{k: v/pivot for k, v in a.items()}, {k: v/pivot for k, v in b.items()}]
for i, (a, b) in enumerate(rows):
if i == j:
continue
scale = a.get(key, 0)
if not scale:
continue
for target, source in zip((a, b), rows[j]):
for k, v in source.items():
value = target.get(k, 0) - scale*v
if abs(value) < 1e-14:
target.pop(k, None)
else:
target[k] = value
pivots.append(key)
lines = [f'double b{i} = {expr};' for i, (_, expr) in enumerate(equations)
if any(i in rows[j][1] for j in range(len(pivots)))]
for j, key in enumerate(pivots):
expr = ' + '.join(f'({num(v)})*b{i}' for i, v in rows[j][1].items()) or '0.0'
lines.append(f'{key} = {expr};')
return lines
def compile_extended_program(network):
components = list(network.components.values())
contracts = catalog_contracts()
for c in components:
if type(c) is not contracts.get(c.model_type):
raise NativeCapabilityError(f'{c.name}: no native contract for {c.model_type} / {type(c).__name__}')
if c.MODEL_VERSION != SUPPORTED_VERSIONS.get(c.model_type):
raise NativeCapabilityError(f'{c.name}: native kernel version does not match the component contract')
variables = tuple(v for c in components for v in c.result_variable_metadata())
if not variables:
raise NativeCapabilityError('Simulation requires a runtime component; medium definitions alone have no outputs')
slots = {v.key: i for i, v in enumerate(variables)}
ports = {(c.name, p.name): p for c in components for p in c.active_port_definitions}
groups = _Groups(ports)
adjacent = {}
for edge in network.connections:
a, b = (p.key for p in edge.endpoints)
if edge.kind == 'physical':
adjacent[a], adjacent[b] = b, a
groups.union(a, b)
else:
source, target = (a, b) if ports[a].nominal_role == 'output' else (b, a)
adjacent[target] = source
for c in components:
for port in c.required_connection_ports:
if (c.name, port) not in adjacent:
raise NativeCapabilityError(f'{c.name}.{port}: unconnected required port')
names = [p.name for p in c.active_port_definitions]
if c.model_type in NODES | {'amesim_pnch023', 'amesim_pnch012', 'amesim_mecmas21', 'amesim_lmechn1'} or (c.model_type=='pipe' and c.lambda_darcy==0):
for p in names[1:]:
groups.union((c.name, names[0]), (c.name, p))
if c.model_type == 'amesim_pnrp17':
for a, b in [('port_2', 'port_5'), ('port_3', 'port_4')]:
groups.union((c.name, a), (c.name, b))
state_keys, initial, gas_initializers = [], [], []
states = {}
def add_states(c, fields, values):
for field, value in zip(fields, values):
states[c.name, field] = len(state_keys)
state_keys.append(f'{c.name}.{field}')
initial.append(float(value))
mass_groups = {}
for c in components:
if c.model_type in GAS_TYPES:
fields = ('m1', 'U1', 'm2', 'U2') if c.model_type == 'amesim_pnl0003' else ('m', 'U')
add_states(c, fields, [0.0]*len(fields))
elif c.model_type == 'amesim_mecmas21':
root = groups.find((c.name, 'port_1'))
mass_groups.setdefault(root, []).append(c)
if len(mass_groups[root]) == 1:
add_states(c, ('v', 'x'), (c.v0, c.x0))
else:
ref = mass_groups[root][0]
if abs(c.v0-ref.v0)>1e-10*max(abs(c.v0),1) or abs(c.x0-ref.x0)>1e-10*max(abs(c.x0),1):
raise NativeCapabilityError('Rigidly connected masses require consistent initial x/v')
for field in ('v', 'x'):
states[c.name, field] = states[ref.name, field]
if len(state_keys)>1024 or len(variables)>16384:
raise NativeCapabilityError('Native model exceeds the 1024-state / 16384-output resource limit')
# Algebraic models use an internal constant state; the public state map stays empty.
nstates = max(len(state_keys), 1)
if not initial:
initial = [0.0]
lines, declarations, breaks = [], [], []
assigned = set()
def w(c, field):
name = c if isinstance(c, str) else c.name
return f'w[{slots[name+"."+field]}]'
def put(c, field, expr, dest=None):
(lines if dest is None else dest).append(f'{w(c,field)} = {expr};')
assigned.add((c if isinstance(c,str) else c.name)+'.'+field)
def y(c, field):
return f'y[{states[c.name,field]}]'
def ep(c, port):
return c.name, port
def pnames(c):
return [p.name for p in c.active_port_definitions if p.domain == 'pneumatic']
def mnames(c):
return [p.name for p in c.active_port_definitions if p.domain == 'mechanical']
for c in components:
if c.model_type == 'amesim_mecmas21':
for f in ('v', 'x'):
put(c, f, y(c, f))
for name in mnames(c):
root = groups.find(ep(c, name))
if root not in mass_groups:
raise NativeCapabilityError(f'{c.name}.{name}: mechanical group has no inertia anchor')
mass = mass_groups[root][0]
for f in ('v', 'x'):
put(c, name+'.'+f, y(mass, f))
if c.model_type == 'amesim_step0':
put(c, 'y', f't < {num(c.time)} ? {num(c.initial)} : {num(c.final)}')
breaks.append(f'if(t < {num(c.time)}) result=fmin(result,{num(c.time)});')
elif c.model_type == 'amesim_ud00':
ident = 'signal_'+str(len(declarations))
declarations.append(f'static const double {ident}[24] = {{'+','.join(num(v) for vs in (c.starts,c.ends,c.durations) for v in vs)+'};')
args=f'{num(c.tstart)}, {c.nstages}, {int(c.iscyclic)}, {ident}'
put(c, 'y', f'native_signal(t, {args})')
breaks.append(f'result=fmin(result,native_signal_break(t,end,{args}));')
else:
continue
put(c, 'out.signal', w(c, 'y'))
for c in components:
for port in c.active_port_definitions:
if port.kind == 'signal' and port.nominal_role == 'input':
target = adjacent.get(ep(c, port.name))
if target:
expr = w(target[0], target[1]+'.signal')
elif c.model_type == 'amesim_pnvo001':
expr = num(c.opening0)
else:
raise NativeCapabilityError(f'{c.name}.{port.name}: signal input missing')
put(c, port.name+'.signal', expr)
media = {}
def medium(c):
m = c.medium
key = (getattr(m, 'SUBSTANCE_ID', None), getattr(m, 'PROPERTY_METHOD_ID', None),
m.R_gas, m.cp_ref, m.T_ref, m.cp_slope, m.viscosity_ref, m.viscosity_T_ref, m.sutherland_constant)
if key not in media:
if key[1] not in (None, 'ideal_gas', 'peng_robinson') or (key[1]=='peng_robinson' and key[0]!='helium'):
raise NativeCapabilityError(f'{c.name}: unsupported medium contract {key[:2]}')
ident = f'medium_{len(media)}'
declarations.append(f'static const NativeMedium {ident} = {{'+str(int(key[1]=='peng_robinson'))+','+','.join(num(v) for v in key[2:])+'};')
media[key]=ident
return '&'+media[key]
pistons = [c for c in components if c.model_type == 'amesim_pnrp17']
for c in pistons:
put(c, 'length', f'{num(c.x0)}+{w(c,"port_5.x")}-{w(c,"port_4.x")}')
put(c, 'volume', f'{num(c.effective_area)}*{w(c,"length")}')
put(c, 'volume_flow', f'{num(c.effective_area)}*({w(c,"port_5.v")}-{w(c,"port_4.v")})')
pneu = [endpoint for endpoint, port in ports.items() if port.domain == 'pneumatic']
pi = {endpoint: i for i, endpoint in enumerate(pneu)}
pgroups = list(dict.fromkeys(groups.find(endpoint) for endpoint in pneu))
pgi = {root: i for i, root in enumerate(pgroups)}
def p(c, name): return f'p[{pgi[groups.find(ep(c,name))]}]'
def q(c, name): return f'q[{pi[ep(c,name)]}]'
def h(c, name): return f'h[{pi[ep(c,name)]}]'
def hin(c, name, temperature=False):
other = adjacent[ep(c,name)]
obj = network.components[other[0]]
if temperature and obj.model_type in NODES-{'tee'}:
other = adjacent[(obj.name, 'port_2')]
return f'h[{pi[other]}]'
gases, anchor, port_gas, volume_rate = {}, {}, {}, {}
anchor_partitions = {}
gas_count = 0
for c in components:
if c.model_type not in GAS_TYPES:
continue
kind = c.model_type
if kind == 'amesim_pnch023':
volume, rate = num(c.cvol), '0.0'
elif kind == 'amesim_pnch012':
attached = [d for d in pistons if adjacent[ep(d,'port_1')][0] == c.name]
volume = num(c.cvol0+sum(c.external_volumes.values()))+''.join('+'+w(d,'volume') for d in attached)
put(c, 'vol', f'fmax({num(c.cvol0/100)}, {volume})')
rate = num(sum(c.external_volume_rates.values()))+''.join('+'+w(d,'volume_flow') for d in attached)
put(c, 'dvol', f'{w(c,"vol")} <= {num(c.cvol0/100)} ? 0.0 : ({rate})')
volume, rate = w(c,'vol'), w(c,'dvol')
elif kind in ('cylinder', 'tank'):
volume, rate = num(c.V), '0.0'
else:
volume, rate = num(c.volume), '0.0'
volume_rate[c.name] = rate
halves = (1,2) if kind == 'amesim_pnl0003' else (0,)
for half in halves:
suffix = str(half) if half else ''
gas = f'g[{gas_count}]';gas_count += 1
gases[c.name,half] = gas
V = num(c.compliance_volume) if half else volume
if half:
p0,T0=c.parameter_values[f'p{half}_0'],c.parameter_values[f'T{half}_0']
initial_volume=c.compliance_volume
else:
p0,T0=c.parameter_values['p0'],c.parameter_values['T0']
initial_volume=(max(c.cvol0+sum(c.external_volumes.values()),c.cvol0/100)
if kind=='amesim_pnch012' else
c.cvol if kind=='amesim_pnch023' else c.V if kind in ('cylinder','tank') else c.volume)
gas_initializers.append(f'if(!native_medium_init({medium(c)},{num(p0)},{num(T0)},{num(initial_volume)},{int(kind in ("cylinder","tank"))},&y[{states[c.name,"m"+suffix]}])) return 0;')
lines.append(f'if(!native_medium_gas({medium(c)}, {y(c,"m"+suffix)}, {y(c,"U"+suffix)}, {V}, &{gas})) return 0;')
for field in ('m', 'U'):
put(c, field+suffix, y(c, field+suffix))
for field in ('p','T','rho','u','h'):
put(c, field+suffix, gas+'.'+field)
anchored = pnames(c)
if kind == 'amesim_pnl0001': anchored=['port_2']
if kind == 'amesim_pnl0002': anchored=[]
if half: anchored=['port_'+suffix]
for name in anchored:
root=groups.find(ep(c,name))
anchor[root]=gas
partition=(c.name,half)
anchor_partitions.setdefault(root, {})[partition]=(c, float(c.compliance_volume if half else c.volume) if kind in ('amesim_pnl0001','amesim_pnl0003') else None)
for name in (['port_'+suffix] if half else pnames(c)):
port_gas[ep(c,name)]=gas
coupled=[]
project=[]
for root,partitions in anchor_partitions.items():
if len(partitions)<2: continue
if any(volume is None for _,volume in partitions.values()) or len({id(c.medium) for c,_ in partitions.values()})!=1:
raise NativeCapabilityError('Direct gas-storage coupling requires compatible fixed pipe compliances; insert a resistance between independent chambers')
offsets=[];volumes=[]
for (name,half),(c,volume) in partitions.items():
offsets.append(states[name,'m'+(str(half) if half else '')]);volumes.append(volume)
for prefix in ('p','T'):
values=[c.parameter_values[f'{prefix}{half}_0'] if half else getattr(c,prefix+'0')
for (_,half),(c,_) in partitions.items()]
if max(values)-min(values)>1e-9*max(1,*map(abs,values)):
raise NativeCapabilityError('Ideally coupled pipe compliances require consistent initial pressure and temperature')
total=sum(volumes)
project.append('{ double mass='+ '+'.join(f'y[{i}]' for i in offsets)+',energy='+ '+'.join(f'y[{i+1}]' for i in offsets)+';')
for i,volume in zip(offsets,volumes):
project += [f'projected[{i}]=mass*{num(volume/total)};projected[{i+1}]=energy*{num(volume/total)};']
project.append('}')
coupled.append((root,offsets,volumes))
for root, gas in anchor.items():
lines.append(f'p[{pgi[root]}]={gas}.p;')
default_h = next(iter(gases.values()))+'.h' if gases else '0.0'
for endpoint, idx in pi.items():
lines.append(f'h[{idx}]={port_gas.get(endpoint,default_h.removesuffix(".h"))}.h;' if endpoint in port_gas else f'h[{idx}]={default_h};')
for c in components:
if c.model_type in {'amesim_pnpl01','amesim_pnrp17'}:
# Closed-end ports retain their declared zero outflow enthalpy.
lines.append(f'{h(c,"port_1")}=0.0;')
flow_lines, flow_known, flow_eq = [], set(), []
def flow(c, name, expr):
target=q(c,name);flow_lines.append(f'{target}={expr};');flow_known.add(target)
def flow_equation(terms):
flow_eq.append(({q(c,name):coef for c,name,coef in terms},'0.0'))
for c in components:
kind=c.model_type
names=pnames(c)
if kind in RESISTORS or kind in NODES:
flow_equation([(c,name,1) for name in names])
if kind in {'amesim_pnpl01','amesim_pnrp17'}:
flow(c,'port_1','0.0')
if kind in RESISTORS:
a,b=names
pa,pb=p(c,a),p(c,b)
if kind=='pipe' and c.lambda_darcy==0:
# A zero-loss pipe is an ideal connection, whose flow is
# determined by the neighbouring constitutive equations.
continue
if kind=='orifice':
flow(c,a,f'{num(c.K_eff)}*copysign(sqrt(fabs({pa}-{pb})),{pa}-{pb})')
elif kind=='pipe':
resistance=c.lambda_darcy*c.L/c.D
flow(c,a,f'copysign(sqrt(fabs({pa}-{pb})*2*fmax(native_density({medium(c)},fmax(.5*({pa}+{pb}),1),{num(c.T0)}),1e-12)*{num(c.area*c.area/resistance)}),{pa}-{pb})')
elif kind=='amesim_pnl00r':
T=f'native_temperature_ph({medium(c)},fmax(fmax({pa},{pb}),1),{pa}>={pb}?{hin(c,a,True)}:{hin(c,b,True)})'
flow(c,a,f'native_pipe_flow({medium(c)},{pa},{pb},{T},{num(c.diam)},{num(c.le)},{num(c.rr)},0)')
else:
opening = w(c,'xv') if kind!='amesim_pnor001' else '1.0'
if kind!='amesim_pnor001':
value = f'fmax(0,fmin(1,{w(c,"res.signal")}))' if kind=='amesim_pnvo001' else num(c.opening)
put(c,'xv',value)
area = c.effective_cq*(c.effective_area if kind=='amesim_pnor001' else c.maximum_area)
flow_lines.append(f'if(!native_medium_orifice({medium(c)},{pa},{pb},{hin(c,a)},{hin(c,b)},{num(area)},{opening},&{q(c,a)},&{w(c,"cm")},&{w(c,"gasvel")})) return 0;')
flow_known.add(q(c,a));assigned.update((c.name+'.cm',c.name+'.gasvel'))
flow(c,b,f'-{q(c,a)}')
elif kind in ('amesim_pnl0001','amesim_pnl0002'):
gas=gases[c.name,0]
for name in (['port_1'] if kind.endswith('1') else names):
T=gas+'.T'
if kind.endswith('2'):
T=f'({p(c,name)}>{gas}.p?native_temperature_ph({medium(c)},fmax({p(c,name)},1),{hin(c,name,True)}):{gas}.T)'
flow(c,name,f'native_pipe_flow({medium(c)},{p(c,name)},{gas}.p,{T},{num(c.diam)},{num(c.le/(2 if kind.endswith("2") else 1))},{num(c.rr)},1)')
for edge in network.connections:
if edge.domain=='pneumatic':
flow_eq.append(({f'q[{pi[e.key]}]':1 for e in edge.endpoints},'0.0'))
unknownq=[f'q[{i}]' for i in range(len(pneu)) if f'q[{i}]' not in flow_known]
reduced=[]
for terms,rhs in flow_eq:
known=''.join(f'-({num(v)})*{k}' for k,v in terms.items() if k in flow_known)
reduced.append(({k:v for k,v in terms.items() if k not in flow_known},rhs+known))
free_flows={f'q[{pi[e]}]' for root,_,_ in coupled for e in pneu if groups.find(e)==root}
flow_lines += linear_schedule(reduced,unknownq,free_flows)
unknownp=[root for root in pgroups if root not in anchor]
residuals=[]
for root in unknownp:
terms=[f'q[{pi[e]}]' for e in pneu if groups.find(e)==root and f'q[{pi[e]}]' in flow_known]
if not terms:
raise NativeCapabilityError('Unanchored pneumatic pressure group has no constitutive flow relation')
residuals.append(' + '.join(terms))
# A monotone nodal mass-balance solve. This is an algebraic connection
# closure; the integration solver's Jacobian policy is unchanged.
pressure_lines=[]
if unknownp:
if not anchor:
raise NativeCapabilityError('Pneumatic pressure network has no storage pressure anchor')
pressure_lines += ['double plo=INFINITY,phi=0;', *[f'plo=fmin(plo,{g}.p);phi=fmax(phi,{g}.p);' for g in anchor.values()]]
pressure_lines += [f'p[{pgi[root]}]=.5*(plo+phi);' for root in unknownp]
pressure_lines += ['int pressure_ok=0;', 'for(int sweep=0;sweep<256;sweep++) {']
for root,expr in zip(unknownp,residuals):
pressure_lines += ['{ double lo=plo,hi=phi;', 'for(int bisect=0;bisect<48;bisect++) {',f'p[{pgi[root]}]=.5*(lo+hi);',
'if(!model_flows(p,h,g,w,q)) return 0;', f'if(({expr})>0) hi=p[{pgi[root]}];else lo=p[{pgi[root]}];','}}']
pressure_lines += ['if(!model_flows(p,h,g,w,q)) return 0;', 'double residual=0;', *[f'residual=fmax(residual,fabs({expr}));' for expr in residuals],
'if(residual<1e-11) { pressure_ok=1;break; }','}', 'if(!pressure_ok) return 0;']
else:
pressure_lines=['if(!model_flows(p,h,g,w,q)) return 0;']
stream_lines=[]
for c in components:
names=pnames(c);kind=c.model_type
if kind in {'amesim_pnpl01','amesim_pnrp17'}:
stream_lines.append(f'{h(c,"port_1")}={hin(c,"port_1")};')
elif kind in RESISTORS:
a,b=names
stream_lines += [f'{h(c,a)}={hin(c,b)};',f'{h(c,b)}={hin(c,a)};']
elif kind in NODES:
stream_lines += ['{ double total=0,energy=0,average=0;', *[f'if({q(c,name)}>1e-12) {{total+={q(c,name)};energy+={q(c,name)}*{hin(c,name)};}} average+={hin(c,name)};' for name in names]]
if kind=='tee':
stream_lines += [f'double mixed=total>1e-12?energy/total:average/{len(names)};', *[f'{h(c,name)}=mixed;' for name in names]]
else:
stream_lines += [f'double ref={hin(c,"port_2")},mixed=total>1e-12?energy/total:ref;', *[f'{h(c,name)}=ref;' for name in names if name!='port_2'],f'{h(c,"port_2")}=mixed;',f'if({q(c,"port_2")}<0) {{ double e=0,scale=0;',
*[f'e+={q(c,name)}*({q(c,name)}>1e-12?{hin(c,name)}:ref);scale+=fabs({q(c,name)});' for name in names if name!='port_2'],
f'double flow={q(c,"port_2")},transition=fmax(.05*scale,1e-12);',
'double inv=-flow>=transition?1/flow:flow*(2*transition*transition-flow*flow)/pow(transition,4);',
f'{h(c,"port_2")}=mixed-(e+flow*mixed)*inv;','}']
# Nodes expose their reference temperature as an output too.
if c.name+'.T' in slots:
raise NativeCapabilityError('Unexpected node temperature output contract')
stream_lines += ['}']
if pneu:
lines += ['int closure_ok=0;',f'for(int closure=0;closure<{max(64,4*len(pneu))};closure++) {{',f'double previous[{len(pneu)}];',f'for(int i=0;i<{len(pneu)};i++) previous[i]=h[i];',*pressure_lines,*stream_lines,
'double change=0;',f'for(int i=0;i<{len(pneu)};i++) change=fmax(change,fabs(h[i]-previous[i])/fmax(1,fabs(h[i])));',
'if(change<1e-12) {closure_ok=1;break;}','}', 'if(!closure_ok) return 0;', 'if(!model_flows(p,h,g,w,q)) return 0;']
for c in components:
for name in pnames(c):
for field,expr in [('p',p(c,name)),('m_flow',q(c,name)),('h_outflow',h(c,name))]:
put(c,name+'.'+field,expr)
# Mechanical force balance includes shared accelerations for rigid groups.
feq=[]
for edge in network.connections:
if edge.domain=='mechanical':
feq.append(({w(e.component,e.port+'.f'):1 for e in edge.endpoints},'0.0'))
for c in components:
kind=c.model_type
if kind=='amesim_forc':
put(c,'force',f'{num(c.direction)}*{w(c,"res.signal")}')
feq.append(({w(c,'port_2.f'):1},'-'+w(c,'force')))
elif kind=='amesim_f000':
feq.append(({w(c,'port_1.f'):1},'0.0'))
elif kind=='amesim_lstp00a':
put(c,'gap',f'{num(c.gap0)}+{w(c,"port_2.x")}-{w(c,"port_1.x")}')
put(c,'penetration',f'fmax(-{w(c,"gap")},0)')
put(c,'force',f'native_contact({w(c,"penetration")},{w(c,"port_1.v")}-{w(c,"port_2.v")},{num(c.kcont)},{num(c.rcont)},{num(c.Pdis)},{int(c.discContactOption)})')
feq += [({w(c,'port_1.f'):1},w(c,'force')),({w(c,'port_2.f'):1},'-'+w(c,'force'))]
elif kind=='amesim_pnrp17':
put(c,'pressure_force',f'({w(c,"port_1.p")}-101300)*{num(c.effective_area)}')
feq += [({w(c,'port_2.f'):1,w(c,'port_5.f'):1},'-'+w(c,'pressure_force')),({w(c,'port_3.f'):1,w(c,'port_4.f'):1},w(c,'pressure_force'))]
elif kind=='amesim_lmechn1':
feq.append(({w(c,name+'.f'):1 for name in mnames(c)},'0.0'))
elif kind=='amesim_mecmas21':
v,x=w(c,'v'),w(c,'x')
put(c,'Fvisc',f'-{num(c.rvisc)}*{v}' if c.use_friction else '0.0')
put(c,'Ffric',f'{v}>0?-{num(c.fcoul)}:({v}<0?{num(c.fcoul)}:0)' if c.use_friction else '0.0')
for field,penetration,velocity,suffix in [('Fmin',num(c.xmin)+'-'+x,'-'+v,'min'),('Fmax',x+'-'+num(c.xmax),v,'max')]:
expr=f'native_limit_force({penetration},{velocity},{num(getattr(c,"Kb"+suffix))},{num(getattr(c,"Db"+suffix))},{num(getattr(c,"Pd"+suffix))},{int(c.discContactOption)})' if int(c.stoptype)==2 else '0.0'
put(c,field,expr)
ref=mass_groups[groups.find(ep(c,'port_1'))][0]
extra=f'{w(c,"Fvisc")}+{w(c,"Ffric")}+{w(c,"Fmin")}-{w(c,"Fmax")}'
if c.use_friction: extra+=f'-{num(c.wind)}*{v}*fabs({v})'
feq.append(({w(c,'port_1.f'):1,w(c,'port_2.f'):1,w(ref,'a'):-c.mass},f'-({extra})'))
unknownf=[w(c,name+'.f') for c in components for name in mnames(c)]+[w(group[0],'a') for group in mass_groups.values()]
lines += linear_schedule(feq,unknownf)
for c in components:
for name in mnames(c): assigned.add(c.name+'.'+name+'.f')
if c.model_type=='amesim_lmechn1':
put(c,'tforce',' + '.join(w(c,name+'.f') for name in mnames(c)[:-1]))
stops=[]
for group in mass_groups.values():
ref=group[0];vi=states[ref.name,'v'];xi=states[ref.name,'x']
limits=[c for c in group if int(c.stoptype) in (1,3)]
lines += [f'dy[{vi}]={w(ref,"a")};dy[{xi}]={y(ref,"v")};']
if limits:
lower=max(c.xmin for c in limits);upper=min(c.xmax for c in limits)
if lower>upper or ref.x0<lower-1e-12 or ref.x0>upper+1e-12:
raise NativeCapabilityError('Inconsistent discrete endstop bounds or initial position')
restitution, thresholds = [], []
for parameter, bound in [('xmin',lower),('xmax',upper)]:
active=[c for c in limits if abs(getattr(c,parameter)-bound)<=1e-12*max(abs(bound),1)]
restitution.append(0 if any(int(c.stoptype)==1 for c in active) else min(c.restcoeff for c in active))
thresholds.append(max((c.restdvel for c in active if int(c.stoptype)==3),default=0))
stops.append((vi,lower,upper,*restitution,*thresholds))
lines.append(f'native_stop_motion({y(ref,"x")},{y(ref,"v")},{num(lower)},{num(upper)},&dy[{vi}],&dy[{xi}]);')
for c in group: put(c,'a',f'dy[{vi}]')
for c in components:
kind=c.model_type
if kind not in GAS_TYPES and kind!='amesim_pnl00r': continue
if kind in GAS_TYPES:
halves=(1,2) if kind=='amesim_pnl0003' else (0,)
center='0.0'
if kind=='amesim_pnl0003':
a,b=gases[c.name,1],gases[c.name,2]
center=w(c,'dmctr')
put(c,'dmctr',f'native_pipe_flow({medium(c)},{a}.p,{b}.p,{a}.p>={b}.p?{a}.T:{b}.T,{num(c.diam)},{num(c.le)},{num(c.rr)},3)')
for half in halves:
gas=gases[c.name,half];suffix=str(half) if half else ''
names=['port_'+suffix] if half else pnames(c)
mass=' + '.join(q(c,name) for name in names)
energy=' + '.join(f'{q(c,name)}*({q(c,name)}>0?{hin(c,name)}:{gas}.h)' for name in names)
if half:
sign='-' if half==1 else '+'
mass+=sign+center
energy+=f'{sign}{center}*({center}>0?{gases[c.name,1]}.h:{gases[c.name,2]}.h)'
heat='0.0'
if kind.startswith('amesim_pnch'):
heat=f'{num(c.kth*c.sth)}*({num(c.extemp)}-{gas}.T)-{gas}.p*({volume_rate[c.name]})'
elif kind.startswith('amesim_pnl') and int(c.mode)!=1:
temp=f'.5*({gases[c.name,1]}.T+{gases[c.name,2]}.T)' if half else gas+'.T'
heat=f'{num(c.kth*c.exchange_area/(2 if half else 1))}*({num(c.extemp)}-({temp}))'
lines += [f'dy[{states[c.name,"m"+suffix]}]={mass};',f'dy[{states[c.name,"U"+suffix]}]={energy}+({heat});']
if kind.startswith('amesim_pnl'):
diag=[]
if kind=='amesim_pnl0002':
gas=gases[c.name,0]
for name in pnames(c):
flow=q(c,name);pp=f'({flow}>=0?fmax({p(c,name)},1):fmax({gas}.p,1))'
temp=f'({flow}>=0?fmax(native_temperature_ph({medium(c)},{pp},{hin(c,name,True)}),1):{gas}.T)'
diag.append((flow,pp,temp,c.le/2,0))
elif kind=='amesim_pnl0003':
a,b=gases[c.name,1],gases[c.name,2];flow=w(c,'dmctr')
diag=[(flow,f'fmax(fmax({a}.p,{b}.p),1)',f'({flow}>=0?{a}.T:{b}.T)',c.le,1)]
else:
pa,pb=p(c,'port_1'),p(c,'port_2');pp=f'fmax(fmax({pa},{pb}),1)'
temp=gases[c.name,0]+'.T' if kind=='amesim_pnl0001' else f'fmax(native_temperature_ph({medium(c)},{pp},{pa}>={pb}?{hin(c,"port_1",True)}:{hin(c,"port_2",True)}),1)'
diag=[(q(c,'port_1'),pp,temp,c.le,0)]
lines.append('{ double d[4],acc[4]={0};')
for flow,pp,temp,length,diagnostic in diag:
lines.append(f'native_pipe_diagnostics({medium(c)},{flow},{pp},{temp},{num(c.diam)},{num(length)},{num(c.rr)},{diagnostic},d);')
if len(diag)>1: lines.append('d[2]=fabs(d[2]);')
lines.append('for(int i=0;i<4;i++) acc[i]+=d[i];')
for i,field in enumerate(('re','cm','v','ff')):
expr=f'acc[{i}]/{len(diag)}'
put(c,field,f'fmin({expr},64000000)' if field=='ff' else expr)
lines.append('}')
for _,offsets,volumes in coupled:
lines.append('{ double mass='+ '+'.join(f'dy[{i}]' for i in offsets)+',energy='+ '+'.join(f'dy[{i+1}]' for i in offsets)+';')
for i,volume in zip(offsets,volumes):
lines.append(f'dy[{i}]=mass*{num(volume/sum(volumes))};dy[{i+1}]=energy*{num(volume/sum(volumes))};')
lines.append('}')
missing=set(slots)-assigned
if missing: raise NativeCapabilityError(f'Native output mapping incomplete: {sorted(missing)}')
if not state_keys: lines.append('dy[0]=0;')
np,ng,nq=max(1,len(pgroups)),max(1,gas_count),max(1,len(pneu))
source='\n'.join(['#include "model.h"','#include <math.h>',*declarations,
f'const NativeStop model_stops[{max(1,len(stops))}] = {{'+(','.join('{'+str(s[0])+','+','.join(num(v) for v in s[1:])+'}' for s in stops) or '{0,0,0,0,0,0,0}')+'};',
'const double model_atol[NSTATES] = {'+','.join('1e-12' if k.endswith(('.v','.x')) else '1e-8' for k in state_keys or ['dummy'])+'};',
'const char *const model_output_keys[NOUTPUTS] = {'+(','.join(json.dumps(v.key,ensure_ascii=True) for v in variables) or '""')+'};',
'static int model_flows(const double *p,const double *h,const NativeGas *g,double *w,double *q) {',
'(void)p;(void)h;(void)g;(void)w;(void)q;',*flow_lines,'return 1;}',
'int model_init(double *y) {',*[f'y[{i}]={num(v)};' for i,v in enumerate(initial)],*gas_initializers,'return 1;}',
'int model_eval(double t,const double *y,double *dy,double *w) {',
*(['double projected[NSTATES];for(int i=0;i<NSTATES;i++) projected[i]=y[i];',*project,'y=projected;'] if project else []),
f'double p[{np}]={{0}},h[{nq}]={{0}},q[{nq}]={{0}};NativeGas g[{ng}];',
'(void)t;(void)y;(void)w;(void)p;(void)h;(void)q;(void)g;(void)model_flows;',*lines,
'for(int i=0;i<NSTATES;i++) if(!isfinite(dy[i])) return 0;',
'for(int i=0;i<NOUTPUTS;i++) if(!isfinite(w[i])) return 0;','return 1;}',
'double model_next_break(double t,double end) { double result=end;(void)t;',*breaks,'return result;}',''])
header=f'''#ifndef GENERATED_NATIVE_MODEL_H
#define GENERATED_NATIVE_MODEL_H
#include "kernels.h"
#define NSTATES {nstates}
#define NOUTPUTS {max(1,len(variables))}
#define NSTOPS {len(stops)}
extern const NativeStop model_stops[{max(1,len(stops))}];
extern const double model_atol[NSTATES];
extern const char *const model_output_keys[NOUTPUTS];
int model_init(double *y);
int model_eval(double t,const double *y,double *dy,double *w);
double model_next_break(double t,double end);
#endif
'''
return NativeProgram(source,header,tuple(state_keys),variables,tuple(sorted({c.model_type for c in components})))
+90
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@@ -0,0 +1,90 @@
"""CLI input adapter; XML stays the numerical backend's execution contract."""
from __future__ import annotations
import ast
from copy import deepcopy
import json
from math import isfinite
import operator
from pathlib import Path
from app.system_xml import validate_system_xml_document
# Matches the editor's displayed-unit conversions. Stored numeric values are
# already SI; only arithmetic expressions are evaluated in the selected unit.
_SCALES = {
"area": {"m2": 1, "cm2": 1e-4, "mm2": 1e-6},
"length": {"m": 1, "cm": .01, "mm": .001},
"pressure": {"Pa": 1, "kPa": 1e3, "MPa": 1e6, "bar": 1e5},
"volume": {"m3": 1, "L": .001, "mL": 1e-6},
}
_OPERATIONS = {ast.Add: operator.add, ast.Sub: operator.sub, ast.Mult: operator.mul,
ast.Div: operator.truediv, ast.Pow: operator.pow}
def arithmetic_value(source: str) -> float:
"""Bounded arithmetic only: never evaluate code, names or function calls."""
source = source.strip().removeprefix("=").strip()
if len(source) > 512:
raise ValueError("Parameter expression exceeds 512 characters.")
tree = ast.parse(source, mode="eval")
if sum(1 for _ in ast.walk(tree)) > 256:
raise ValueError("Parameter expression is too complex.")
def visit(node, depth=0):
if depth > 32:
raise ValueError("Parameter expression is nested too deeply.")
if isinstance(node, ast.Constant) and type(node.value) in (int, float):
result = float(node.value)
elif isinstance(node, ast.UnaryOp) and type(node.op) in (ast.UAdd, ast.USub):
result = visit(node.operand, depth+1) * (-1 if isinstance(node.op, ast.USub) else 1)
elif isinstance(node, ast.BinOp) and type(node.op) in _OPERATIONS:
a, b = visit(node.left, depth+1), visit(node.right, depth+1)
if isinstance(node.op, ast.Pow) and abs(b) > 16:
raise ValueError("CLI parameter exponents must be between -16 and 16.")
result = _OPERATIONS[type(node.op)](a, b)
else:
raise ValueError("CLI supports arithmetic expressions only; export complex expressions as XML from the editor.")
if not isinstance(result, (int, float)) or not isfinite(result):
raise ValueError("Parameter expression must produce a finite real number.")
return result
return float(visit(tree.body))
def project_xml(data: dict) -> bytes:
from app.main import ReactFlowProjectPayload, build_reactflow_system_xml
from app.simulation.registry import get_component_model_spec
normalized = deepcopy(data)
for node in normalized.get("nodes", []):
model = node["data"]
spec = get_component_model_spec(model["modelType"])
for name, value in list(model.get("parameters", {}).items()):
if not isinstance(value, str):
continue
try:
number = float(value)
except ValueError:
definition = spec.parameter_by_name[name]
if definition.editor:
raise ValueError(f"{node['id']}.{name}: a discrete parameter cannot be an expression.")
number = arithmetic_value(value)
unit = model.get("parameterUnits", {}).get(name, definition.unit)
if definition.quantity in _SCALES:
if unit not in _SCALES[definition.quantity]:
raise ValueError(f"Unsupported parameter unit: {unit}.")
number *= _SCALES[definition.quantity][unit]
elif definition.quantity == "temperature" and unit == "degC":
number += 273.15
elif unit != definition.unit:
raise ValueError(f"Unsupported parameter unit: {unit}.")
if not isfinite(number):
raise ValueError(f"{node['id']}.{name}: parameter must be finite.")
model["parameters"][name] = number
return build_reactflow_system_xml(ReactFlowProjectPayload.model_validate(normalized))
def load_input(path: Path):
xml = project_xml(json.loads(path.read_text(encoding="utf-8"))) if path.suffix.lower() == ".json" else path.read_bytes()
report = validate_system_xml_document(xml)
if not report.valid or report.document is None:
raise ValueError(f"Invalid simulation XML: {report.as_dict()}")
return xml, report.document
+128
View File
@@ -0,0 +1,128 @@
"""Isolated native numerical execution; Python only handles process I/O."""
from __future__ import annotations
import json
import os
from pathlib import Path
import queue
import subprocess
import tempfile
import threading
import time
from app.simulation.config import SolveIVPConfig
from app.simulation.results import GenericSimulationResult
from .build import NativeBuild, build_native
from .compiler import NativeCapabilityError, compile_native_program
def execute_native(build: NativeBuild, config: SolveIVPConfig, sample_step: float, *,
run_dir: Path, record_samples=True, cancel_check=None,
progress_callback=None, activity_tracker=None, timeout=300.0) -> dict:
if config.method not in ("RK45", "BDF"):
raise NativeCapabilityError(f"Native v1 does not support method {config.method}.")
if not isinstance(config.atol, (int, float)) or config.atol != 1e-8 or config.first_step is not None:
raise NativeCapabilityError("Native v1 uses the existing default gas/mechanical absolute tolerances and automatic initial step.")
run_dir.mkdir(parents=True, exist_ok=True)
output = run_dir / "result.json"
cancel_path = run_dir / "cancel.request"
if output.exists() or cancel_path.exists():
raise ValueError("Native execution requires a fresh run directory.")
command = [str(build.executable), "--method", config.method,
"--start", str(config.t_start), "--stop", str(config.t_stop),
"--sample-step", str(sample_step), "--max-step", str(config.max_step),
"--rtol", str(config.rtol), "--timeout", str(timeout),
"--cancel-file", str(cancel_path.resolve()), "--output", str(output.resolve())]
if not record_samples:
command.append("--solve-only")
creationflags = subprocess.CREATE_NO_WINDOW if os.name == "nt" else 0
started = time.perf_counter()
process = subprocess.Popen(command, cwd=build.executable.parent, stdin=subprocess.DEVNULL,
stdout=subprocess.DEVNULL, stderr=subprocess.PIPE,
text=True, encoding="utf-8", errors="replace", creationflags=creationflags)
messages: queue.Queue[str] = queue.Queue()
def read_stderr():
assert process.stderr is not None
for line in process.stderr:
messages.put(line)
reader = threading.Thread(target=read_stderr, daemon=True)
reader.start()
if activity_tracker is not None:
activity_tracker.start_integration(config.t_start)
cancelled_at = None
last_time = config.t_start
try:
with (run_dir / "worker.log").open("w", encoding="utf-8") as log:
while process.poll() is None or not messages.empty() or reader.is_alive():
now = time.perf_counter()
if cancel_check is not None and cancel_check() and cancelled_at is None:
cancel_path.write_text("cancel\n", encoding="ascii")
cancelled_at = now
if now-started > timeout+5 or (cancelled_at is not None and now-cancelled_at > 5):
process.kill()
process.wait(timeout=5)
raise RuntimeError("Native worker was terminated after failing to return within its time limit.")
try:
line = messages.get(timeout=0.05)
except queue.Empty:
continue
log.write(line)
try:
event = json.loads(line)
except json.JSONDecodeError:
continue
if event.get("phase") == "integrating":
last_time = max(last_time, min(config.t_stop, float(event["time"])))
if progress_callback:
progress_callback((last_time-config.t_start)/(config.t_stop-config.t_start), "integrating")
if activity_tracker is not None:
activity_tracker.record_native_progress(last_time, int(event["nfev"]), int(event["acceptedSteps"]))
finally:
if process.poll() is None:
process.kill()
process.wait(timeout=5)
reader.join(timeout=2)
if process.stderr is not None:
process.stderr.close()
if not output.is_file():
raise RuntimeError(f"Native worker exited with code {process.returncode} without results; see {run_dir / 'worker.log'}.")
payload = json.loads(output.read_text(encoding="utf-8"))
if process.returncode not in (0, 2):
raise RuntimeError(f"Native worker failed with exit code {process.returncode}.")
payload["processWallSeconds"] = time.perf_counter()-started
payload["buildKey"] = build.manifest["buildKey"]
payload["cacheHit"] = build.cache_hit
payload["buildSeconds"] = build.seconds
if activity_tracker is not None:
activity_tracker.record_native_progress(payload["simulatedUntil"], payload["nfev"], payload["acceptedSteps"])
return payload
def simulate_native(network, config, *, sample_step, progress_callback=None,
cancel_check=None, activity_tracker=None):
if config.method not in ("RK45", "BDF"):
raise NativeCapabilityError(f"Native v1 does not support method {config.method}.")
if progress_callback:
progress_callback(0.0, "initializing")
program = compile_native_program(network)
build = build_native(program)
with tempfile.TemporaryDirectory(prefix="native-simulation-") as directory:
data = execute_native(build, config, sample_step, run_dir=Path(directory),
cancel_check=cancel_check, progress_callback=progress_callback,
activity_tracker=activity_tracker)
totals = {
"nfev": data["nfev"], "njev": data["njev"], "nlu": data["nlu"],
"acceptedStepCount": data["acceptedSteps"], "rejectedStepCount": data["rejectedSteps"],
"stateTransitionCount": data["stateTransitions"], "solverStartCount": data["solverStarts"],
}
if progress_callback:
fraction = (data["simulatedUntil"]-config.t_start)/(config.t_stop-config.t_start)
progress_callback(fraction, "complete" if data["success"] else data["status"])
return GenericSimulationResult(
success=data["success"], status=data["status"], message=data["message"],
simulated_until=data["simulatedUntil"], requested_stop_time=config.t_stop,
variables=program.variables, series=data["series"], final=data["final"],
diagnostics={"backend": "native-c", "native": {k: v for k, v in data.items()
if k not in ("series", "final", "finalState")}, "integration": {"method": config.method, "totals": totals},
"stateCount": len(program.state_keys), "sampleCount": len(data["series"]["time"])},
)
+62 -563
View File
@@ -1,32 +1,19 @@
"""Low-overhead, run-local performance instrumentation for simulations.
The profiling mode is intentionally read once when this module is imported.
``standard`` records low-frequency pipeline stages, while ``audit`` also wraps
hot RHS/property operations and computes exact-input reuse metrics. With
profiling disabled, decorators return the original callable while classes are
being defined, so ordinary simulation calls do not pass through a wrapper.
"""
"""Run-local timing of Python orchestration; numeric timings come from C."""
from __future__ import annotations
from collections.abc import Callable, Generator, Mapping
from contextlib import contextmanager
from contextvars import ContextVar, Token
from contextvars import ContextVar
from dataclasses import dataclass, field
from functools import wraps
import inspect
import os
import struct
from time import perf_counter_ns
from typing import Any, Literal, ParamSpec, TypeVar, cast
ProfileMode = Literal["off", "standard", "audit"]
_P = ParamSpec("_P")
_R = TypeVar("_R")
_MODE_RANK: Mapping[ProfileMode, int] = {"off": 0, "standard": 1, "audit": 2}
ProfileMode = Literal['off', 'standard', 'audit']
_P = ParamSpec('_P')
_R = TypeVar('_R')
_MODE_RANK: Mapping[ProfileMode, int] = {'off': 0, 'standard': 1, 'audit': 2}
def _read_startup_mode() -> ProfileMode:
raw_mode = os.getenv("SIMULATIONAPP_PROFILE", "off").strip().lower()
@@ -50,17 +37,12 @@ def _read_startup_mode() -> ProfileMode:
"SIMULATIONAPP_PROFILE must be one of: off, standard, audit."
) from exc
PROFILE_MODE: ProfileMode = _read_startup_mode()
def _minimum_mode(value: str) -> ProfileMode:
normalized = value.strip().lower()
if normalized not in _MODE_RANK:
raise ValueError("minimum_mode must be one of: off, standard, audit.")
return cast(ProfileMode, normalized)
def _mode_enabled(minimum_mode: ProfileMode) -> bool:
# ``off`` is an unconditional zero-wrapper mode, even if a caller passes
# ``minimum_mode="off"`` by mistake.
@@ -69,7 +51,6 @@ def _mode_enabled(minimum_mode: ProfileMode) -> bool:
and _MODE_RANK[PROFILE_MODE] >= _MODE_RANK[minimum_mode]
)
@dataclass
class _TimingStats:
calls: int = 0
@@ -95,311 +76,10 @@ class _TimingStats:
"errors": self.errors,
}
@dataclass
class _PropertyStats(_TimingStats):
operation: str = ""
layer: str = "semantic"
medium: str = "unknown"
exact_input_unique: int = 0
exact_input_repeats: int = 0
iteration_calls: int = 0
iteration_total: int = 0
iteration_max: int = 0
iteration_converged: int = 0
iteration_nonconverged: int = 0
cache_lookups: int = 0
cache_hits: int = 0
cache_misses: int = 0
def snapshot(self, *, audit: bool) -> dict[str, object]:
result: dict[str, object] = super().snapshot()
result.update(
{
"operation": self.operation,
"layer": self.layer,
"medium": self.medium,
"cacheLookups": self.cache_lookups,
"cacheHits": self.cache_hits,
"cacheMisses": self.cache_misses,
}
)
if audit:
result.update(
{
"exactInputUnique": self.exact_input_unique,
"exactInputRepeats": self.exact_input_repeats,
"iterationCalls": self.iteration_calls,
"iterationTotal": self.iteration_total,
"iterationMax": self.iteration_max,
"iterationConverged": self.iteration_converged,
"iterationNonconverged": self.iteration_nonconverged,
}
)
return result
@dataclass
class _ActiveSpan:
trace: PerformanceTrace
name: str
started_ns: int
property_key: str | None = None
property_operation: str | None = None
property_outermost: bool = False
child_ns: int = 0
@dataclass
class PerformanceTrace:
"""Mutable counters owned by exactly one :func:`profile_run` context."""
mode: ProfileMode
_phases: dict[str, _TimingStats] = field(default_factory=dict, repr=False)
_properties: dict[str, _PropertyStats] = field(default_factory=dict, repr=False)
_property_outermost_ns: int = field(default=0, repr=False)
@property
def enabled(self) -> bool:
return self.mode != "off"
def _property_stats(
self,
key: str,
*,
operation: str,
layer: str,
medium: str,
) -> _PropertyStats:
stats = self._properties.get(key)
if stats is None:
stats = _PropertyStats(
operation=operation,
layer=layer,
medium=medium,
)
self._properties[key] = stats
return stats
def _record_span(self, frame: _ActiveSpan, elapsed_ns: int, error: bool) -> None:
self_ns = max(0, elapsed_ns - frame.child_ns)
if frame.property_key is None:
stats = self._phases.setdefault(frame.name, _TimingStats())
else:
layer, medium, operation = frame.property_key.split("|", 2)
stats = self._property_stats(
frame.property_key,
operation=operation,
layer=layer,
medium=medium,
)
if frame.property_outermost:
self._property_outermost_ns += elapsed_ns
stats.record(elapsed_ns, self_ns, error)
def _record_exact_input(
self,
key: str,
*,
operation: str,
layer: str,
medium: str,
fingerprint: object,
) -> None:
stats = self._property_stats(
key,
operation=operation,
layer=layer,
medium=medium,
)
shadow_key = (key, fingerprint)
shadow = _PROPERTY_SHADOW.get()
if shadow is None:
# A trace normally installs its own set in ``profile_run``. Keep
# the ContextVar default immutable so no task can accidentally
# share a process-global shadow set.
shadow = set()
_PROPERTY_SHADOW.set(shadow)
if shadow_key in shadow:
stats.exact_input_repeats += 1
else:
shadow.add(shadow_key)
stats.exact_input_unique += 1
def _record_iterations(
self,
key: str,
*,
operation: str,
layer: str,
medium: str,
iterations: int,
converged: bool,
) -> None:
stats = self._property_stats(
key,
operation=operation,
layer=layer,
medium=medium,
)
iteration_count = max(0, int(iterations))
stats.iteration_calls += 1
stats.iteration_total += iteration_count
stats.iteration_max = max(stats.iteration_max, iteration_count)
if converged:
stats.iteration_converged += 1
else:
stats.iteration_nonconverged += 1
def _record_cache(
self,
key: str,
*,
operation: str,
layer: str,
medium: str,
hits: int,
misses: int,
) -> None:
stats = self._property_stats(
key,
operation=operation,
layer=layer,
medium=medium,
)
hit_delta = max(0, hits)
miss_delta = max(0, misses)
stats.cache_hits += hit_delta
stats.cache_misses += miss_delta
stats.cache_lookups += hit_delta + miss_delta
def snapshot(self) -> dict[str, object]:
"""Return a detached, JSON-serializable copy of all counters."""
audit = self.mode == "audit"
return {
"mode": self.mode,
"phases": {
name: self._phases[name].snapshot()
for name in sorted(self._phases)
},
"properties": {
_public_property_key(key): self._properties[key].snapshot(audit=audit)
for key in sorted(self._properties)
},
"propertyOutermostNs": self._property_outermost_ns,
}
_CURRENT_TRACE: ContextVar[PerformanceTrace | None] = ContextVar(
"simulation_performance_trace",
default=None,
)
_ACTIVE_SPANS: ContextVar[tuple[_ActiveSpan, ...]] = ContextVar(
"simulation_performance_spans",
default=(),
)
_PROPERTY_SHADOW: ContextVar[set[object] | None] = ContextVar(
"simulation_property_shadow",
default=None,
)
def _public_property_key(key: str) -> str:
layer, medium, operation = key.split("|", 2)
return f"{layer}.{medium}.{operation}"
@contextmanager
def _tracked_span(
trace: PerformanceTrace,
name: str,
*,
property_key: str | None = None,
property_operation: str | None = None,
reset_property_shadow: bool = False,
) -> Generator[None, None, None]:
stack = _ACTIVE_SPANS.get()
property_outermost = property_key is not None and not any(
item.property_key is not None for item in stack
)
frame = _ActiveSpan(
trace=trace,
name=name,
started_ns=perf_counter_ns(),
property_key=property_key,
property_operation=property_operation,
property_outermost=property_outermost,
)
stack_token = _ACTIVE_SPANS.set((*stack, frame))
shadow_token: Token[set[object] | None] | None = None
if reset_property_shadow and trace.mode == "audit":
shadow_token = _PROPERTY_SHADOW.set(set())
error = False
try:
yield
except BaseException:
error = True
raise
finally:
elapsed_ns = max(0, perf_counter_ns() - frame.started_ns)
_ACTIVE_SPANS.reset(stack_token)
if shadow_token is not None:
_PROPERTY_SHADOW.reset(shadow_token)
if stack:
stack[-1].child_ns += elapsed_ns
trace._record_span(frame, elapsed_ns, error)
@contextmanager
def profile_run() -> Generator[PerformanceTrace, None, None]:
"""Create and bind an isolated trace for one simulation run.
The yielded trace remains usable after the context exits, which lets the
caller attach ``trace.snapshot()`` to a result without exposing live state.
"""
trace = PerformanceTrace(mode=PROFILE_MODE)
trace_token = _CURRENT_TRACE.set(trace)
spans_token = _ACTIVE_SPANS.set(())
shadow_token = _PROPERTY_SHADOW.set(set())
try:
if trace.enabled:
with _tracked_span(trace, "simulation.total"):
yield trace
else:
yield trace
finally:
_PROPERTY_SHADOW.reset(shadow_token)
_ACTIVE_SPANS.reset(spans_token)
_CURRENT_TRACE.reset(trace_token)
@contextmanager
def performance_span(
name: str,
minimum_mode: str = "standard",
reset_property_shadow: bool = False,
) -> Generator[None, None, None]:
"""Time a block in the current run, or act as a no-op outside one."""
minimum = _minimum_mode(minimum_mode)
trace = _CURRENT_TRACE.get()
if trace is None or not _mode_enabled(minimum):
yield
return
with _tracked_span(
trace,
name,
reset_property_shadow=reset_property_shadow,
):
yield
def profile_phase(
name: str,
minimum_mode: str = "standard",
reset_property_shadow: bool = False,
) -> Callable[[Callable[_P, _R]], Callable[_P, _R]]:
"""Decorate a simulation phase while preserving the off-mode callable."""
@@ -419,7 +99,7 @@ def profile_phase(
with _tracked_span(
trace,
name,
reset_property_shadow=reset_property_shadow,
):
return await function(*args, **kwargs)
@@ -433,7 +113,7 @@ def profile_phase(
with _tracked_span(
trace,
name,
reset_property_shadow=reset_property_shadow,
):
return function(*args, **kwargs)
@@ -441,249 +121,68 @@ def profile_phase(
return decorate
PROFILE_MODE = _read_startup_mode()
def _medium_name(args: tuple[object, ...]) -> str:
if not args:
return "unknown"
owner = args[0]
configured_name = getattr(owner, "name", None)
if isinstance(configured_name, str) and configured_name:
return configured_name
return type(owner).__name__
@dataclass
class _ActiveSpan:
name: str
started_ns: int
child_ns: int = 0
@dataclass
class PerformanceTrace:
mode: ProfileMode
_phases: dict[str, _TimingStats] = field(default_factory=dict, repr=False)
def _fingerprint(value: object) -> object:
"""Build a hashable, bit-exact token without retaining arbitrary objects."""
@property
def enabled(self):
return self.mode != 'off'
if value is None or isinstance(value, (bool, int, str, bytes)):
return (type(value).__name__, value)
if isinstance(value, float):
return ("float64", struct.pack("!d", value))
if isinstance(value, tuple):
return ("tuple", tuple(_fingerprint(item) for item in value))
if isinstance(value, list):
return ("list", tuple(_fingerprint(item) for item in value))
if isinstance(value, Mapping):
items = [(_fingerprint(key), _fingerprint(item)) for key, item in value.items()]
items.sort(key=repr)
return ("mapping", tuple(items))
return (
"object",
type(value).__module__,
type(value).__qualname__,
id(value),
)
def snapshot(self):
return {'mode': self.mode, 'phases': {key: value.snapshot() for key, value in sorted(self._phases.items())}}
_CURRENT_TRACE = ContextVar('simulation_trace', default=None)
_ACTIVE_SPANS = ContextVar('simulation_spans', default=())
def _input_fingerprint(
signature: inspect.Signature | None,
args: tuple[object, ...],
kwargs: dict[str, object],
) -> object:
if signature is not None:
try:
bound = signature.bind(*args, **kwargs)
bound.apply_defaults()
return tuple(
(name, _fingerprint(value))
for name, value in bound.arguments.items()
)
except TypeError:
pass
return (
_fingerprint(args),
tuple(sorted((name, _fingerprint(value)) for name, value in kwargs.items())),
)
def _cache_counts(function: Callable[..., object]) -> tuple[int, int] | None:
cache_info = getattr(function, "cache_info", None)
if not callable(cache_info):
return None
@contextmanager
def _tracked_span(trace, name):
stack = _ACTIVE_SPANS.get()
frame = _ActiveSpan(name, perf_counter_ns())
token = _ACTIVE_SPANS.set((*stack, frame))
error = False
try:
info = cache_info()
return int(info.hits), int(info.misses)
except (AttributeError, TypeError, ValueError):
return None
yield
except BaseException:
error = True
raise
finally:
elapsed = max(0, perf_counter_ns()-frame.started_ns)
_ACTIVE_SPANS.reset(token)
if stack:
stack[-1].child_ns += elapsed
trace._phases.setdefault(name, _TimingStats()).record(elapsed, max(0, elapsed-frame.child_ns), error)
@contextmanager
def profile_run():
trace = PerformanceTrace(PROFILE_MODE)
token = _CURRENT_TRACE.set(trace)
spans = _ACTIVE_SPANS.set(())
try:
if trace.enabled:
with _tracked_span(trace, 'simulation.total'):
yield trace
else:
yield trace
finally:
_ACTIVE_SPANS.reset(spans)
_CURRENT_TRACE.reset(token)
def _copy_cache_api(source: Callable[..., object], target: Callable[..., object]) -> None:
for attribute in ("cache_clear", "cache_info", "cache_parameters"):
value = getattr(source, attribute, None)
if value is not None:
setattr(target, attribute, value)
def profile_property(
operation: str,
layer: str = "semantic",
minimum_mode: str = "audit",
capture_inputs: bool = True,
track_cache: bool = False,
) -> Callable[[Callable[_P, _R]], Callable[_P, _R]]:
"""Decorate one thermodynamic property operation."""
@contextmanager
def performance_span(name: str, minimum_mode: str = 'standard'):
minimum = _minimum_mode(minimum_mode)
def decorate(function: Callable[_P, _R]) -> Callable[_P, _R]:
if not _mode_enabled(minimum):
return function
try:
signature: inspect.Signature | None = inspect.signature(function)
except (TypeError, ValueError):
signature = None
def prepare(
args: tuple[object, ...],
kwargs: dict[str, object],
) -> tuple[PerformanceTrace | None, str, str, tuple[int, int] | None]:
trace = _CURRENT_TRACE.get()
medium = _medium_name(args)
key = f"{layer}|{medium}|{operation}"
if trace is not None and trace.mode == "audit" and capture_inputs:
trace._record_exact_input(
key,
operation=operation,
layer=layer,
medium=medium,
fingerprint=_input_fingerprint(signature, args, kwargs),
)
before = _cache_counts(function) if trace is not None and track_cache else None
return trace, medium, key, before
def finish_cache(
trace: PerformanceTrace | None,
medium: str,
key: str,
before: tuple[int, int] | None,
) -> None:
if trace is None or before is None:
return
after = _cache_counts(function)
if after is None:
return
trace._record_cache(
key,
operation=operation,
layer=layer,
medium=medium,
hits=after[0] - before[0],
misses=after[1] - before[1],
)
if inspect.iscoroutinefunction(function):
@wraps(function)
async def async_wrapper(*args: _P.args, **kwargs: _P.kwargs) -> Any:
object_args = cast(tuple[object, ...], args)
object_kwargs = cast(dict[str, object], kwargs)
trace, medium, key, before = prepare(object_args, object_kwargs)
try:
if trace is None:
return await function(*args, **kwargs)
with _tracked_span(
trace,
f"property.{_public_property_key(key)}",
property_key=key,
property_operation=operation,
):
return await function(*args, **kwargs)
finally:
finish_cache(trace, medium, key, before)
_copy_cache_api(function, async_wrapper)
return cast(Callable[_P, _R], async_wrapper)
@wraps(function)
def wrapper(*args: _P.args, **kwargs: _P.kwargs) -> _R:
object_args = cast(tuple[object, ...], args)
object_kwargs = cast(dict[str, object], kwargs)
trace, medium, key, before = prepare(object_args, object_kwargs)
try:
if trace is None:
return function(*args, **kwargs)
with _tracked_span(
trace,
f"property.{_public_property_key(key)}",
property_key=key,
property_operation=operation,
):
return function(*args, **kwargs)
finally:
finish_cache(trace, medium, key, before)
_copy_cache_api(function, wrapper)
return wrapper
return decorate
def record_property_iterations(
operation: str,
iterations: int,
converged: bool,
) -> None:
"""Record inverse-property solver iterations in audit mode."""
trace = _CURRENT_TRACE.get()
if trace is None or trace.mode != "audit":
if trace is None or not _mode_enabled(minimum):
yield
return
for frame in reversed(_ACTIVE_SPANS.get()):
if (
frame.property_key is not None
and frame.property_operation == operation
):
layer, medium, _unused_operation = frame.property_key.split("|", 2)
trace._record_iterations(
frame.property_key,
operation=operation,
layer=layer,
medium=medium,
iterations=iterations,
converged=converged,
)
return
key = f"semantic|unknown|{operation}"
trace._record_iterations(
key,
operation=operation,
layer="semantic",
medium="unknown",
iterations=iterations,
converged=converged,
)
def record_property_cache(operation: str, *, hit: bool) -> None:
"""Record one run-local property-cache lookup in audit mode."""
trace = _CURRENT_TRACE.get()
if trace is None or trace.mode != "audit":
return
for frame in reversed(_ACTIVE_SPANS.get()):
if (
frame.property_key is not None
and frame.property_operation == operation
):
layer, medium, _unused_operation = frame.property_key.split("|", 2)
trace._record_cache(
frame.property_key,
operation=operation,
layer=layer,
medium=medium,
hits=1 if hit else 0,
misses=0 if hit else 1,
)
return
__all__ = [
"PROFILE_MODE",
"PerformanceTrace",
"performance_span",
"profile_phase",
"profile_property",
"profile_run",
"record_property_cache",
"record_property_iterations",
]
with _tracked_span(trace, name):
yield
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-234
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"""Run-local, exact-key cache for expensive thermodynamic calculations.
The cache is deliberately bound to one simulation through ``ContextVar``.
That keeps concurrent runs isolated and releases all cached states when the
run finishes. Keys use the original Python values with no rounding or
tolerance-based reuse that could flatten numerical residuals seen by ODE and
nonlinear solvers.
"""
from __future__ import annotations
from collections.abc import Callable, Generator
from contextlib import contextmanager
from contextvars import ContextVar
from dataclasses import dataclass
from functools import lru_cache, wraps
import os
from typing import ParamSpec, TypeVar
from app.simulation.performance import PROFILE_MODE, record_property_cache
_P = ParamSpec("_P")
_R = TypeVar("_R")
DEFAULT_PROPERTY_CACHE_MAX_ENTRIES = 8192
def _read_cache_enabled() -> bool:
raw_value = os.getenv("SIMULATIONAPP_PROPERTY_CACHE", "on").strip().lower()
if raw_value in {"", "1", "true", "yes", "on"}:
return True
if raw_value in {"0", "false", "no", "off"}:
return False
raise ValueError(
"SIMULATIONAPP_PROPERTY_CACHE must be one of: on, off, true, false, 1, 0."
)
PROPERTY_CACHE_ENABLED = _read_cache_enabled()
@dataclass(frozen=True)
class PropertyCacheInfo:
hits: int
misses: int
max_entries_per_cache: int
cache_count: int
current_entries: int
evictions: int
class SimulationPropertyCache:
"""Bounded C-level LRUs owned by one simulation run."""
def __init__(self, max_entries: int = DEFAULT_PROPERTY_CACHE_MAX_ENTRIES) -> None:
if max_entries <= 0:
raise ValueError("Property cache max_entries must be positive.")
self.max_entries_per_cache = int(max_entries)
self._functions: dict[
tuple[str, int, Callable[..., object]],
Callable[..., object],
] = {}
self._failed_misses: dict[
tuple[str, int, Callable[..., object]],
int,
] = {}
self._owners: dict[int, tuple[object, int]] = {}
self._next_owner_token = 0
def owner_token(self, owner: object) -> int:
"""Return a stable identity token and retain its owner for this run."""
identity = id(owner)
existing = self._owners.get(identity)
if existing is not None and existing[0] is owner:
return existing[1]
self._next_owner_token += 1
self._owners[identity] = (owner, self._next_owner_token)
return self._next_owner_token
def get_or_compute(
self,
operation: str,
owner: object,
function: Callable[..., _R],
args: tuple[object, ...],
kwargs: dict[str, object],
) -> _R:
cache_key = (operation, self.owner_token(owner), function)
cached_function = self._functions.get(cache_key)
if cached_function is None:
@lru_cache(maxsize=self.max_entries_per_cache, typed=True)
def invoke(*cached_args: object, **cached_kwargs: object) -> _R:
return function(owner, *cached_args, **cached_kwargs)
cached_function = invoke
self._functions[cache_key] = cached_function
if PROFILE_MODE != "audit":
try:
return cached_function(*args, **kwargs)
except Exception:
self._failed_misses[cache_key] = (
self._failed_misses.get(cache_key, 0) + 1
)
raise
before = cached_function.cache_info() # type: ignore[attr-defined]
try:
value = cached_function(*args, **kwargs)
except Exception:
self._failed_misses[cache_key] = (
self._failed_misses.get(cache_key, 0) + 1
)
raise
finally:
after = cached_function.cache_info() # type: ignore[attr-defined]
hit = after.hits > before.hits
record_property_cache(operation, hit=hit)
return value
def info(self) -> PropertyCacheInfo:
cache_infos = {
key: cached.cache_info() # type: ignore[attr-defined]
for key, cached in self._functions.items()
}
return PropertyCacheInfo(
hits=sum(info.hits for info in cache_infos.values()),
misses=sum(info.misses for info in cache_infos.values()),
max_entries_per_cache=self.max_entries_per_cache,
cache_count=len(self._functions),
current_entries=sum(info.currsize for info in cache_infos.values()),
evictions=sum(
max(
0,
info.misses
- self._failed_misses.get(key, 0)
- info.currsize,
)
for key, info in cache_infos.items()
),
)
_CURRENT_PROPERTY_CACHE: ContextVar[SimulationPropertyCache | None] = ContextVar(
"simulation_property_cache",
default=None,
)
def current_property_cache() -> SimulationPropertyCache | None:
return _CURRENT_PROPERTY_CACHE.get()
@contextmanager
def property_cache_run(
*,
max_entries: int = DEFAULT_PROPERTY_CACHE_MAX_ENTRIES,
) -> Generator[SimulationPropertyCache | None, None, None]:
"""Bind a fresh cache to one top-level simulation run.
Nested uses reuse the existing cache so lower-level simulation helpers can
safely opt in without replacing the cache created by the API entry point.
"""
existing = _CURRENT_PROPERTY_CACHE.get()
if existing is not None:
yield existing
return
if not PROPERTY_CACHE_ENABLED:
yield None
return
cache = SimulationPropertyCache(max_entries=max_entries)
token = _CURRENT_PROPERTY_CACHE.set(cache)
try:
yield cache
finally:
_CURRENT_PROPERTY_CACHE.reset(token)
def cache_property_calculation(
operation: str,
) -> Callable[[Callable[_P, _R]], Callable[_P, _R]]:
"""Cache one pure property calculation with hashable arguments per run."""
def decorate(function: Callable[_P, _R]) -> Callable[_P, _R]:
if not PROPERTY_CACHE_ENABLED:
return function
@wraps(function)
def wrapper(*args: _P.args, **kwargs: _P.kwargs) -> _R:
cache = _CURRENT_PROPERTY_CACHE.get()
if cache is None:
return function(*args, **kwargs)
owner = args[0] if args else function
return cache.get_or_compute(
operation,
owner,
function,
tuple(args[1:] if args else ()),
dict(kwargs),
)
return wrapper
return decorate
def with_property_cache(function: Callable[_P, _R]) -> Callable[_P, _R]:
"""Ensure a simulation entry point has a run-local cache."""
if not PROPERTY_CACHE_ENABLED:
return function
@wraps(function)
def wrapper(*args: _P.args, **kwargs: _P.kwargs) -> _R:
with property_cache_run():
return function(*args, **kwargs)
return wrapper
__all__ = [
"DEFAULT_PROPERTY_CACHE_MAX_ENTRIES",
"PROPERTY_CACHE_ENABLED",
"PropertyCacheInfo",
"SimulationPropertyCache",
"cache_property_calculation",
"current_property_cache",
"property_cache_run",
"with_property_cache",
]
+1 -23
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@@ -1,23 +1 @@
from app.simulation.reporting.testmodel_outputs import (
COMPARISON_KEYS,
MODELICA_COMPARISON_COLUMNS,
PRIMARY_KEYS,
TestModelArtifacts,
export_testmodel_artifacts,
format_testmodel_run_report,
load_modelica_series,
write_testmodel_run_report,
write_modelica_comparison,
)
__all__ = [
"COMPARISON_KEYS",
"MODELICA_COMPARISON_COLUMNS",
"PRIMARY_KEYS",
"TestModelArtifacts",
"export_testmodel_artifacts",
"format_testmodel_run_report",
"load_modelica_series",
"write_testmodel_run_report",
"write_modelica_comparison",
]
"""Readers for external simulation results."""
-263
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@@ -1,263 +0,0 @@
from __future__ import annotations
import argparse
import json
from dataclasses import dataclass
from pathlib import Path
from typing import Mapping
from app.simulation.components.amesim.flow.pipes import AmesimPnl0002
from app.simulation.reporting.amesim_results import (
AmesimResults,
load_test_mql_amesim_results,
)
@dataclass(frozen=True, slots=True)
class Pnl0002ReplayPaths:
"""AMESim data paths needed to replay one PNL0002 resistance."""
center_pressure: str
center_temperature: str
port_1_pressure: str
port_1_temperature: str
port_1_mass_flow: str
port_2_pressure: str
port_2_temperature: str
port_2_mass_flow: str
reynolds: str
friction_factor: str
PNL83_REPLAY_PATHS = Pnl0002ReplayPaths(
center_pressure="pctr@pneumatic_83",
center_temperature="tctr@pneumatic_83",
port_1_pressure="press1@pnnode4_16",
port_1_temperature="temp1@pnnode4_16",
port_1_mass_flow="dm1@pneumatic_83",
port_2_pressure="press3@pnnode4_17",
port_2_temperature="temp3@pnnode4_17",
port_2_mass_flow="dm2@pneumatic_83",
reynolds="re@pneumatic_83",
friction_factor="ff@pneumatic_83",
)
def _required_series(
results: AmesimResults,
path: str,
) -> tuple[float, ...]:
try:
values = results.series(path)
except KeyError as exc:
raise ValueError(f"AMESim replay variable is not saved: {path}") from exc
if len(values) != len(results.times):
raise ValueError(f"AMESim replay variable has an invalid length: {path}")
return values
def _metric_summary(
rows: list[dict[str, float]],
key: str,
) -> dict[str, float]:
values = [float(row[key]) for row in rows]
max_index = max(range(len(values)), key=lambda index: abs(values[index]))
return {
"maxAbs": abs(values[max_index]),
"maxAbsTime": rows[max_index]["time"],
"finalSigned": values[-1],
}
def replay_pnl0002_amesim_states(
pipe: AmesimPnl0002,
results: AmesimResults,
paths: Pnl0002ReplayPaths,
*,
amesim_mass_flow_scale: float = -1.0e-3,
) -> dict[str, object]:
"""Replay saved AMESim states through current PNL0002 flow functions.
This is a calibration-only, no-integration calculation. It does not write
states into the pipe or alter the production simulation path.
"""
series_by_field = {
field: _required_series(results, getattr(paths, field))
for field in paths.__dataclass_fields__
}
rows: list[dict[str, float]] = []
for index, time_s in enumerate(results.times):
center_pressure = series_by_field["center_pressure"][index]
center_temperature = series_by_field["center_temperature"][index]
port_1_pressure = series_by_field["port_1_pressure"][index]
port_2_pressure = series_by_field["port_2_pressure"][index]
observed_flow_1 = (
amesim_mass_flow_scale
* series_by_field["port_1_mass_flow"][index]
)
observed_flow_2 = (
amesim_mass_flow_scale
* series_by_field["port_2_mass_flow"][index]
)
upstream_temperature_1 = (
series_by_field["port_1_temperature"][index]
if observed_flow_1 >= 0.0
else center_temperature
)
upstream_temperature_2 = (
series_by_field["port_2_temperature"][index]
if observed_flow_2 >= 0.0
else center_temperature
)
predicted_flow_1 = pipe.mass_flow(
port_1_pressure,
center_pressure,
upstream_temperature_1,
)
predicted_flow_2 = pipe.mass_flow(
port_2_pressure,
center_pressure,
upstream_temperature_2,
)
reynolds_1 = pipe.reynolds_number(
observed_flow_1,
upstream_temperature_1,
)
reynolds_2 = pipe.reynolds_number(
observed_flow_2,
upstream_temperature_2,
)
friction_1 = pipe.friction_factor(reynolds_1)
friction_2 = pipe.friction_factor(reynolds_2)
replay_reynolds = 0.5 * (reynolds_1 + reynolds_2)
replay_friction = 0.5 * (friction_1 + friction_2)
rows.append(
{
"time": float(time_s),
"centerPressure": center_pressure,
"centerTemperature": center_temperature,
"port1Pressure": port_1_pressure,
"port2Pressure": port_2_pressure,
"observedPort1MassFlow": observed_flow_1,
"observedPort2MassFlow": observed_flow_2,
"predictedPort1MassFlow": predicted_flow_1,
"predictedPort2MassFlow": predicted_flow_2,
"port1MassFlowError": predicted_flow_1 - observed_flow_1,
"port2MassFlowError": predicted_flow_2 - observed_flow_2,
"amesimReynolds": series_by_field["reynolds"][index],
"replayReynolds": replay_reynolds,
"reynoldsError": (
replay_reynolds - series_by_field["reynolds"][index]
),
"amesimFrictionFactor": series_by_field["friction_factor"][index],
"replayFrictionFactor": replay_friction,
"frictionFactorError": (
replay_friction
- series_by_field["friction_factor"][index]
),
}
)
metric_keys = (
"port1MassFlowError",
"port2MassFlowError",
"reynoldsError",
"frictionFactorError",
)
return {
"mode": "amesim-state-replay-no-integration",
"component": pipe.name,
"pointCount": len(rows),
"massFlowScale": amesim_mass_flow_scale,
"paths": {
field: getattr(paths, field)
for field in paths.__dataclass_fields__
},
"parameters": dict(pipe.parameter_values),
"summary": {
key: _metric_summary(rows, key)
for key in metric_keys
},
"rows": rows,
}
def _compile_project_pipe(
project_path: Path,
component_name: str,
) -> AmesimPnl0002:
from app.main import (
ReactFlowProjectPayload,
_compile_xml_document_or_422,
_validated_xml_document_or_422,
build_reactflow_system_xml,
validate_system_xml_document,
)
payload = ReactFlowProjectPayload.model_validate_json(
project_path.read_text(encoding="utf-8")
)
xml_bytes = build_reactflow_system_xml(payload)
document = _validated_xml_document_or_422(
validate_system_xml_document(xml_bytes)
)
_project, network = _compile_xml_document_or_422(document)
try:
component = network.components[component_name]
except KeyError as exc:
raise ValueError(f"Project component does not exist: {component_name}") from exc
if not isinstance(component, AmesimPnl0002):
raise ValueError(f"Project component is not PNL0002: {component_name}")
return component
def _paths_from_arguments(arguments: argparse.Namespace) -> Pnl0002ReplayPaths:
values: Mapping[str, str] = {
field: getattr(arguments, field)
for field in PNL83_REPLAY_PATHS.__dataclass_fields__
}
return Pnl0002ReplayPaths(**values)
def main() -> None:
parser = argparse.ArgumentParser(
description="Replay saved AMESim p/T/m_flow through a PNL0002 model without integration."
)
parser.add_argument("project", type=Path)
parser.add_argument("amesim_archive", type=Path)
parser.add_argument("output", type=Path)
parser.add_argument("--component", default="pneumatic_83")
parser.add_argument("--mass-flow-scale", type=float, default=-1.0e-3)
for field in PNL83_REPLAY_PATHS.__dataclass_fields__:
parser.add_argument(
"--" + field.replace("_", "-"),
dest=field,
default=getattr(PNL83_REPLAY_PATHS, field),
)
arguments = parser.parse_args()
pipe = _compile_project_pipe(arguments.project, arguments.component)
results = load_test_mql_amesim_results(arguments.amesim_archive)
report = replay_pnl0002_amesim_states(
pipe,
results,
_paths_from_arguments(arguments),
amesim_mass_flow_scale=arguments.mass_flow_scale,
)
arguments.output.parent.mkdir(parents=True, exist_ok=True)
arguments.output.write_text(
json.dumps(report, ensure_ascii=False, indent=2) + "\n",
encoding="utf-8",
)
print(json.dumps({key: report[key] for key in (
"mode",
"component",
"pointCount",
"parameters",
"summary",
)}, ensure_ascii=False, indent=2))
if __name__ == "__main__":
main()
@@ -1,195 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.reporting.amesim_results import AmesimResults
from app.simulation.reporting.test_mql_variables import (
TestMqlVariableBinding,
TestMqlVariableCatalog,
build_test_mql_variable_catalog,
)
from app.simulation.examples.test_mql.pneumatic import (
TestMqlPneumaticAssembly,
build_test_mql_pneumatic_assembly,
)
@dataclass(frozen=True)
class TestMqlChamberObservation:
time: float
pressure_pa: float
temperature_k: float
gas_mass_g: float
volume_cm3: float | None
@dataclass(frozen=True)
class TestMqlChamberBinding:
alias: str
submodel: str
pressure_path: str
temperature_path: str
gas_mass_path: str
pressure_duplicate_paths: tuple[str, ...]
temperature_duplicate_paths: tuple[str, ...]
volume_path: str | None
@property
def is_variable(self) -> bool:
return self.volume_path is not None
def observation_at(self, results: AmesimResults, index: int) -> TestMqlChamberObservation:
return TestMqlChamberObservation(
time=results.times[index],
pressure_pa=results.series(self.pressure_path)[index],
temperature_k=results.series(self.temperature_path)[index],
gas_mass_g=results.series(self.gas_mass_path)[index],
volume_cm3=(
results.series(self.volume_path)[index]
if self.volume_path is not None
else None
),
)
@dataclass(frozen=True)
class TestMqlChamberObservationCatalog:
bindings: tuple[TestMqlChamberBinding, ...]
@property
def fixed_count(self) -> int:
return sum(1 for binding in self.bindings if binding.submodel == "PNCH023")
@property
def variable_count(self) -> int:
return sum(1 for binding in self.bindings if binding.submodel == "PNCH012")
def by_alias(self, alias: str) -> TestMqlChamberBinding:
for binding in self.bindings:
if binding.alias == alias:
return binding
raise KeyError(alias)
def build_test_mql_chamber_observation_catalog(
results: AmesimResults,
*,
variable_catalog: TestMqlVariableCatalog | None = None,
assembly: TestMqlPneumaticAssembly | None = None,
) -> TestMqlChamberObservationCatalog:
variable_catalog = variable_catalog or build_test_mql_variable_catalog(results)
assembly = assembly or build_test_mql_pneumatic_assembly()
chamber_aliases = {
**{alias: "PNCH023" for alias in assembly.fixed_chambers},
**{alias: "PNCH012" for alias in assembly.variable_chambers},
}
bindings = []
for alias, submodel in chamber_aliases.items():
variables = tuple(
variable
for variable in variable_catalog.variables
if variable.owner_alias == alias
)
pressure = _primary_observable(variables, "press", expected_units="Pa")
temperature = _primary_observable(variables, "temp", expected_units="K")
gas_mass = _required_path(
variables,
"mgas1" if submodel == "PNCH012" else "mgas",
expected_units="g",
)
volume = _optional_path(variables, "vol", expected_units="cm**3")
bindings.append(
TestMqlChamberBinding(
alias=alias,
submodel=submodel,
pressure_path=pressure.data_path,
temperature_path=temperature.data_path,
gas_mass_path=gas_mass,
pressure_duplicate_paths=_duplicate_paths(variables, "press", expected_units="Pa"),
temperature_duplicate_paths=_duplicate_paths(variables, "temp", expected_units="K"),
volume_path=volume,
)
)
return TestMqlChamberObservationCatalog(
bindings=tuple(sorted(bindings, key=lambda binding: binding.alias))
)
def _primary_observable(
variables: tuple[TestMqlVariableBinding, ...],
signal_prefix: str,
*,
expected_units: str,
) -> TestMqlVariableBinding:
matches = tuple(
variable
for variable in variables
if variable.signal_name == signal_prefix
and "duplicate" not in variable.label
)
variable = _single(matches, f"primary {signal_prefix}")
_assert_units(variable, expected_units)
return variable
def _duplicate_paths(
variables: tuple[TestMqlVariableBinding, ...],
signal_prefix: str,
*,
expected_units: str,
) -> tuple[str, ...]:
matches = tuple(
variable
for variable in variables
if variable.signal_name.startswith(signal_prefix)
and variable.signal_name != signal_prefix
and "duplicate" in variable.label
)
for variable in matches:
_assert_units(variable, expected_units)
return tuple(variable.data_path for variable in matches)
def _required_path(
variables: tuple[TestMqlVariableBinding, ...],
signal_name: str,
*,
expected_units: str,
) -> str:
variable = _single(
tuple(variable for variable in variables if variable.signal_name == signal_name),
signal_name,
)
_assert_units(variable, expected_units)
return variable.data_path
def _optional_path(
variables: tuple[TestMqlVariableBinding, ...],
signal_name: str,
*,
expected_units: str,
) -> str | None:
matches = tuple(variable for variable in variables if variable.signal_name == signal_name)
if not matches:
return None
variable = _single(matches, signal_name)
_assert_units(variable, expected_units)
return variable.data_path
def _single(
matches: tuple[TestMqlVariableBinding, ...],
description: str,
) -> TestMqlVariableBinding:
if len(matches) != 1:
raise ValueError(f"Expected one {description} variable, found {len(matches)}.")
return matches[0]
def _assert_units(variable: TestMqlVariableBinding, expected_units: str) -> None:
if variable.units != expected_units:
raise ValueError(
f"Unexpected units for {variable.data_path}: "
f"{variable.units!r}, expected {expected_units!r}."
)
@@ -1,274 +0,0 @@
from __future__ import annotations
from bisect import bisect_left
import csv
from dataclasses import dataclass
from pathlib import Path
from app.simulation.reporting.amesim_results import AmesimResults
DEFAULT_TEST_MQL_ALIGNMENT_PATHS = (
"temp3@pn_c1_8",
"press3@pn_c1_8",
"vvol1@pn_brp2_8",
"vol1@pn_brp2_8",
)
@dataclass(frozen=True)
class TestMqlComparisonMetric:
data_path: str
sample_count: int
max_abs_error: float
mean_abs_error: float
max_rel_error: float
undefined_rel_error_count: int
near_zero_baseline_count: int
final_abs_error: float
@dataclass(frozen=True)
class TestMqlComparisonResult:
metrics: tuple[TestMqlComparisonMetric, ...]
def metric(self, data_path: str) -> TestMqlComparisonMetric:
for metric in self.metrics:
if metric.data_path == data_path:
return metric
raise KeyError(data_path)
@property
def max_abs_error(self) -> float:
return max((metric.max_abs_error for metric in self.metrics), default=0.0)
@property
def max_rel_error(self) -> float:
return max((metric.max_rel_error for metric in self.metrics), default=0.0)
@property
def undefined_rel_error_count(self) -> int:
return sum(metric.undefined_rel_error_count for metric in self.metrics)
class TestMqlComparisonError(ValueError):
"""Raised when Python and AMESim series cannot be aligned."""
def compare_test_mql_series(
*,
python_times: tuple[float, ...] | list[float],
python_series_by_data_path: dict[str, tuple[float, ...] | list[float]],
amesim_results: AmesimResults,
data_paths: tuple[str, ...] | list[str] | None = None,
relative_floor: float = 1.0e-12,
) -> TestMqlComparisonResult:
"""Compare current values directly with AMESim simulation values.
``relative_floor`` only identifies near-zero baselines for reporting. It is
never substituted into the relative-error denominator. An exact zero
AMESim baseline has undefined relative error and is counted separately;
absolute error remains available for judgement.
"""
if relative_floor < 0.0:
raise TestMqlComparisonError("relative_floor cannot be negative.")
_validate_time_axis(python_times)
selected_paths = _select_data_paths(python_series_by_data_path, amesim_results, data_paths)
metrics = []
for data_path in selected_paths:
python_values = tuple(float(value) for value in python_series_by_data_path[data_path])
if len(python_values) != len(python_times):
raise TestMqlComparisonError(
f"Python series length mismatch for {data_path!r}: "
f"{len(python_values)} values for {len(python_times)} time samples."
)
amesim_values = amesim_results.series(data_path)
abs_errors = []
rel_errors = []
undefined_rel_error_count = 0
near_zero_baseline_count = 0
for time_value, python_value in zip(python_times, python_values):
amesim_value = interpolate_series_value(amesim_results.times, amesim_values, time_value)
abs_error = abs(python_value - amesim_value)
abs_errors.append(abs_error)
if abs(amesim_value) <= relative_floor:
near_zero_baseline_count += 1
if amesim_value == 0.0:
undefined_rel_error_count += 1
else:
rel_errors.append(abs_error / abs(amesim_value))
final_amesim_value = interpolate_series_value(
amesim_results.times,
amesim_values,
float(python_times[-1]),
)
metrics.append(
TestMqlComparisonMetric(
data_path=data_path,
sample_count=len(python_times),
max_abs_error=max(abs_errors, default=0.0),
mean_abs_error=sum(abs_errors) / max(len(abs_errors), 1),
max_rel_error=max(rel_errors, default=0.0),
undefined_rel_error_count=undefined_rel_error_count,
near_zero_baseline_count=near_zero_baseline_count,
final_abs_error=abs(python_values[-1] - final_amesim_value),
)
)
return TestMqlComparisonResult(metrics=tuple(metrics))
def write_test_mql_amesim_baseline_csv(
output_dir: Path,
amesim_results: AmesimResults,
data_paths: tuple[str, ...] | list[str] = DEFAULT_TEST_MQL_ALIGNMENT_PATHS,
) -> Path:
output_dir.mkdir(parents=True, exist_ok=True)
csv_path = output_dir / "test_mql_amesim_baseline.csv"
_validate_amesim_data_paths(amesim_results, data_paths)
with csv_path.open("w", newline="", encoding="utf-8") as handle:
writer = csv.writer(handle)
writer.writerow(["time_s", *data_paths])
for index, time_value in enumerate(amesim_results.times):
writer.writerow(
[time_value, *(amesim_results.series(data_path)[index] for data_path in data_paths)]
)
return csv_path
def write_test_mql_comparison_csv(
*,
output_dir: Path,
python_times: tuple[float, ...] | list[float],
python_series_by_data_path: dict[str, tuple[float, ...] | list[float]],
amesim_results: AmesimResults,
data_paths: tuple[str, ...] | list[str] | None = None,
) -> tuple[Path, Path, TestMqlComparisonResult]:
output_dir.mkdir(parents=True, exist_ok=True)
selected_paths = _select_data_paths(python_series_by_data_path, amesim_results, data_paths)
comparison = compare_test_mql_series(
python_times=python_times,
python_series_by_data_path=python_series_by_data_path,
amesim_results=amesim_results,
data_paths=selected_paths,
)
csv_path = output_dir / "test_mql_amesim_comparison.csv"
summary_path = output_dir / "test_mql_amesim_comparison_summary.txt"
with csv_path.open("w", newline="", encoding="utf-8") as handle:
writer = csv.writer(handle)
header = ["time_s"]
for data_path in selected_paths:
header.extend(
[
f"python.{data_path}",
f"amesim.{data_path}",
f"abs_error.{data_path}",
f"rel_error.{data_path}",
]
)
writer.writerow(header)
for index, time_value in enumerate(python_times):
row = [time_value]
for data_path in selected_paths:
python_value = float(python_series_by_data_path[data_path][index])
amesim_value = interpolate_series_value(
amesim_results.times,
amesim_results.series(data_path),
float(time_value),
)
abs_error = abs(python_value - amesim_value)
rel_error = (
None
if amesim_value == 0.0
else abs_error / abs(amesim_value)
)
row.extend(
[
python_value,
amesim_value,
abs_error,
"" if rel_error is None else rel_error,
]
)
writer.writerow(row)
summary_lines = [
(
f"{metric.data_path}: samples={metric.sample_count}, "
f"max_abs_error={metric.max_abs_error:.12g}, "
f"mean_abs_error={metric.mean_abs_error:.12g}, "
f"max_rel_error={metric.max_rel_error:.12%}, "
f"undefined_rel_error_count={metric.undefined_rel_error_count}, "
f"final_abs_error={metric.final_abs_error:.12g}"
)
for metric in comparison.metrics
]
summary_path.write_text("\n".join(summary_lines) + "\n", encoding="utf-8")
return csv_path, summary_path, comparison
def interpolate_series_value(
time_values: tuple[float, ...] | list[float],
values: tuple[float, ...] | list[float],
target_time: float,
) -> float:
if len(time_values) != len(values):
raise TestMqlComparisonError("time and value series lengths differ.")
if not time_values:
raise TestMqlComparisonError("cannot interpolate an empty series.")
if target_time <= time_values[0]:
return float(values[0])
if target_time >= time_values[-1]:
return float(values[-1])
right_index = bisect_left(time_values, target_time)
if right_index < len(time_values) and abs(time_values[right_index] - target_time) <= 1.0e-12:
return float(values[right_index])
left_index = right_index - 1
left_time = float(time_values[left_index])
right_time = float(time_values[right_index])
fraction = (target_time - left_time) / (right_time - left_time)
return float(values[left_index]) + fraction * (float(values[right_index]) - float(values[left_index]))
def _select_data_paths(
python_series_by_data_path: dict[str, tuple[float, ...] | list[float]],
amesim_results: AmesimResults,
data_paths: tuple[str, ...] | list[str] | None,
) -> tuple[str, ...]:
if data_paths is None:
data_paths = tuple(
data_path
for data_path in python_series_by_data_path
if data_path in amesim_results.series_by_data_path
)
selected_paths = tuple(data_paths)
if not selected_paths:
raise TestMqlComparisonError("no common Data_Path values are available for comparison.")
missing_python = [data_path for data_path in selected_paths if data_path not in python_series_by_data_path]
if missing_python:
raise TestMqlComparisonError(f"Python series missing Data_Path values: {missing_python}")
_validate_amesim_data_paths(amesim_results, selected_paths)
return selected_paths
def _validate_amesim_data_paths(
amesim_results: AmesimResults,
data_paths: tuple[str, ...] | list[str],
) -> None:
missing_amesim = [data_path for data_path in data_paths if data_path not in amesim_results.series_by_data_path]
if missing_amesim:
raise TestMqlComparisonError(f"AMESim results missing Data_Path values: {missing_amesim}")
def _validate_time_axis(time_values: tuple[float, ...] | list[float]) -> None:
if not time_values:
raise TestMqlComparisonError("Python time axis is empty.")
previous = float(time_values[0])
for value in time_values[1:]:
value = float(value)
if value < previous:
raise TestMqlComparisonError("Python time axis must be monotonically increasing.")
previous = value
@@ -1,211 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.reporting.amesim_results import AmesimResults
from app.simulation.reporting.test_mql_variables import (
TestMqlVariableBinding,
TestMqlVariableCatalog,
build_test_mql_variable_catalog,
)
from app.simulation.examples.test_mql.lines import (
TestMqlLineAssembly,
build_test_mql_line_assembly,
)
G_PER_S_TO_KG_PER_S = 1.0e-3
@dataclass(frozen=True)
class TestMqlLineObservation:
time: float
mass_flows_kg_s: dict[str, float]
enthalpy_flows_w: dict[str, float]
pressures_pa: dict[str, float]
temperatures_k: dict[str, float]
gas_mass_g: float | None
reynolds_number: float
mass_flow_parameter: float
gas_velocity_m_s: float
friction_factor: float
@dataclass(frozen=True)
class TestMqlLineObservationBinding:
alias: str
submodel: str
pattern: str
mass_flow_paths: tuple[str, ...]
enthalpy_flow_paths: tuple[str, ...]
pressure_paths: tuple[str, ...]
temperature_paths: tuple[str, ...]
gas_mass_path: str | None
reynolds_path: str
mass_flow_parameter_path: str
gas_velocity_path: str
friction_factor_path: str
def mass_flow_kg_s_series(
self,
results: AmesimResults,
data_path: str | None = None,
) -> tuple[float, ...]:
path = data_path or self.mass_flow_paths[0]
if path not in self.mass_flow_paths:
raise KeyError(path)
return tuple(value * G_PER_S_TO_KG_PER_S for value in results.series(path))
def observation_at(self, results: AmesimResults, index: int) -> TestMqlLineObservation:
return TestMqlLineObservation(
time=results.times[index],
mass_flows_kg_s={
path: results.series(path)[index] * G_PER_S_TO_KG_PER_S
for path in self.mass_flow_paths
},
enthalpy_flows_w={
path: results.series(path)[index]
for path in self.enthalpy_flow_paths
},
pressures_pa={
path: results.series(path)[index]
for path in self.pressure_paths
},
temperatures_k={
path: results.series(path)[index]
for path in self.temperature_paths
},
gas_mass_g=(
results.series(self.gas_mass_path)[index]
if self.gas_mass_path is not None
else None
),
reynolds_number=results.series(self.reynolds_path)[index],
mass_flow_parameter=results.series(self.mass_flow_parameter_path)[index],
gas_velocity_m_s=results.series(self.gas_velocity_path)[index],
friction_factor=results.series(self.friction_factor_path)[index],
)
@dataclass(frozen=True)
class TestMqlLineObservationCatalog:
bindings: tuple[TestMqlLineObservationBinding, ...]
@property
def line_count(self) -> int:
return len(self.bindings)
def by_alias(self, alias: str) -> TestMqlLineObservationBinding:
for binding in self.bindings:
if binding.alias == alias:
return binding
raise KeyError(alias)
def by_submodel(self, submodel: str) -> tuple[TestMqlLineObservationBinding, ...]:
return tuple(binding for binding in self.bindings if binding.submodel == submodel)
def build_test_mql_line_observation_catalog(
results: AmesimResults,
*,
variable_catalog: TestMqlVariableCatalog | None = None,
line_assembly: TestMqlLineAssembly | None = None,
) -> TestMqlLineObservationCatalog:
variable_catalog = variable_catalog or build_test_mql_variable_catalog(results)
line_assembly = line_assembly or build_test_mql_line_assembly(results, variable_catalog)
bindings = []
for line in line_assembly.lines:
variables = tuple(
variable
for variable in variable_catalog.variables
if variable.owner_alias == line.alias
)
bindings.append(
TestMqlLineObservationBinding(
alias=line.alias,
submodel=line.submodel,
pattern=line.pattern,
mass_flow_paths=_paths_with_prefix(variables, "dm", expected_units="g/s"),
enthalpy_flow_paths=_paths_with_prefix(variables, "dh", expected_units="J/s"),
pressure_paths=_paths_with_prefix(variables, "p", expected_units="Pa"),
temperature_paths=_paths_with_prefix(variables, "t", expected_units="K"),
gas_mass_path=_optional_path(variables, "mgas", expected_units="g"),
reynolds_path=_required_path(variables, "re", expected_units=None),
mass_flow_parameter_path=_required_path(
variables,
"cm",
expected_units="(kg*K/J)**(1/2)",
),
gas_velocity_path=_required_path(variables, "v", expected_units="m/s"),
friction_factor_path=_required_path(variables, "ff", expected_units=None),
)
)
return TestMqlLineObservationCatalog(bindings=tuple(bindings))
def _paths_with_prefix(
variables: tuple[TestMqlVariableBinding, ...],
prefix: str,
*,
expected_units: str | None,
) -> tuple[str, ...]:
matches = tuple(
variable
for variable in variables
if variable.signal_name.startswith(prefix)
)
for variable in matches:
_assert_units(variable, expected_units)
return tuple(variable.data_path for variable in matches)
def _required_path(
variables: tuple[TestMqlVariableBinding, ...],
signal_name: str,
*,
expected_units: str | None,
) -> str:
variable = _single_signal(variables, signal_name)
_assert_units(variable, expected_units)
return variable.data_path
def _optional_path(
variables: tuple[TestMqlVariableBinding, ...],
signal_name: str,
*,
expected_units: str | None,
) -> str | None:
matches = tuple(variable for variable in variables if variable.signal_name == signal_name)
if not matches:
return None
variable = _single(matches, signal_name)
_assert_units(variable, expected_units)
return variable.data_path
def _single_signal(
variables: tuple[TestMqlVariableBinding, ...],
signal_name: str,
) -> TestMqlVariableBinding:
return _single(
tuple(variable for variable in variables if variable.signal_name == signal_name),
signal_name,
)
def _single(
matches: tuple[TestMqlVariableBinding, ...],
description: str,
) -> TestMqlVariableBinding:
if len(matches) != 1:
raise ValueError(f"Expected one {description} variable, found {len(matches)}.")
return matches[0]
def _assert_units(variable: TestMqlVariableBinding, expected_units: str | None) -> None:
if variable.units != expected_units:
raise ValueError(
f"Unexpected units for {variable.data_path}: "
f"{variable.units!r}, expected {expected_units!r}."
)
@@ -1,395 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.reporting.amesim_results import AmesimResults
from app.simulation.reporting.test_mql_variables import (
TestMqlVariableBinding,
TestMqlVariableCatalog,
build_test_mql_variable_catalog,
)
from app.simulation.examples.test_mql.mechanical import (
TestMqlMechanicalAssembly,
build_test_mql_mechanical_assembly,
)
@dataclass(frozen=True)
class TestMqlPistonObservation:
time: float
chamber_volume_cm3: float
chamber_volume_rate_l_min: float
chamber_length_mm: float
force_port_2_n: float
force_port_3_n: float
displacement_port_2_m: float
velocity_port_2_m_s: float
displacement_port_3_m: float
velocity_port_3_m_s: float
@dataclass(frozen=True)
class TestMqlMassEndstopObservation:
time: float
displacement_m: float
velocity_m_s: float
acceleration_m_s2: float
lower_contact_force_n: float
upper_contact_force_n: float
viscous_friction_force_n: float
dry_friction_force_n: float
stick_flag: float
@dataclass(frozen=True)
class TestMqlElasticEndstopObservation:
time: float
force_n: float
duplicate_force_n: float
gap_mm: float
stiffness_n_m: float
@dataclass(frozen=True)
class TestMqlForceSourceObservation:
time: float
force_n: float
@dataclass(frozen=True)
class TestMqlForceConnectorObservation:
time: float
force_n: float
@dataclass(frozen=True)
class TestMqlMechanicalNodeObservation:
time: float
velocities_m_s: dict[int, float]
displacements_m: dict[int, float]
total_force_n: float
@dataclass(frozen=True)
class TestMqlPistonObservationBinding:
alias: str
volume_path: str
volume_rate_path: str
length_path: str
force_port_2_path: str
force_port_3_path: str
displacement_port_2_path: str
velocity_port_2_path: str
displacement_port_3_path: str
velocity_port_3_path: str
def observation_at(self, results: AmesimResults, index: int) -> TestMqlPistonObservation:
return TestMqlPistonObservation(
time=results.times[index],
chamber_volume_cm3=results.series(self.volume_path)[index],
chamber_volume_rate_l_min=results.series(self.volume_rate_path)[index],
chamber_length_mm=results.series(self.length_path)[index],
force_port_2_n=results.series(self.force_port_2_path)[index],
force_port_3_n=results.series(self.force_port_3_path)[index],
displacement_port_2_m=results.series(self.displacement_port_2_path)[index],
velocity_port_2_m_s=results.series(self.velocity_port_2_path)[index],
displacement_port_3_m=results.series(self.displacement_port_3_path)[index],
velocity_port_3_m_s=results.series(self.velocity_port_3_path)[index],
)
@dataclass(frozen=True)
class TestMqlMassEndstopObservationBinding:
alias: str
displacement_path: str
velocity_path: str
acceleration_path: str
displacement_duplicate_path: str
velocity_duplicate_path: str
acceleration_duplicate_path: str
lower_contact_force_path: str
upper_contact_force_path: str
viscous_friction_force_path: str
dry_friction_force_path: str
stick_flag_path: str
def observation_at(self, results: AmesimResults, index: int) -> TestMqlMassEndstopObservation:
return TestMqlMassEndstopObservation(
time=results.times[index],
displacement_m=results.series(self.displacement_path)[index],
velocity_m_s=results.series(self.velocity_path)[index],
acceleration_m_s2=results.series(self.acceleration_path)[index],
lower_contact_force_n=results.series(self.lower_contact_force_path)[index],
upper_contact_force_n=results.series(self.upper_contact_force_path)[index],
viscous_friction_force_n=results.series(self.viscous_friction_force_path)[index],
dry_friction_force_n=results.series(self.dry_friction_force_path)[index],
stick_flag=results.series(self.stick_flag_path)[index],
)
@dataclass(frozen=True)
class TestMqlElasticEndstopObservationBinding:
alias: str
force_path: str
duplicate_force_path: str
gap_path: str
stiffness_path: str
def observation_at(self, results: AmesimResults, index: int) -> TestMqlElasticEndstopObservation:
return TestMqlElasticEndstopObservation(
time=results.times[index],
force_n=results.series(self.force_path)[index],
duplicate_force_n=results.series(self.duplicate_force_path)[index],
gap_mm=results.series(self.gap_path)[index],
stiffness_n_m=results.series(self.stiffness_path)[index],
)
@dataclass(frozen=True)
class TestMqlForceSourceObservationBinding:
alias: str
force_path: str
def observation_at(self, results: AmesimResults, index: int) -> TestMqlForceSourceObservation:
return TestMqlForceSourceObservation(
time=results.times[index],
force_n=results.series(self.force_path)[index],
)
@dataclass(frozen=True)
class TestMqlForceConnectorObservationBinding:
alias: str
force_path: str
def observation_at(self, results: AmesimResults, index: int) -> TestMqlForceConnectorObservation:
return TestMqlForceConnectorObservation(
time=results.times[index],
force_n=results.series(self.force_path)[index],
)
@dataclass(frozen=True)
class TestMqlMechanicalNodeObservationBinding:
alias: str
velocity_paths_by_port: dict[int, str]
displacement_paths_by_port: dict[int, str]
total_force_path: str
def observation_at(self, results: AmesimResults, index: int) -> TestMqlMechanicalNodeObservation:
return TestMqlMechanicalNodeObservation(
time=results.times[index],
velocities_m_s={
port: results.series(path)[index]
for port, path in self.velocity_paths_by_port.items()
},
displacements_m={
port: results.series(path)[index]
for port, path in self.displacement_paths_by_port.items()
},
total_force_n=results.series(self.total_force_path)[index],
)
@dataclass(frozen=True)
class TestMqlMechanicalObservationCatalog:
pistons: dict[str, TestMqlPistonObservationBinding]
masses: dict[str, TestMqlMassEndstopObservationBinding]
elastic_endstops: dict[str, TestMqlElasticEndstopObservationBinding]
zero_force_sources: dict[str, TestMqlForceSourceObservationBinding]
force_connectors: dict[str, TestMqlForceConnectorObservationBinding]
mechanical_nodes: dict[str, TestMqlMechanicalNodeObservationBinding]
@property
def binding_count(self) -> int:
return (
len(self.pistons)
+ len(self.masses)
+ len(self.elastic_endstops)
+ len(self.zero_force_sources)
+ len(self.force_connectors)
+ len(self.mechanical_nodes)
)
def build_test_mql_mechanical_observation_catalog(
results: AmesimResults,
*,
variable_catalog: TestMqlVariableCatalog | None = None,
mechanical_assembly: TestMqlMechanicalAssembly | None = None,
) -> TestMqlMechanicalObservationCatalog:
variable_catalog = variable_catalog or build_test_mql_variable_catalog(results)
mechanical_assembly = mechanical_assembly or build_test_mql_mechanical_assembly(
amesim_results=results,
variable_catalog=variable_catalog,
)
return TestMqlMechanicalObservationCatalog(
pistons={
alias: _build_piston_binding(alias, variable_catalog)
for alias in mechanical_assembly.pistons
},
masses={
alias: _build_mass_binding(alias, variable_catalog)
for alias in mechanical_assembly.masses
},
elastic_endstops={
alias: _build_elastic_endstop_binding(alias, variable_catalog)
for alias in mechanical_assembly.elastic_endstops
},
zero_force_sources={
alias: _build_zero_force_source_binding(alias, variable_catalog)
for alias in mechanical_assembly.zero_force_sources
},
force_connectors={
alias: _build_force_connector_binding(alias, variable_catalog)
for alias in mechanical_assembly.force_connectors
},
mechanical_nodes={
alias: _build_mechanical_node_binding(alias, variable_catalog)
for alias in mechanical_assembly.mechanical_nodes
},
)
def _build_piston_binding(
alias: str,
variable_catalog: TestMqlVariableCatalog,
) -> TestMqlPistonObservationBinding:
variables = _owner_variables(variable_catalog, alias)
return TestMqlPistonObservationBinding(
alias=alias,
volume_path=_required_path(variables, "vol1", expected_units="cm**3"),
volume_rate_path=_required_path(variables, "vvol1", expected_units="L/min"),
length_path=_required_path(variables, "length", expected_units="mm"),
force_port_2_path=_required_path(variables, "f2", expected_units="N"),
force_port_3_path=_required_path(variables, "f3", expected_units="N"),
displacement_port_2_path=_required_path(variables, "x5", expected_units="m"),
velocity_port_2_path=_required_path(variables, "v5", expected_units="m/s"),
displacement_port_3_path=_required_path(variables, "x4", expected_units="m"),
velocity_port_3_path=_required_path(variables, "v4", expected_units="m/s"),
)
def _build_mass_binding(
alias: str,
variable_catalog: TestMqlVariableCatalog,
) -> TestMqlMassEndstopObservationBinding:
variables = _owner_variables(variable_catalog, alias)
return TestMqlMassEndstopObservationBinding(
alias=alias,
displacement_path=_required_path(variables, "x1", expected_units="m"),
velocity_path=_required_path(variables, "v1", expected_units="m/s"),
acceleration_path=_required_path(variables, "acc1", expected_units="m/s/s"),
displacement_duplicate_path=_required_path(variables, "x1dup", expected_units="m"),
velocity_duplicate_path=_required_path(variables, "v1dup", expected_units="m/s"),
acceleration_duplicate_path=_required_path(variables, "acc1dup", expected_units="m/s/s"),
lower_contact_force_path=_required_path(variables, "Fmin", expected_units="N"),
upper_contact_force_path=_required_path(variables, "Fmax", expected_units="N"),
viscous_friction_force_path=_required_path(variables, "Fvisc", expected_units="N"),
dry_friction_force_path=_required_path(variables, "Ffric", expected_units="N"),
stick_flag_path=_required_path(variables, "stick", expected_units=None),
)
def _build_elastic_endstop_binding(
alias: str,
variable_catalog: TestMqlVariableCatalog,
) -> TestMqlElasticEndstopObservationBinding:
variables = _owner_variables(variable_catalog, alias)
return TestMqlElasticEndstopObservationBinding(
alias=alias,
force_path=_required_path(variables, "f1", expected_units="N"),
duplicate_force_path=_required_path(variables, "f2", expected_units="N"),
gap_path=_required_path(variables, "gap", expected_units="mm"),
stiffness_path=_required_path(variables, "kval", expected_units="N/m"),
)
def _build_zero_force_source_binding(
alias: str,
variable_catalog: TestMqlVariableCatalog,
) -> TestMqlForceSourceObservationBinding:
variables = _owner_variables(variable_catalog, alias)
return TestMqlForceSourceObservationBinding(
alias=alias,
force_path=_required_path(variables, "fzero", expected_units="N"),
)
def _build_force_connector_binding(
alias: str,
variable_catalog: TestMqlVariableCatalog,
) -> TestMqlForceConnectorObservationBinding:
variables = _owner_variables(variable_catalog, alias)
return TestMqlForceConnectorObservationBinding(
alias=alias,
force_path=_required_path(variables, "force", expected_units="N"),
)
def _build_mechanical_node_binding(
alias: str,
variable_catalog: TestMqlVariableCatalog,
) -> TestMqlMechanicalNodeObservationBinding:
variables = _owner_variables(variable_catalog, alias)
velocity_paths_by_port = {}
displacement_paths_by_port = {}
for port in range(1, 9):
velocity_paths_by_port[port] = _required_path(
variables,
f"p{port}__vt",
expected_units="m/s",
)
displacement_paths_by_port[port] = _required_path(
variables,
f"p{port}__xt",
expected_units="m",
)
return TestMqlMechanicalNodeObservationBinding(
alias=alias,
velocity_paths_by_port=velocity_paths_by_port,
displacement_paths_by_port=displacement_paths_by_port,
total_force_path=_required_path(variables, "tforce", expected_units="N"),
)
def _owner_variables(
variable_catalog: TestMqlVariableCatalog,
alias: str,
) -> tuple[TestMqlVariableBinding, ...]:
return tuple(
variable
for variable in variable_catalog.variables
if variable.owner_alias == alias
)
def _required_path(
variables: tuple[TestMqlVariableBinding, ...],
signal_name: str,
*,
expected_units: str | None,
) -> str:
variable = _single(
tuple(variable for variable in variables if variable.signal_name == signal_name),
signal_name,
)
_assert_units(variable, expected_units)
return variable.data_path
def _single(
matches: tuple[TestMqlVariableBinding, ...],
description: str,
) -> TestMqlVariableBinding:
if len(matches) != 1:
raise ValueError(f"Expected one {description} variable, found {len(matches)}.")
return matches[0]
def _assert_units(variable: TestMqlVariableBinding, expected_units: str | None) -> None:
if variable.units != expected_units:
raise ValueError(
f"Unexpected units for {variable.data_path}: "
f"{variable.units!r}, expected {expected_units!r}."
)
@@ -1,210 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.reporting.amesim_results import AmesimResults
from app.simulation.reporting.test_mql_chamber_observations import (
TestMqlChamberObservationCatalog,
build_test_mql_chamber_observation_catalog,
)
from app.simulation.reporting.test_mql_line_observations import (
TestMqlLineObservationCatalog,
build_test_mql_line_observation_catalog,
)
from app.simulation.reporting.test_mql_mechanical_observations import (
TestMqlMechanicalObservationCatalog,
build_test_mql_mechanical_observation_catalog,
)
from app.simulation.reporting.test_mql_orifice_observations import (
TestMqlOrificeObservationCatalog,
build_test_mql_orifice_observation_catalog,
)
from app.simulation.reporting.test_mql_variables import (
TestMqlVariableCatalog,
build_test_mql_variable_catalog,
)
@dataclass(frozen=True)
class TestMqlObservationCatalog:
variable_catalog: TestMqlVariableCatalog
chambers: TestMqlChamberObservationCatalog
orifices: TestMqlOrificeObservationCatalog
lines: TestMqlLineObservationCatalog
mechanical: TestMqlMechanicalObservationCatalog
@property
def binding_count(self) -> int:
return (
len(self.chambers.bindings)
+ len(self.orifices.bindings)
+ self.lines.line_count
+ self.mechanical.binding_count
)
def data_paths_by_domain(self) -> dict[str, tuple[str, ...]]:
return {
"chambers": _sorted_unique(_chamber_data_paths(self.chambers)),
"orifices": _sorted_unique(_orifice_data_paths(self.orifices)),
"lines": _sorted_unique(_line_data_paths(self.lines)),
"mechanical": _sorted_unique(_mechanical_data_paths(self.mechanical)),
}
def data_paths(self) -> tuple[str, ...]:
paths = []
for domain_paths in self.data_paths_by_domain().values():
paths.extend(domain_paths)
return _sorted_unique(paths)
def baseline_series_by_data_path(
self,
results: AmesimResults,
data_paths: tuple[str, ...] | list[str] | None = None,
) -> dict[str, tuple[float, ...]]:
selected_paths = tuple(data_paths) if data_paths is not None else self.data_paths()
_validate_observed_paths(self, selected_paths)
return {data_path: results.series(data_path) for data_path in selected_paths}
def build_test_mql_observation_catalog(results: AmesimResults) -> TestMqlObservationCatalog:
variable_catalog = build_test_mql_variable_catalog(results)
return TestMqlObservationCatalog(
variable_catalog=variable_catalog,
chambers=build_test_mql_chamber_observation_catalog(
results,
variable_catalog=variable_catalog,
),
orifices=build_test_mql_orifice_observation_catalog(
results,
variable_catalog=variable_catalog,
),
lines=build_test_mql_line_observation_catalog(
results,
variable_catalog=variable_catalog,
),
mechanical=build_test_mql_mechanical_observation_catalog(
results,
variable_catalog=variable_catalog,
),
)
def _chamber_data_paths(catalog: TestMqlChamberObservationCatalog) -> tuple[str, ...]:
paths = []
for binding in catalog.bindings:
paths.extend(
[
binding.pressure_path,
binding.temperature_path,
binding.gas_mass_path,
*binding.pressure_duplicate_paths,
*binding.temperature_duplicate_paths,
]
)
if binding.volume_path is not None:
paths.append(binding.volume_path)
return tuple(paths)
def _orifice_data_paths(catalog: TestMqlOrificeObservationCatalog) -> tuple[str, ...]:
paths = []
for binding in catalog.bindings:
paths.extend(
[
binding.primary_mass_flow_path,
binding.primary_enthalpy_flow_path,
binding.reversed_mass_flow_path,
binding.reversed_enthalpy_flow_path,
binding.mass_flow_parameter_path,
binding.gas_velocity_path,
]
)
if binding.opening_path is not None:
paths.append(binding.opening_path)
return tuple(paths)
def _line_data_paths(catalog: TestMqlLineObservationCatalog) -> tuple[str, ...]:
paths = []
for binding in catalog.bindings:
paths.extend(binding.mass_flow_paths)
paths.extend(binding.enthalpy_flow_paths)
paths.extend(binding.pressure_paths)
paths.extend(binding.temperature_paths)
if binding.gas_mass_path is not None:
paths.append(binding.gas_mass_path)
paths.extend(
[
binding.reynolds_path,
binding.mass_flow_parameter_path,
binding.gas_velocity_path,
binding.friction_factor_path,
]
)
return tuple(paths)
def _mechanical_data_paths(catalog: TestMqlMechanicalObservationCatalog) -> tuple[str, ...]:
paths = []
for binding in catalog.pistons.values():
paths.extend(
[
binding.volume_path,
binding.volume_rate_path,
binding.length_path,
binding.force_port_2_path,
binding.force_port_3_path,
binding.displacement_port_2_path,
binding.velocity_port_2_path,
binding.displacement_port_3_path,
binding.velocity_port_3_path,
]
)
for binding in catalog.masses.values():
paths.extend(
[
binding.displacement_path,
binding.velocity_path,
binding.acceleration_path,
binding.displacement_duplicate_path,
binding.velocity_duplicate_path,
binding.acceleration_duplicate_path,
binding.lower_contact_force_path,
binding.upper_contact_force_path,
binding.viscous_friction_force_path,
binding.dry_friction_force_path,
binding.stick_flag_path,
]
)
for binding in catalog.elastic_endstops.values():
paths.extend(
[
binding.force_path,
binding.duplicate_force_path,
binding.gap_path,
binding.stiffness_path,
]
)
for binding in catalog.zero_force_sources.values():
paths.append(binding.force_path)
for binding in catalog.force_connectors.values():
paths.append(binding.force_path)
for binding in catalog.mechanical_nodes.values():
paths.extend(binding.velocity_paths_by_port.values())
paths.extend(binding.displacement_paths_by_port.values())
paths.append(binding.total_force_path)
return tuple(paths)
def _validate_observed_paths(
catalog: TestMqlObservationCatalog,
data_paths: tuple[str, ...],
) -> None:
observed_paths = set(catalog.data_paths())
missing = [data_path for data_path in data_paths if data_path not in observed_paths]
if missing:
raise KeyError(f"Data_Path values are not in the test_mql observation catalog: {missing}")
def _sorted_unique(data_paths: tuple[str, ...] | list[str]) -> tuple[str, ...]:
return tuple(sorted(set(data_paths)))
@@ -1,194 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from app.simulation.reporting.amesim_results import AmesimResults
from app.simulation.reporting.test_mql_variables import (
TestMqlVariableBinding,
TestMqlVariableCatalog,
build_test_mql_variable_catalog,
)
from app.simulation.examples.test_mql.pneumatic import (
TestMqlPneumaticAssembly,
build_test_mql_pneumatic_assembly,
)
G_PER_S_TO_KG_PER_S = 1.0e-3
@dataclass(frozen=True)
class TestMqlOrificeObservation:
time: float
mass_flow_kg_s: float
enthalpy_flow_w: float
mass_flow_parameter: float
gas_velocity_m_s: float
opening: float
effective_area_m2: float
@dataclass(frozen=True)
class TestMqlOrificeBinding:
alias: str
submodel: str
nominal_area_m2: float
flow_coefficient: float
primary_mass_flow_path: str
primary_enthalpy_flow_path: str
reversed_mass_flow_path: str
reversed_enthalpy_flow_path: str
mass_flow_parameter_path: str
gas_velocity_path: str
opening_path: str | None
@property
def is_variable(self) -> bool:
return self.opening_path is not None
def opening_series(self, results: AmesimResults) -> tuple[float, ...]:
if self.opening_path is None:
return tuple(1.0 for _ in results.times)
return tuple(results.series(self.opening_path))
def mass_flow_kg_s_series(self, results: AmesimResults) -> tuple[float, ...]:
return tuple(value * G_PER_S_TO_KG_PER_S for value in results.series(self.primary_mass_flow_path))
def reversed_mass_flow_kg_s_series(self, results: AmesimResults) -> tuple[float, ...]:
return tuple(value * G_PER_S_TO_KG_PER_S for value in results.series(self.reversed_mass_flow_path))
def effective_area_series(self, results: AmesimResults) -> tuple[float, ...]:
return tuple(self.nominal_area_m2 * max(opening, 0.0) for opening in self.opening_series(results))
def observation_at(self, results: AmesimResults, index: int) -> TestMqlOrificeObservation:
opening = self.opening_series(results)[index]
return TestMqlOrificeObservation(
time=results.times[index],
mass_flow_kg_s=results.series(self.primary_mass_flow_path)[index] * G_PER_S_TO_KG_PER_S,
enthalpy_flow_w=results.series(self.primary_enthalpy_flow_path)[index],
mass_flow_parameter=results.series(self.mass_flow_parameter_path)[index],
gas_velocity_m_s=results.series(self.gas_velocity_path)[index],
opening=opening,
effective_area_m2=self.nominal_area_m2 * max(opening, 0.0),
)
@dataclass(frozen=True)
class TestMqlOrificeObservationCatalog:
bindings: tuple[TestMqlOrificeBinding, ...]
@property
def fixed_count(self) -> int:
return sum(1 for binding in self.bindings if binding.submodel == "PNOR001")
@property
def variable_count(self) -> int:
return sum(1 for binding in self.bindings if binding.submodel == "PNVO001")
def by_alias(self, alias: str) -> TestMqlOrificeBinding:
for binding in self.bindings:
if binding.alias == alias:
return binding
raise KeyError(alias)
def build_test_mql_orifice_observation_catalog(
results: AmesimResults,
*,
variable_catalog: TestMqlVariableCatalog | None = None,
assembly: TestMqlPneumaticAssembly | None = None,
) -> TestMqlOrificeObservationCatalog:
variable_catalog = variable_catalog or build_test_mql_variable_catalog(results)
assembly = assembly or build_test_mql_pneumatic_assembly()
bindings = []
for alias, orifice in {
**assembly.fixed_orifices,
**assembly.variable_orifices,
}.items():
owner_variables = tuple(
variable
for variable in variable_catalog.variables
if variable.owner_alias == alias
)
primary_mass_flow = _find_primary(owner_variables, signal_prefix="dm")
primary_enthalpy_flow = _find_primary(owner_variables, signal_prefix="dh")
reversed_mass_flow = _find_reversed(owner_variables, signal_prefix="dm")
reversed_enthalpy_flow = _find_reversed(owner_variables, signal_prefix="dh")
mass_flow_parameter = _find_by_signal(owner_variables, "cm")
gas_velocity = _find_by_signal(owner_variables, "gasvel")
opening = _find_optional_by_signal(owner_variables, "xv")
bindings.append(
TestMqlOrificeBinding(
alias=alias,
submodel=primary_mass_flow.submodel,
nominal_area_m2=orifice.area,
flow_coefficient=orifice.flow_coefficient,
primary_mass_flow_path=primary_mass_flow.data_path,
primary_enthalpy_flow_path=primary_enthalpy_flow.data_path,
reversed_mass_flow_path=reversed_mass_flow.data_path,
reversed_enthalpy_flow_path=reversed_enthalpy_flow.data_path,
mass_flow_parameter_path=mass_flow_parameter.data_path,
gas_velocity_path=gas_velocity.data_path,
opening_path=opening.data_path if opening is not None else None,
)
)
return TestMqlOrificeObservationCatalog(
bindings=tuple(sorted(bindings, key=lambda binding: binding.alias))
)
def _find_primary(
variables: tuple[TestMqlVariableBinding, ...],
*,
signal_prefix: str,
) -> TestMqlVariableBinding:
matches = [
variable
for variable in variables
if variable.signal_name.startswith(signal_prefix)
and "sign reversed duplicate" not in variable.label
]
return _single(matches, f"primary {signal_prefix}")
def _find_reversed(
variables: tuple[TestMqlVariableBinding, ...],
*,
signal_prefix: str,
) -> TestMqlVariableBinding:
matches = [
variable
for variable in variables
if variable.signal_name.startswith(signal_prefix)
and "sign reversed duplicate" in variable.label
]
return _single(matches, f"reversed {signal_prefix}")
def _find_by_signal(
variables: tuple[TestMqlVariableBinding, ...],
signal_name: str,
) -> TestMqlVariableBinding:
return _single(
[variable for variable in variables if variable.signal_name == signal_name],
signal_name,
)
def _find_optional_by_signal(
variables: tuple[TestMqlVariableBinding, ...],
signal_name: str,
) -> TestMqlVariableBinding | None:
matches = [variable for variable in variables if variable.signal_name == signal_name]
if not matches:
return None
return _single(matches, signal_name)
def _single(
matches: list[TestMqlVariableBinding],
description: str,
) -> TestMqlVariableBinding:
if len(matches) != 1:
raise ValueError(f"Expected one {description} variable, found {len(matches)}.")
return matches[0]
@@ -1,100 +0,0 @@
from __future__ import annotations
from collections import Counter
from dataclasses import dataclass
from app.simulation.reporting.amesim_results import AmesimResults
from app.simulation.reporting.test_mql_observations import (
TestMqlObservationCatalog,
build_test_mql_observation_catalog,
)
from app.simulation.reporting.test_mql_variables import TestMqlVariableBinding
@dataclass(frozen=True)
class TestMqlOutputSignal:
data_path: str
domain: str
owner_alias: str
owner_kind: str
submodel: str
signal_name: str
units: str | None
amesim_index: int
saved: bool
@dataclass(frozen=True)
class TestMqlOutputSchema:
signals: tuple[TestMqlOutputSignal, ...]
@property
def signal_count(self) -> int:
return len(self.signals)
def by_data_path(self, data_path: str) -> TestMqlOutputSignal:
for signal in self.signals:
if signal.data_path == data_path:
return signal
raise KeyError(data_path)
def data_paths(self) -> tuple[str, ...]:
return tuple(signal.data_path for signal in self.signals)
def data_paths_by_domain(self, domain: str) -> tuple[str, ...]:
return tuple(signal.data_path for signal in self.signals if signal.domain == domain)
def counts_by_domain(self) -> dict[str, int]:
return dict(Counter(signal.domain for signal in self.signals))
def counts_by_submodel(self) -> dict[str, int]:
return dict(Counter(signal.submodel for signal in self.signals))
def counts_by_owner_kind(self) -> dict[str, int]:
return dict(Counter(signal.owner_kind for signal in self.signals))
def counts_by_units(self) -> dict[str | None, int]:
return dict(Counter(signal.units for signal in self.signals))
def build_test_mql_output_schema(
results: AmesimResults,
*,
observation_catalog: TestMqlObservationCatalog | None = None,
) -> TestMqlOutputSchema:
observation_catalog = observation_catalog or build_test_mql_observation_catalog(results)
domain_by_data_path = _domain_by_data_path(observation_catalog)
signals = []
for data_path in sorted(domain_by_data_path):
variable = observation_catalog.variable_catalog.by_data_path(data_path)
signals.append(_signal_from_variable(variable, domain_by_data_path[data_path]))
return TestMqlOutputSchema(signals=tuple(signals))
def _domain_by_data_path(
observation_catalog: TestMqlObservationCatalog,
) -> dict[str, str]:
domain_by_data_path = {}
for domain, data_paths in observation_catalog.data_paths_by_domain().items():
for data_path in data_paths:
if data_path in domain_by_data_path:
raise ValueError(f"Data_Path {data_path!r} is assigned to multiple domains.")
domain_by_data_path[data_path] = domain
return domain_by_data_path
def _signal_from_variable(
variable: TestMqlVariableBinding,
domain: str,
) -> TestMqlOutputSignal:
return TestMqlOutputSignal(
data_path=variable.data_path,
domain=domain,
owner_alias=variable.owner_alias,
owner_kind=variable.owner_kind,
submodel=variable.submodel,
signal_name=variable.signal_name,
units=variable.units,
amesim_index=variable.index,
saved=variable.saved,
)
@@ -1,161 +0,0 @@
from __future__ import annotations
from dataclasses import dataclass
from math import isfinite
from app.simulation.reporting.amesim_results import AmesimResults
from app.simulation.reporting.test_mql_comparison import (
TestMqlComparisonResult,
compare_test_mql_series,
)
from app.simulation.reporting.test_mql_output_schema import TestMqlOutputSchema
class TestMqlOutputValidationError(ValueError):
"""Raised when a Python test_mql output does not satisfy the AMESim output contract."""
@dataclass(frozen=True)
class TestMqlValidatedOutput:
times: tuple[float, ...]
series_by_data_path: dict[str, tuple[float, ...]]
data_paths: tuple[str, ...]
def series(self, data_path: str) -> tuple[float, ...]:
if data_path not in self.series_by_data_path:
raise KeyError(data_path)
return self.series_by_data_path[data_path]
def validate_test_mql_output(
*,
times: tuple[float, ...] | list[float],
series_by_data_path: dict[str, tuple[float, ...] | list[float]],
schema: TestMqlOutputSchema,
data_paths: tuple[str, ...] | list[str] | None = None,
allow_extra_paths: bool = False,
require_all_schema_paths: bool = False,
) -> TestMqlValidatedOutput:
validated_times = _validate_time_axis(times)
selected_paths = _select_paths(
series_by_data_path=series_by_data_path,
schema=schema,
data_paths=data_paths,
allow_extra_paths=allow_extra_paths,
require_all_schema_paths=require_all_schema_paths,
)
validated_series = {
data_path: _validate_series(
data_path=data_path,
values=series_by_data_path[data_path],
expected_count=len(validated_times),
)
for data_path in selected_paths
}
return TestMqlValidatedOutput(
times=validated_times,
series_by_data_path=validated_series,
data_paths=selected_paths,
)
def compare_validated_test_mql_output(
*,
times: tuple[float, ...] | list[float],
series_by_data_path: dict[str, tuple[float, ...] | list[float]],
schema: TestMqlOutputSchema,
amesim_results: AmesimResults,
data_paths: tuple[str, ...] | list[str] | None = None,
allow_extra_paths: bool = False,
require_all_schema_paths: bool = False,
relative_floor: float = 1.0e-12,
) -> TestMqlComparisonResult:
validated = validate_test_mql_output(
times=times,
series_by_data_path=series_by_data_path,
schema=schema,
data_paths=data_paths,
allow_extra_paths=allow_extra_paths,
require_all_schema_paths=require_all_schema_paths,
)
return compare_test_mql_series(
python_times=validated.times,
python_series_by_data_path=validated.series_by_data_path,
amesim_results=amesim_results,
data_paths=validated.data_paths,
relative_floor=relative_floor,
)
def _validate_time_axis(times: tuple[float, ...] | list[float]) -> tuple[float, ...]:
if not times:
raise TestMqlOutputValidationError("Python time axis is empty.")
validated = tuple(_finite_float("time", value) for value in times)
previous = validated[0]
for value in validated[1:]:
if value < previous:
raise TestMqlOutputValidationError("Python time axis must be monotonically increasing.")
previous = value
return validated
def _select_paths(
*,
series_by_data_path: dict[str, tuple[float, ...] | list[float]],
schema: TestMqlOutputSchema,
data_paths: tuple[str, ...] | list[str] | None,
allow_extra_paths: bool,
require_all_schema_paths: bool,
) -> tuple[str, ...]:
schema_paths = set(schema.data_paths())
provided_paths = set(series_by_data_path)
if not allow_extra_paths:
extra_paths = sorted(provided_paths - schema_paths)
if extra_paths:
raise TestMqlOutputValidationError(
f"Python output contains Data_Path values outside test_mql schema: {extra_paths}"
)
if require_all_schema_paths:
missing_schema_paths = sorted(schema_paths - provided_paths)
if missing_schema_paths:
raise TestMqlOutputValidationError(
f"Python output is missing required test_mql schema Data_Path values: {missing_schema_paths}"
)
selected_paths = tuple(data_paths) if data_paths is not None else tuple(sorted(provided_paths & schema_paths))
if not selected_paths:
raise TestMqlOutputValidationError("no test_mql schema Data_Path values are available.")
unknown_selected = [data_path for data_path in selected_paths if data_path not in schema_paths]
if unknown_selected:
raise TestMqlOutputValidationError(
f"Requested Data_Path values are outside test_mql schema: {unknown_selected}"
)
missing_selected = [data_path for data_path in selected_paths if data_path not in series_by_data_path]
if missing_selected:
raise TestMqlOutputValidationError(
f"Python output is missing selected Data_Path values: {missing_selected}"
)
return selected_paths
def _validate_series(
*,
data_path: str,
values: tuple[float, ...] | list[float],
expected_count: int,
) -> tuple[float, ...]:
if len(values) != expected_count:
raise TestMqlOutputValidationError(
f"Python series length mismatch for {data_path!r}: "
f"{len(values)} values for {expected_count} time samples."
)
return tuple(_finite_float(data_path, value) for value in values)
def _finite_float(label: str, value: float) -> float:
try:
numeric_value = float(value)
except (TypeError, ValueError) as exc:
raise TestMqlOutputValidationError(f"{label!r} contains a non-numeric value: {value!r}") from exc
if not isfinite(numeric_value):
raise TestMqlOutputValidationError(f"{label!r} contains a non-finite value: {value!r}")
return numeric_value
@@ -1,111 +0,0 @@
from __future__ import annotations
import re
from collections import Counter
from dataclasses import dataclass
from app.simulation.reporting.amesim_results import AmesimResults, AmesimVariable
from app.simulation.examples.test_mql.system import COMPONENT_SPECS, CONNECTION_SPECS
_UNIT_RE = re.compile(r"\[([^\]]+)\]\s*$")
@dataclass(frozen=True)
class TestMqlVariableBinding:
index: int
data_path: str
signal_name: str
owner_alias: str
owner_kind: str
submodel: str
label: str
units: str | None
saved: bool
@dataclass(frozen=True)
class TestMqlVariableCatalog:
variables: tuple[TestMqlVariableBinding, ...]
@property
def data_path_count(self) -> int:
return len(self.variables)
@property
def saved_data_path_count(self) -> int:
return sum(1 for variable in self.variables if variable.saved)
def by_data_path(self, data_path: str) -> TestMqlVariableBinding:
for variable in self.variables:
if variable.data_path == data_path:
return variable
raise KeyError(data_path)
def counts_by_submodel(self) -> dict[str, int]:
return dict(Counter(variable.submodel for variable in self.variables))
def counts_by_owner_kind(self) -> dict[str, int]:
return dict(Counter(variable.owner_kind for variable in self.variables))
def data_paths_for_owner(self, owner_alias: str) -> tuple[str, ...]:
return tuple(
variable.data_path
for variable in self.variables
if variable.owner_alias == owner_alias
)
def build_test_mql_variable_catalog(amesim_results: AmesimResults) -> TestMqlVariableCatalog:
owner_map = _build_owner_map()
saved_indices = set(amesim_results.saved_variable_indices)
bindings = []
for variable in amesim_results.variables:
if variable.data_path is None:
continue
signal_name, owner_alias = split_data_path(variable.data_path)
owner_kind, submodel = owner_map[owner_alias]
bindings.append(
TestMqlVariableBinding(
index=variable.index,
data_path=variable.data_path,
signal_name=signal_name,
owner_alias=owner_alias,
owner_kind=owner_kind,
submodel=submodel,
label=variable.label,
units=_extract_units(variable),
saved=variable.index in saved_indices,
)
)
return TestMqlVariableCatalog(variables=tuple(bindings))
def split_data_path(data_path: str) -> tuple[str, str]:
if "@" not in data_path:
raise ValueError(f"AMESim Data_Path does not contain an owner alias: {data_path!r}")
signal_name, owner_alias = data_path.rsplit("@", 1)
if not signal_name or not owner_alias:
raise ValueError(f"Invalid AMESim Data_Path: {data_path!r}")
return signal_name, owner_alias
def _build_owner_map() -> dict[str, tuple[str, str]]:
owner_map = {
str(spec["alias"]): ("component", str(spec["submodel"]))
for spec in COMPONENT_SPECS
}
owner_map.update(
{
str(spec["alias"]): ("connection", str(spec["submodel"]))
for spec in CONNECTION_SPECS
}
)
return owner_map
def _extract_units(variable: AmesimVariable) -> str | None:
match = _UNIT_RE.search(variable.label)
if match is None:
return None
return match.group(1)
@@ -1,393 +0,0 @@
from __future__ import annotations
from bisect import bisect_left
import csv
from dataclasses import dataclass
from pathlib import Path
from typing import Any
PRIMARY_KEYS = (
"mytank.p",
"mytank.T",
"mycylinder.p",
"mycylinder.T",
)
MODELICA_COMPARISON_COLUMNS = {
"mytank.p": "mytank.p",
"mytank.T": "mytank.T",
"mycylinder.p": "mycylinder.p",
"mycylinder.T": "mycylinder.T",
"branch.upper_branch.p": "mypipe.p",
"branch.upper_branch.in": "myorifice.port_a.m_flow",
"branch.upper_branch.out": "mytee1.port_out2.m_flow",
"branch.lower_branch.p": "mypipe1.p",
"branch.lower_branch.in": "myorifice1.port_a.m_flow",
"branch.lower_branch.out": "mytee1.port_out1.m_flow",
}
COMPARISON_KEYS = tuple(MODELICA_COMPARISON_COLUMNS.keys())
def _branch_series_values(
series: dict[str, list[float]],
branch_name: str,
legacy_key: str,
) -> list[float]:
generic_key = f"branch.{branch_name}.{legacy_key.split('.')[-1]}"
if generic_key in series:
return series[generic_key]
return series[legacy_key]
@dataclass(frozen=True)
class TestModelArtifacts:
primary_csv_path: Path
temperature_csv_path: Path
temperature_svg_path: Path
run_report_path: Path
comparison_csv_path: Path | None = None
comparison_summary_path: Path | None = None
def format_testmodel_run_report(
*,
network_summary: str,
initialization: Any,
raw_initial_state: tuple[float, ...],
consistent_initial_state: tuple[float, ...],
solution: Any,
series: dict[str, list[float]],
solve_diagnostics: Any,
artifacts: TestModelArtifacts,
comparison_summary: dict[str, tuple[float, float]] | None,
) -> str:
lines = [
network_summary,
"",
f"Initialization converged: {initialization.converged}",
f"Initialization iterations: {initialization.iterations}",
f"Initialization max state delta: {initialization.max_state_delta:.6e}",
f"Initialization max flow delta: {initialization.max_flow_delta:.6e}",
f"Initialization max enthalpy delta: {initialization.max_enthalpy_delta:.6e}",
(
"Initialization downstream pressure spread: "
f"{initialization.downstream_pressure_spread:.6e}"
),
"",
"Raw initial state vector:",
str(list(raw_initial_state)),
"",
"Constraint-consistent initial state vector:",
str(list(consistent_initial_state)),
"",
f"Solver success: {solution.success}",
f"Solver message: {solution.message}",
f"Final time: {solution.t[-1]:.2f} s",
f"Final tank pressure: {series['mytank.p'][-1]:.3f} Pa",
f"Final tank temperature: {series['mytank.T'][-1]:.3f} K",
f"Final cylinder pressure: {series['mycylinder.p'][-1]:.3f} Pa",
(
"Final branch inflow: "
f"{_branch_series_values(series, 'upper_branch', 'branch_upper.in')[-1] + _branch_series_values(series, 'lower_branch', 'branch_lower.in')[-1]:.6f} kg/s"
),
]
if solve_diagnostics is not None:
lines.extend(
[
"",
"Final closure solve diagnostics:",
(
"Upper branch inlet solve: "
f"converged={solve_diagnostics.upper_branch_inlet.converged}, "
f"iterations={solve_diagnostics.upper_branch_inlet.iterations}, "
f"residual={solve_diagnostics.upper_branch_inlet.residual:.6e}"
),
(
"Lower branch inlet solve: "
f"converged={solve_diagnostics.lower_branch_inlet.converged}, "
f"iterations={solve_diagnostics.lower_branch_inlet.iterations}, "
f"residual={solve_diagnostics.lower_branch_inlet.residual:.6e}"
),
]
)
if solve_diagnostics.downstream_pressure_projection is not None:
lines.append(
"Downstream pressure projection: "
f"converged={solve_diagnostics.downstream_pressure_projection.converged}, "
f"iterations={solve_diagnostics.downstream_pressure_projection.iterations}, "
f"residual={solve_diagnostics.downstream_pressure_projection.residual:.6e}"
)
lines.extend(
[
f"Primary series CSV: {artifacts.primary_csv_path}",
f"Temperature CSV: {artifacts.temperature_csv_path}",
f"Temperature plot: {artifacts.temperature_svg_path}",
f"Run report TXT: {artifacts.run_report_path}",
]
)
if (
artifacts.comparison_csv_path is not None
and artifacts.comparison_summary_path is not None
):
lines.extend(
[
f"Modelica comparison CSV: {artifacts.comparison_csv_path}",
f"Modelica comparison summary: {artifacts.comparison_summary_path}",
]
)
if comparison_summary is not None:
for key, (max_abs_error, max_rel_error) in comparison_summary.items():
lines.append(
f"{key} max abs error: {max_abs_error:.6f}, "
f"max rel error: {max_rel_error:.6%}"
)
return "\n".join(lines) + "\n"
def write_testmodel_run_report(output_dir: Path, report_text: str) -> Path:
report_path = output_dir / "testmodel_run_report.txt"
report_path.write_text(report_text, encoding="utf-8")
return report_path
def _write_primary_series_csv(output_dir: Path, series: dict[str, list[float]]) -> Path:
csv_path = output_dir / "testmodel_primary_series.csv"
with csv_path.open("w", newline="", encoding="utf-8") as handle:
writer = csv.writer(handle)
writer.writerow(["time_s", *PRIMARY_KEYS])
for index, time_value in enumerate(series["time"]):
writer.writerow([time_value, *(series[key][index] for key in PRIMARY_KEYS)])
return csv_path
def _write_temperature_csv(output_dir: Path, time_values: list[float], temperatures: list[float]) -> Path:
csv_path = output_dir / "testmodel_tank_temperature.csv"
with csv_path.open("w", newline="", encoding="utf-8") as handle:
writer = csv.writer(handle)
writer.writerow(["time_s", "mytank_T_K"])
writer.writerows(zip(time_values, temperatures))
return csv_path
def _write_temperature_svg(output_dir: Path, time_values: list[float], temperatures: list[float]) -> Path:
svg_path = output_dir / "testmodel_tank_temperature.svg"
width = 900
height = 520
left = 90
right = 40
top = 60
bottom = 70
plot_width = width - left - right
plot_height = height - top - bottom
min_time = min(time_values)
max_time = max(time_values)
min_temp = min(temperatures)
max_temp = max(temperatures)
temp_padding = max(1.0, (max_temp - min_temp) * 0.08)
min_temp -= temp_padding
max_temp += temp_padding
def scale_x(value: float) -> float:
return left + (value - min_time) / max(max_time - min_time, 1e-12) * plot_width
def scale_y(value: float) -> float:
return top + (max_temp - value) / max(max_temp - min_temp, 1e-12) * plot_height
points = " ".join(
f"{scale_x(time_value):.2f},{scale_y(temperature):.2f}"
for time_value, temperature in zip(time_values, temperatures)
)
x_ticks = 5
y_ticks = 5
x_tick_markup = []
y_tick_markup = []
for index in range(x_ticks + 1):
fraction = index / x_ticks
time_value = min_time + fraction * (max_time - min_time)
x = left + fraction * plot_width
x_tick_markup.append(
f'<line x1="{x:.2f}" y1="{top}" x2="{x:.2f}" y2="{top + plot_height}" '
'stroke="#d9e2ec" stroke-width="1" />'
)
x_tick_markup.append(
f'<text x="{x:.2f}" y="{height - 30}" text-anchor="middle" '
'font-size="14" fill="#102a43">'
f"{time_value:.1f}</text>"
)
for index in range(y_ticks + 1):
fraction = index / y_ticks
temp_value = min_temp + fraction * (max_temp - min_temp)
y = top + plot_height - fraction * plot_height
y_tick_markup.append(
f'<line x1="{left}" y1="{y:.2f}" x2="{left + plot_width}" y2="{y:.2f}" '
'stroke="#d9e2ec" stroke-width="1" />'
)
y_tick_markup.append(
f'<text x="{left - 12}" y="{y + 5:.2f}" text-anchor="end" '
'font-size="14" fill="#102a43">'
f"{temp_value:.1f}</text>"
)
svg_content = f"""<svg xmlns="http://www.w3.org/2000/svg" width="{width}" height="{height}" viewBox="0 0 {width} {height}">
<rect width="{width}" height="{height}" fill="#f7fafc" rx="18" ry="18" />
<text x="{width / 2:.0f}" y="32" text-anchor="middle" font-size="24" fill="#102a43">Python Testmodel Tank Temperature</text>
<text x="{width / 2:.0f}" y="{height - 8}" text-anchor="middle" font-size="16" fill="#486581">Time (s)</text>
<text x="26" y="{height / 2:.0f}" text-anchor="middle" font-size="16" fill="#486581" transform="rotate(-90 26 {height / 2:.0f})">Temperature (K)</text>
<rect x="{left}" y="{top}" width="{plot_width}" height="{plot_height}" fill="#ffffff" stroke="#bcccdc" stroke-width="1.5" />
{''.join(x_tick_markup)}
{''.join(y_tick_markup)}
<polyline fill="none" stroke="#d64545" stroke-width="3" stroke-linejoin="round" stroke-linecap="round" points="{points}" />
</svg>
"""
svg_path.write_text(svg_content, encoding="utf-8")
return svg_path
def load_modelica_series(csv_path: Path, variable_names: tuple[str, ...]) -> dict[str, list[float]]:
series = {"time": []}
for variable_name in variable_names:
series[variable_name] = []
with csv_path.open("r", newline="", encoding="utf-8") as handle:
reader = csv.DictReader(handle)
available_variable_names = tuple(
variable_name
for variable_name in variable_names
if MODELICA_COMPARISON_COLUMNS.get(variable_name, variable_name) in (reader.fieldnames or ())
)
for row in reader:
series["time"].append(float(row["time"]))
for variable_name in available_variable_names:
modelica_column = MODELICA_COMPARISON_COLUMNS.get(variable_name, variable_name)
series[variable_name].append(float(row[modelica_column]))
return series
def _interpolate_series_value(time_values: list[float], values: list[float], target_time: float) -> float:
if target_time <= time_values[0]:
return values[0]
if target_time >= time_values[-1]:
return values[-1]
right_index = bisect_left(time_values, target_time)
if right_index < len(time_values) and abs(time_values[right_index] - target_time) <= 1e-12:
return values[right_index]
left_index = right_index - 1
left_time = time_values[left_index]
right_time = time_values[right_index]
fraction = (target_time - left_time) / (right_time - left_time)
return values[left_index] + fraction * (values[right_index] - values[left_index])
def write_modelica_comparison(
output_dir: Path,
python_series: dict[str, list[float]],
modelica_series: dict[str, list[float]],
) -> tuple[Path, Path, dict[str, tuple[float, float]]]:
comparison_csv_path = output_dir / "testmodel_modelica_comparison.csv"
summary_path = output_dir / "testmodel_modelica_comparison_summary.txt"
summary: dict[str, tuple[float, float]] = {}
with comparison_csv_path.open("w", newline="", encoding="utf-8") as handle:
writer = csv.writer(handle)
header = ["time_s"]
comparison_keys = tuple(
key
for key in COMPARISON_KEYS
if key in python_series and key in modelica_series and modelica_series[key]
)
for key in comparison_keys:
header.extend(
[
f"python.{key}",
f"modelica.{key}",
f"abs_error.{key}",
f"rel_error.{key}",
]
)
writer.writerow(header)
max_abs_errors = {key: 0.0 for key in comparison_keys}
max_rel_errors = {key: 0.0 for key in comparison_keys}
for index, time_value in enumerate(python_series["time"]):
row = [time_value]
for key in comparison_keys:
python_value = python_series[key][index]
modelica_value = _interpolate_series_value(
modelica_series["time"],
modelica_series[key],
time_value,
)
abs_error = abs(python_value - modelica_value)
rel_error = abs_error / max(abs(modelica_value), 1e-9)
max_abs_errors[key] = max(max_abs_errors[key], abs_error)
max_rel_errors[key] = max(max_rel_errors[key], rel_error)
row.extend([python_value, modelica_value, abs_error, rel_error])
writer.writerow(row)
summary_lines = []
for key in comparison_keys:
summary[key] = (max_abs_errors[key], max_rel_errors[key])
summary_lines.append(
f"{key}: max_abs_error={max_abs_errors[key]:.6f}, "
f"max_rel_error={max_rel_errors[key]:.6%}"
)
summary_path.write_text("\n".join(summary_lines) + "\n", encoding="utf-8")
return comparison_csv_path, summary_path, summary
def export_testmodel_artifacts(
*,
output_dir: Path,
series: dict[str, list[float]],
modelica_series: dict[str, list[float]] | None = None,
) -> tuple[TestModelArtifacts, dict[str, tuple[float, float]] | None]:
output_dir.mkdir(parents=True, exist_ok=True)
primary_csv_path = _write_primary_series_csv(output_dir, series)
temperature_csv_path = _write_temperature_csv(
output_dir,
series["time"],
series["mytank.T"],
)
temperature_svg_path = _write_temperature_svg(
output_dir,
series["time"],
series["mytank.T"],
)
comparison_csv_path = None
comparison_summary_path = None
comparison_summary = None
if modelica_series is not None:
(
comparison_csv_path,
comparison_summary_path,
comparison_summary,
) = write_modelica_comparison(output_dir, series, modelica_series)
return (
TestModelArtifacts(
primary_csv_path=primary_csv_path,
temperature_csv_path=temperature_csv_path,
temperature_svg_path=temperature_svg_path,
run_report_path=output_dir / "testmodel_run_report.txt",
comparison_csv_path=comparison_csv_path,
comparison_summary_path=comparison_summary_path,
),
comparison_summary,
)
+49
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@@ -0,0 +1,49 @@
"""Backend-neutral simulation result and preparation error contracts."""
from __future__ import annotations
from dataclasses import dataclass
from typing import Literal
from app.simulation.core.metadata import ResultVariableMetadata
SimulationRunStatus = Literal["completed", "cancelled", "failed"]
@dataclass(frozen=True)
class SimulationPreparationIssue:
code: str
message: str
def as_dict(self) -> dict[str, str]:
return {"code": self.code, "message": self.message}
class SimulationPreparationError(ValueError):
def __init__(self, issues: tuple[SimulationPreparationIssue, ...]) -> None:
super().__init__("The compiled model is not ready for simulation.")
self.issues = issues
@dataclass(frozen=True)
class GenericSimulationResult:
success: bool
status: SimulationRunStatus
message: str
simulated_until: float
requested_stop_time: float
variables: tuple[ResultVariableMetadata, ...]
series: dict[str, list[float]]
final: dict[str, float]
diagnostics: dict[str, object]
def as_dict(self) -> dict[str, object]:
return {
"success": self.success,
"status": self.status,
"partial": self.status != "completed",
"message": self.message,
"simulatedUntil": self.simulated_until,
"requestedStopTime": self.requested_stop_time,
"variables": [variable.as_dict() for variable in self.variables],
"series": self.series,
"final": self.final,
"diagnostics": self.diagnostics,
}
+101
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@@ -0,0 +1,101 @@
"""Validate the requested output time grid before starting the C worker."""
from __future__ import annotations
from math import floor, isfinite
from sys import maxsize
from app.simulation.config import SolveIVPConfig
class SimulationSampleTimeError(ValueError):
"""Stable failure contract for an unsafe or unrepresentable sample grid."""
def __init__(self, code: str, message: str) -> None:
super().__init__(message)
self.code = code
def simulation_sample_times(
config: SolveIVPConfig,
step: float,
) -> list[float]:
t_start = float(config.t_start)
t_stop = float(config.t_stop)
if not isfinite(t_start) or not isfinite(t_stop):
raise SimulationSampleTimeError(
"SIMULATION_VALUE_NOT_FINITE",
"Simulation start and stop times must be finite.",
)
if step <= 0.0 or not isfinite(step):
raise SimulationSampleTimeError(
"SIMULATION_SAMPLE_STEP_INVALID",
"Simulation sample step must be finite and greater than zero.",
)
duration = t_stop - t_start
if not isfinite(duration):
raise SimulationSampleTimeError(
"SIMULATION_TIME_SPAN_NOT_FINITE",
"Simulation time span must be finite.",
)
if duration <= 0.0:
raise SimulationSampleTimeError(
"SIMULATION_TIME_RANGE_INVALID",
"Simulation stop time must be greater than start time.",
)
ratio = duration / step
if not isfinite(ratio):
raise SimulationSampleTimeError(
"SIMULATION_SAMPLE_COUNT_UNREPRESENTABLE",
"Simulation sample count cannot be represented by this runtime; "
"increase sampleStep.",
)
interval_count = floor(ratio)
# There is no product-level point cap. Still reject a collection that the
# Python runtime cannot index before multiplying by the potentially huge
# interval count or allocating the output grid.
if interval_count > maxsize - 2:
raise SimulationSampleTimeError(
"SIMULATION_SAMPLE_COUNT_UNREPRESENTABLE",
"Simulation sample count cannot be represented by this runtime; "
"increase sampleStep.",
)
last_regular_time = t_start + interval_count * step
append_stop = last_regular_time < t_stop
requested_point_count = interval_count + 1 + int(append_stop)
if requested_point_count > maxsize:
raise SimulationSampleTimeError(
"SIMULATION_SAMPLE_COUNT_UNREPRESENTABLE",
"Simulation sample count cannot be represented by this runtime; "
"increase sampleStep.",
)
times = [t_start]
for index in range(1, interval_count + 1):
candidate = t_start + index * step
if not isfinite(candidate):
raise SimulationSampleTimeError(
"SIMULATION_SAMPLE_TIME_UNREPRESENTABLE",
"Simulation sampleStep cannot be represented over the requested "
"absolute time range.",
)
if candidate >= t_stop:
candidate = t_stop
if candidate <= times[-1]:
raise SimulationSampleTimeError(
"SIMULATION_SAMPLE_TIME_UNREPRESENTABLE",
"Simulation sampleStep is too small to advance floating-point "
"time over the requested absolute time range.",
)
times.append(candidate)
if candidate == t_stop:
break
if times[-1] < t_stop:
times.append(t_stop)
if len(times) < 2 or any(
current >= following
for current, following in zip(times, times[1:])
):
raise SimulationSampleTimeError(
"SIMULATION_SAMPLE_TIME_UNREPRESENTABLE",
"Simulation sample times must contain at least two strictly "
"increasing values.",
)
return times
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@@ -1 +0,0 @@
"""Numerical solvers used by simulation systems."""
File diff suppressed because it is too large. Load diff
File diff suppressed because it is too large. Load diff
-794
View File
@@ -1,794 +0,0 @@
"""Executable reference IR for compile-proven causal algebraic programs.
The IR eliminates duplicate *logical* effort coordinates, but intentionally
keeps a compatibility scatter map to existing ``PortState`` objects. Stream
propagation, derivatives, and result collection still consume those objects;
this is a reference for a future flat backend, not physical slot deletion.
"""
from __future__ import annotations
from collections.abc import Callable, Iterable
from dataclasses import dataclass, replace
from enum import StrEnum
from hashlib import sha256
import json
from math import isfinite
from typing import TYPE_CHECKING, Any
if TYPE_CHECKING:
import numpy as np
CAUSAL_NUMERIC_IR_SCHEMA_VERSION = 1
PRESSURE_LOWER_BOUND_PA = 0.0
class CausalIROpcode(StrEnum):
EFFORT_BROADCAST = "effort_broadcast"
EFFORT_DIRECT_RESIDUAL = "effort_direct_residual"
EFFORT_COMPONENT_RESIDUAL = "effort_component_residual"
FLOW_DIRECT = "flow_direct"
FLOW_COMPONENT_RESIDUAL = "flow_component_residual"
@dataclass(frozen=True, slots=True)
class CausalIRCompatibilitySlot:
slot: int
id: str
variable: str
@dataclass(frozen=True, slots=True)
class CausalIRCanonicalSlot:
slot: int
id: str
variable: str
kind: str
@dataclass(frozen=True, slots=True)
class CausalIREffortOperation:
opcode: CausalIROpcode
variable: str
result_slot: int
anchor_compatibility_slot: int
scatter_compatibility_slots: tuple[int, ...]
equation_id: str
@dataclass(frozen=True, slots=True)
class CausalIREffortEvaluation:
opcode: CausalIROpcode
output_indices: tuple[int, ...]
equation_indices: tuple[int, ...]
equation_ids: tuple[str, ...]
evaluator_slot: int
@dataclass(frozen=True, slots=True)
class CausalIREffortStage:
variable: str
operations: tuple[CausalIREffortOperation, ...]
evaluations: tuple[CausalIREffortEvaluation, ...]
@dataclass(frozen=True, slots=True)
class CausalIRFlowOperation:
opcode: CausalIROpcode
output_indices: tuple[int, ...]
equation_indices: tuple[int, ...]
equation_ids: tuple[str, ...]
evaluator_slot: int
@dataclass(frozen=True, slots=True)
class CausalIRFlowStage:
target_slots: tuple[int, ...]
scatter_compatibility_slots: tuple[int, ...]
equation_ids: tuple[str, ...]
operations: tuple[CausalIRFlowOperation, ...]
@dataclass(frozen=True, slots=True)
class CausalIRProgram:
"""Immutable callback-free structure used as the backend cache key."""
schema_version: int
canonical_slots: tuple[CausalIRCanonicalSlot, ...]
compatibility_slots: tuple[CausalIRCompatibilitySlot, ...]
reset_compatibility_slots: tuple[int, ...]
external_effort_compatibility_slots: tuple[int, ...]
effort_stages: tuple[CausalIREffortStage, ...]
flow_stages: tuple[CausalIRFlowStage, ...]
structural_signature: str
@property
def assignment_count(self) -> int:
return len(self.canonical_slots)
@property
def effort_group_count(self) -> int:
return sum(len(stage.operations) for stage in self.effort_stages)
@property
def flow_assignment_count(self) -> int:
return sum(len(stage.target_slots) for stage in self.flow_stages)
@property
def effort_scatter_count(self) -> int:
return sum(
len(operation.scatter_compatibility_slots)
for stage in self.effort_stages
for operation in stage.operations
)
@property
def eliminated_effort_replica_count(self) -> int:
return self.effort_scatter_count - self.effort_group_count
@property
def maximum_effort_stage_width(self) -> int:
return max((len(stage.operations) for stage in self.effort_stages), default=0)
@property
def maximum_flow_stage_width(self) -> int:
return max((len(stage.target_slots) for stage in self.flow_stages), default=0)
def structural_dict(self) -> dict[str, object]:
return {
"schemaVersion": self.schema_version,
"canonicalSlots": [
{
"slot": item.slot,
"id": item.id,
"variable": item.variable,
"kind": item.kind,
}
for item in self.canonical_slots
],
"compatibilitySlots": [
{"slot": item.slot, "id": item.id, "variable": item.variable}
for item in self.compatibility_slots
],
"resetCompatibilitySlots": list(self.reset_compatibility_slots),
"externalEffortCompatibilitySlots": list(
self.external_effort_compatibility_slots
),
"effortStages": [
{
"variable": stage.variable,
"operations": [
{
"opcode": operation.opcode.value,
"resultSlot": operation.result_slot,
"anchorCompatibilitySlot": (
operation.anchor_compatibility_slot
),
"scatterCompatibilitySlots": list(
operation.scatter_compatibility_slots
),
"equationId": operation.equation_id,
}
for operation in stage.operations
],
"evaluations": [
{
"opcode": evaluation.opcode.value,
"outputIndices": list(evaluation.output_indices),
"equationIndices": list(evaluation.equation_indices),
"equationIds": list(evaluation.equation_ids),
"evaluatorSlot": evaluation.evaluator_slot,
}
for evaluation in stage.evaluations
],
}
for stage in self.effort_stages
],
"flowStages": [
{
"targetSlots": list(stage.target_slots),
"scatterCompatibilitySlots": list(
stage.scatter_compatibility_slots
),
"equationIds": list(stage.equation_ids),
"operations": [
{
"opcode": operation.opcode.value,
"outputIndices": list(operation.output_indices),
"equationIndices": list(operation.equation_indices),
"equationIds": list(operation.equation_ids),
"evaluatorSlot": operation.evaluator_slot,
}
for operation in stage.operations
],
}
for stage in self.flow_stages
],
}
def calculate_structural_signature(self) -> str:
payload = json.dumps(
self.structural_dict(),
ensure_ascii=True,
separators=(",", ":"),
sort_keys=True,
).encode("utf-8")
return sha256(payload).hexdigest()
@dataclass(frozen=True, slots=True)
class CausalIRBindings:
readers: tuple[Callable[[], float], ...]
writers: tuple[Callable[[float], None], ...]
evaluators: tuple[Callable[[], object], ...]
@dataclass(slots=True)
class CausalIRWorkspace:
structural_signature: str
canonical_values: "np.ndarray[Any, Any]"
effort_residuals: "np.ndarray[Any, Any]"
effort_written: "np.ndarray[Any, Any]"
flow_values: "np.ndarray[Any, Any]"
flow_written: "np.ndarray[Any, Any]"
transaction_values: "np.ndarray[Any, Any]"
@dataclass(frozen=True, slots=True)
class CausalIRExecutionResult:
success: bool
fallback_reason: str | None
structural_signature: str
effort_assignment_count: int
flow_assignment_count: int
completed_effort_stage_count: int
completed_flow_stage_count: int
rolled_back: bool
StageObserver = Callable[
[str, int, tuple[int, ...], tuple[float, ...]],
None,
]
@dataclass(frozen=True, slots=True)
class CausalNumericIR:
"""Bound reference IR; its normal path performs no full snapshot."""
program: CausalIRProgram
bindings: CausalIRBindings
def create_workspace(self) -> CausalIRWorkspace:
try:
import numpy as np
except ImportError as exc: # pragma: no cover
raise RuntimeError("The causal numeric reference IR requires NumPy.") from exc
return CausalIRWorkspace(
structural_signature=self.program.structural_signature,
canonical_values=np.empty(
max(len(self.program.canonical_slots), 1), dtype=np.float64
),
effort_residuals=np.empty(
max(self.program.maximum_effort_stage_width, 1), dtype=np.float64
),
effort_written=np.empty(
max(self.program.maximum_effort_stage_width, 1), dtype=np.bool_
),
flow_values=np.empty(
max(self.program.maximum_flow_stage_width, 1), dtype=np.float64
),
flow_written=np.empty(
max(self.program.maximum_flow_stage_width, 1), dtype=np.bool_
),
transaction_values=np.empty(
max(len(self.program.compatibility_slots), 1), dtype=np.float64
),
)
def execute(
self,
workspace: CausalIRWorkspace,
*,
effort_variables: tuple[str, ...] = ("p",),
transactional: bool = False,
stage_observer: StageObserver | None = None,
) -> CausalIRExecutionResult:
"""Interpret the IR; transactional snapshots are audit-only."""
program = self.program
bindings = self.bindings
signature = program.structural_signature
if workspace.structural_signature != signature:
raise ValueError("Causal IR workspace belongs to a different program.")
if len(bindings.readers) != len(program.compatibility_slots) or len(
bindings.writers
) != len(program.compatibility_slots):
raise ValueError("Causal IR compatibility binding count is inconsistent.")
if any(variable not in {"p", "x", "v"} for variable in effort_variables):
return CausalIRExecutionResult(
False, "unsupportedEffortVariable", signature, 0, 0, 0, 0, False
)
snapshot_count = 0
if transactional:
try:
for slot, reader in enumerate(bindings.readers):
workspace.transaction_values[slot] = float(reader())
snapshot_count += 1
except MemoryError:
raise
except (ArithmeticError, RuntimeError, TypeError, ValueError) as exc:
return CausalIRExecutionResult(
False,
f"slotReadFailed:{type(exc).__name__}",
signature,
0,
0,
0,
0,
False,
)
effort_count = 0
flow_count = 0
completed_effort_stages = 0
completed_flow_stages = 0
def failed(reason: str) -> CausalIRExecutionResult:
rolled_back = False
if transactional:
for slot in range(snapshot_count):
bindings.writers[slot](float(workspace.transaction_values[slot]))
rolled_back = True
return CausalIRExecutionResult(
False,
reason,
signature,
effort_count,
flow_count,
completed_effort_stages,
completed_flow_stages,
rolled_back,
)
selected_efforts = frozenset(effort_variables)
for stage_index, stage in enumerate(program.effort_stages):
if stage.variable not in selected_efforts:
continue
width = len(stage.operations)
workspace.effort_written[:width] = False
for evaluation in stage.evaluations:
try:
evaluated = bindings.evaluators[evaluation.evaluator_slot]()
if evaluation.opcode is CausalIROpcode.EFFORT_DIRECT_RESIDUAL:
output = evaluation.output_indices[0]
workspace.effort_residuals[output] = float(evaluated)
workspace.effort_written[output] = True
continue
if not hasattr(evaluated, "__len__"):
raise TypeError("component evaluator returned no sequence")
for output, equation in zip(
evaluation.output_indices, evaluation.equation_indices
):
if equation >= len(evaluated):
raise IndexError("component equation disappeared")
workspace.effort_residuals[output] = float(evaluated[equation])
workspace.effort_written[output] = True
except MemoryError:
raise
except Exception as exc:
return failed(f"effortEvaluationFailed:{type(exc).__name__}")
if any(not bool(workspace.effort_written[index]) for index in range(width)):
return failed("effortEvaluationCoverageMismatch")
for output, operation in enumerate(stage.operations):
try:
anchor = float(bindings.readers[operation.anchor_compatibility_slot]())
target = anchor - float(workspace.effort_residuals[output])
except MemoryError:
raise
except (
ArithmeticError,
IndexError,
RuntimeError,
TypeError,
ValueError,
) as exc:
return failed(f"effortAssignmentFailed:{type(exc).__name__}")
if not isfinite(target) or (
stage.variable == "p" and target <= PRESSURE_LOWER_BOUND_PA
):
return failed("nonFiniteOrInvalidEffortAssignment")
workspace.canonical_values[operation.result_slot] = target
for slot in operation.scatter_compatibility_slots:
bindings.writers[slot](target)
effort_count += 1
completed_effort_stages += 1
if stage_observer is not None:
try:
stage_observer(
f"effort:{stage.variable}",
stage_index,
tuple(item.result_slot for item in stage.operations),
tuple(
float(workspace.canonical_values[item.result_slot])
for item in stage.operations
),
)
except MemoryError:
raise
except Exception as exc:
return failed(f"stageObserverFailed:{type(exc).__name__}")
try:
external_finite = all(
isfinite(float(bindings.readers[slot]()))
for slot in program.external_effort_compatibility_slots
)
except MemoryError:
raise
except (ArithmeticError, RuntimeError, TypeError, ValueError) as exc:
return failed(f"externalEffortReadFailed:{type(exc).__name__}")
if not external_finite:
return failed("nonFiniteExternalEffort")
for slot in program.reset_compatibility_slots:
bindings.writers[slot](0.0)
for stage_index, stage in enumerate(program.flow_stages):
width = len(stage.target_slots)
workspace.flow_written[:width] = False
for operation in stage.operations:
try:
evaluated = bindings.evaluators[operation.evaluator_slot]()
if operation.opcode is CausalIROpcode.FLOW_DIRECT:
output = operation.output_indices[0]
workspace.flow_values[output] = float(evaluated)
workspace.flow_written[output] = True
continue
if not hasattr(evaluated, "__len__"):
raise TypeError("component evaluator returned no sequence")
for output, equation in zip(
operation.output_indices, operation.equation_indices
):
if equation >= len(evaluated):
raise IndexError("component equation disappeared")
# Targets are zero before the stage; preserve -residual.
workspace.flow_values[output] = -float(evaluated[equation])
workspace.flow_written[output] = True
except MemoryError:
raise
except (
ArithmeticError,
IndexError,
RuntimeError,
TypeError,
ValueError,
) as exc:
return failed(f"flowEvaluationFailed:{type(exc).__name__}")
if any(not bool(workspace.flow_written[index]) for index in range(width)):
return failed("flowAssignmentCoverageMismatch")
for output, (canonical, compatibility) in enumerate(
zip(stage.target_slots, stage.scatter_compatibility_slots)
):
target = float(workspace.flow_values[output])
if not isfinite(target):
return failed("nonFiniteFlowAssignment")
workspace.canonical_values[canonical] = target
bindings.writers[compatibility](target)
flow_count += 1
completed_flow_stages += 1
if stage_observer is not None:
try:
stage_observer(
"flow",
stage_index,
stage.target_slots,
tuple(float(workspace.flow_values[i]) for i in range(width)),
)
except MemoryError:
raise
except Exception as exc:
return failed(f"stageObserverFailed:{type(exc).__name__}")
return CausalIRExecutionResult(
True,
None,
signature,
effort_count,
flow_count,
completed_effort_stages,
completed_flow_stages,
False,
)
@dataclass(frozen=True, slots=True)
class CausalIRCompilation:
ir: CausalNumericIR | None
fallback_reason: str | None
@property
def supported(self) -> bool:
return self.ir is not None and self.fallback_reason is None
def _unsupported(reason: str) -> CausalIRCompilation:
return CausalIRCompilation(ir=None, fallback_reason=reason)
def _unique_slots(items: Iterable[int]) -> tuple[int, ...]:
return tuple(dict.fromkeys(int(item) for item in items))
def _compile_effort_evaluations(
operations: tuple[CausalIREffortOperation, ...],
anchor_evaluators: tuple[Callable[[], float], ...],
direct_residuals: tuple[bool, ...],
component_locations: dict[
str, tuple[object, Callable[[], tuple[float, ...]], int]
],
evaluators: list[Callable[[], object]],
) -> tuple[CausalIREffortEvaluation, ...]:
grouped: dict[int, list[tuple[int, int, str]]] = {}
component_callbacks: dict[int, Callable[[], tuple[float, ...]]] = {}
direct: list[tuple[int, Callable[[], float], str]] = []
for output, (operation, anchor_evaluate, direct_residual) in enumerate(
zip(operations, anchor_evaluators, direct_residuals)
):
location = (
None
if direct_residual
else component_locations.get(operation.equation_id)
)
if location is None:
direct.append((output, anchor_evaluate, operation.equation_id))
continue
owner, evaluate, equation = location
key = id(owner)
component_callbacks[key] = evaluate
grouped.setdefault(key, []).append((output, equation, operation.equation_id))
compiled: list[CausalIREffortEvaluation] = []
for output, evaluate, equation_id in direct:
evaluator = len(evaluators)
evaluators.append(evaluate)
compiled.append(
CausalIREffortEvaluation(
CausalIROpcode.EFFORT_DIRECT_RESIDUAL,
(output,),
(),
(equation_id,),
evaluator,
)
)
for key, entries in grouped.items():
evaluator = len(evaluators)
evaluators.append(component_callbacks[key])
compiled.append(
CausalIREffortEvaluation(
CausalIROpcode.EFFORT_COMPONENT_RESIDUAL,
tuple(item[0] for item in entries),
tuple(item[1] for item in entries),
tuple(item[2] for item in entries),
evaluator,
)
)
return tuple(compiled)
def compile_causal_numeric_ir(solver: object) -> CausalIRCompilation:
"""Lower a compile-proven global plan; unsupported plans fail closed."""
if not bool(getattr(solver, "_causal_fast_path_eligible", False)):
return _unsupported(
str(
getattr(solver, "_causal_fast_path_fallback_reason", None)
or "causalProofNotAvailable"
)
)
try:
unknowns = tuple(getattr(solver, "unknowns"))
effort_plan = getattr(solver, "_causal_effort_plan_by_variable")
flow_plan = tuple(getattr(solver, "_explicit_flow_plan"))
component_plan = tuple(getattr(solver, "_component_equation_plan"))
reset_unknowns = tuple(
getattr(solver, "_explicit_flow_unknowns_by_variables")[
frozenset(("f", "m_flow"))
]
)
external_unknowns = tuple(
getattr(solver, "_causal_external_effort_unknowns")
)
except (AttributeError, KeyError, TypeError):
return _unsupported("unsupportedCausalSolverContract")
unknown_ids = tuple(str(item.id) for item in unknowns)
if len(set(unknown_ids)) != len(unknown_ids):
return _unsupported("duplicateAlgebraicUnknown")
compatibility_slot_by_id = {
unknown_id: slot for slot, unknown_id in enumerate(unknown_ids)
}
compatibility_slots = tuple(
CausalIRCompatibilitySlot(slot, unknown_id, str(unknown.variable))
for slot, (unknown_id, unknown) in enumerate(zip(unknown_ids, unknowns))
)
readers = tuple(item.read for item in unknowns)
writers = tuple(item.write for item in unknowns)
evaluators: list[Callable[[], object]] = []
canonical_slots: list[CausalIRCanonicalSlot] = []
component_locations: dict[
str, tuple[object, Callable[[], tuple[float, ...]], int]
] = {}
try:
for plan in component_plan:
for equation, template in enumerate(plan.templates):
component_locations[str(template.id)] = (
plan.component,
plan.evaluate,
equation,
)
except (AttributeError, TypeError):
return _unsupported("unsupportedComponentEvaluationContract")
effort_stages: list[CausalIREffortStage] = []
try:
for variable in ("p", "x", "v"):
operations: list[CausalIREffortOperation] = []
anchors: list[Callable[[], float]] = []
direct_residuals: list[bool] = []
for assignment in effort_plan[variable]:
result = len(canonical_slots)
equation_id = str(assignment.anchor.equation_id)
scatter = tuple(
compatibility_slot_by_id[item.id]
for item in assignment.members
)
if not scatter or len(set(scatter)) != len(scatter):
return _unsupported("invalidEffortScatterSlots")
canonical_slots.append(
CausalIRCanonicalSlot(
result,
f"effort:{variable}:{equation_id}",
variable,
"effort_group",
)
)
operations.append(
CausalIREffortOperation(
CausalIROpcode.EFFORT_BROADCAST,
variable,
result,
compatibility_slot_by_id[assignment.anchor.unknown.id],
scatter,
equation_id,
)
)
causal_evaluate = getattr(
assignment.anchor,
"causal_evaluate",
None,
)
anchors.append(
causal_evaluate
if causal_evaluate is not None
else assignment.anchor.evaluate
)
direct_residuals.append(causal_evaluate is not None)
operation_tuple = tuple(operations)
effort_stages.append(
CausalIREffortStage(
variable,
operation_tuple,
_compile_effort_evaluations(
operation_tuple,
tuple(anchors),
tuple(direct_residuals),
component_locations,
evaluators,
),
)
)
except (AttributeError, KeyError, TypeError):
return _unsupported("unsupportedEffortPlanContract")
flow_stages: list[CausalIRFlowStage] = []
try:
for stage in flow_plan:
scatter = tuple(
compatibility_slot_by_id[item.unknown.id]
for item in stage.assignments
)
equation_ids = tuple(str(item.equation_id) for item in stage.assignments)
if len(set(scatter)) != len(scatter):
return _unsupported("duplicateFlowTargetInStage")
targets: list[int] = []
for assignment in stage.assignments:
target = len(canonical_slots)
targets.append(target)
canonical_slots.append(
CausalIRCanonicalSlot(
target,
f"flow:{assignment.unknown.id}",
str(assignment.unknown.variable),
"flow_assignment",
)
)
covered: list[int] = []
operations: list[CausalIRFlowOperation] = []
for output, evaluate in stage.direct_evaluations:
output = int(output)
evaluator = len(evaluators)
evaluators.append(evaluate)
operations.append(
CausalIRFlowOperation(
CausalIROpcode.FLOW_DIRECT,
(output,),
(),
(equation_ids[output],),
evaluator,
)
)
covered.append(output)
for evaluation in stage.component_evaluations:
evaluator = len(evaluators)
evaluators.append(evaluation.evaluate)
outputs = tuple(int(item) for item in evaluation.assignment_indices)
operations.append(
CausalIRFlowOperation(
CausalIROpcode.FLOW_COMPONENT_RESIDUAL,
outputs,
tuple(int(item) for item in evaluation.equation_indices),
tuple(str(item) for item in evaluation.equation_ids),
evaluator,
)
)
covered.extend(outputs)
if sorted(covered) != list(range(len(scatter))):
return _unsupported("flowStageEvaluationCoverageMismatch")
flow_stages.append(
CausalIRFlowStage(
tuple(targets), scatter, equation_ids, tuple(operations)
)
)
except (AttributeError, IndexError, KeyError, TypeError):
return _unsupported("unsupportedFlowPlanContract")
try:
reset_slots = _unique_slots(
compatibility_slot_by_id[item.id] for item in reset_unknowns
)
external_slots = _unique_slots(
compatibility_slot_by_id[item.id] for item in external_unknowns
)
except (AttributeError, KeyError):
return _unsupported("unknownCausalBoundarySlot")
flow_scatter = tuple(
item for stage in flow_stages for item in stage.scatter_compatibility_slots
)
if len(set(flow_scatter)) != len(flow_scatter):
return _unsupported("duplicateExplicitFlowAssignment")
if set(flow_scatter) != set(reset_slots):
return _unsupported("incompleteExplicitFlowCoverage")
program = CausalIRProgram(
CAUSAL_NUMERIC_IR_SCHEMA_VERSION,
tuple(canonical_slots),
compatibility_slots,
reset_slots,
external_slots,
tuple(effort_stages),
tuple(flow_stages),
"",
)
program = replace(
program, structural_signature=program.calculate_structural_signature()
)
return CausalIRCompilation(
CausalNumericIR(
program,
CausalIRBindings(readers, writers, tuple(evaluators)),
),
None,
)
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from __future__ import annotations
from dataclasses import dataclass
from typing import TYPE_CHECKING, Iterable, Sequence
from app.simulation.components.amesim.flow.pipes import (
AmesimPnl0001,
AmesimPnl0002,
AmesimPnl0003,
)
from app.simulation.solvers.mechanical import MechanicalConstraintGroup
from app.simulation.systems.network import Endpoint, SimulationNetwork
if TYPE_CHECKING:
from app.simulation.core.base import DynamicComponent
from app.simulation.solvers.mechanical import MechanicalStateReducer
@dataclass(frozen=True)
class PneumaticStoragePartition:
"""One fixed-volume ``[mass, internal energy]`` pressure-state partition."""
component: DynamicComponent
state_offset: int
volume: float
@property
def key(self) -> tuple[str, int]:
return self.component.name, self.state_offset
@dataclass(frozen=True)
class IdealPneumaticStorageGroup:
partitions: tuple[PneumaticStoragePartition, ...]
@property
def names(self) -> tuple[str, ...]:
return tuple(partition.component.name for partition in self.partitions)
def pneumatic_storage_partition(
network: SimulationNetwork,
endpoint: Endpoint,
) -> PneumaticStoragePartition | None:
"""Map an AMESim pressure-state port to its fixed gas-volume state slice.
PNL0001 exposes its C side at ``port_2``. PNL0003 exposes one compliance
at each end. PNL0002 has resistances at both external ports, so its center
compliance is intentionally not returned here.
"""
component = network.components[endpoint.component]
if isinstance(component, AmesimPnl0003):
if endpoint.port == "port_1":
return PneumaticStoragePartition(
component=component,
state_offset=0,
volume=component.compliance_volume,
)
if endpoint.port == "port_2":
return PneumaticStoragePartition(
component=component,
state_offset=2,
volume=component.compliance_volume,
)
return None
if isinstance(component, AmesimPnl0001) and not isinstance(
component, AmesimPnl0002
):
if endpoint.port == "port_2":
return PneumaticStoragePartition(
component=component,
state_offset=0,
volume=component.volume,
)
return None
def ideal_storage_group_is_reducible(
network: SimulationNetwork,
storage_endpoints: Iterable[Endpoint],
) -> bool:
partitions = [
pneumatic_storage_partition(network, endpoint)
for endpoint in storage_endpoints
]
if not partitions or any(partition is None for partition in partitions):
return False
unique = {partition.key: partition for partition in partitions if partition}
if len(unique) < 2:
return False
media = {id(partition.component.medium) for partition in unique.values()}
return len(media) == 1 and all(partition.volume > 0.0 for partition in unique.values())
def _pressure_storage_endpoint_groups(
network: SimulationNetwork,
) -> tuple[tuple[Endpoint, ...], ...]:
pneumatic_endpoints = {
Endpoint(component.name, definition.name)
for component in network.components.values()
for definition in component.active_port_definitions
if definition.kind == "physical" and definition.domain == "pneumatic"
}
parent = {endpoint: endpoint for endpoint in pneumatic_endpoints}
def find(endpoint: Endpoint) -> Endpoint:
root = endpoint
while parent[root] != root:
root = parent[root]
while parent[endpoint] != endpoint:
next_endpoint = parent[endpoint]
parent[endpoint] = root
endpoint = next_endpoint
return root
def union(first: Endpoint, second: Endpoint) -> None:
first_root = find(first)
second_root = find(second)
if first_root != second_root:
parent[second_root] = first_root
for connection in network.connections:
first, second = connection.endpoints
if first in pneumatic_endpoints and second in pneumatic_endpoints:
union(first, second)
storage_endpoints: set[Endpoint] = set()
for component in network.components.values():
for equation in component.pressure_flow_equation_residuals():
pressure_endpoints = [
Endpoint(component.name, variable.rsplit(".", 2)[1])
for variable in equation.variables
if variable.startswith(f"{component.name}.") and variable.endswith(".p")
]
if equation.relation == "equal":
for endpoint in pressure_endpoints[1:]:
union(pressure_endpoints[0], endpoint)
elif equation.relation == "state":
storage_endpoints.update(pressure_endpoints)
by_root: dict[Endpoint, list[Endpoint]] = {}
for endpoint in storage_endpoints:
by_root.setdefault(find(endpoint), []).append(endpoint)
return tuple(tuple(endpoints) for endpoints in by_root.values())
class IdealPneumaticStorageReducer:
"""Project supported ideal C-C connections onto one thermodynamic state.
AMESim permits compatible pipe compliances to share an ideal pneumatic
junction. The public ODE solver keeps the original result states but
projects their mass and energy densities together and distributes the
group's total derivative by physical volume. This removes the redundant
pressure constraint without adding a fictitious resistance.
"""
def __init__(
self,
network: SimulationNetwork,
mechanical_state_reducer: MechanicalStateReducer,
) -> None:
self.network = network
self.mechanical_state_reducer = mechanical_state_reducer
self.groups = self._build_groups()
self._component_offsets = self._build_component_offsets()
def _build_groups(self) -> tuple[IdealPneumaticStorageGroup, ...]:
groups: list[IdealPneumaticStorageGroup] = []
for endpoints in _pressure_storage_endpoint_groups(self.network):
partitions = [
pneumatic_storage_partition(self.network, endpoint)
for endpoint in endpoints
]
unique = {
partition.key: partition
for partition in partitions
if partition is not None
}
if len(unique) > 1 and len(unique) == len(
{endpoint.component for endpoint in endpoints}
):
group = IdealPneumaticStorageGroup(tuple(unique.values()))
if ideal_storage_group_is_reducible(self.network, endpoints):
groups.append(group)
return tuple(groups)
def _build_component_offsets(self) -> dict[str, int]:
offsets: dict[str, int] = {}
cursor = 0
for entry in self.mechanical_state_reducer.state_entries:
if isinstance(entry, MechanicalConstraintGroup):
cursor += 2
else:
offsets[entry.name] = cursor
cursor += entry.state_size
return offsets
def _global_offset(self, partition: PneumaticStoragePartition) -> int:
return self._component_offsets[partition.component.name] + partition.state_offset
def synchronize_state_vector(
self,
values: Sequence[float],
*,
validate: bool = False,
) -> list[float]:
projected = [float(value) for value in values]
for group in self.groups:
volumes = [partition.volume for partition in group.partitions]
offsets = [self._global_offset(partition) for partition in group.partitions]
mass_densities = [
projected[offset] / volume
for offset, volume in zip(offsets, volumes)
]
energy_densities = [
projected[offset + 1] / volume
for offset, volume in zip(offsets, volumes)
]
if validate:
mass_scale = max([abs(value) for value in mass_densities] + [1.0])
energy_scale = max([abs(value) for value in energy_densities] + [1.0])
if (
max(mass_densities) - min(mass_densities) > 1.0e-9 * mass_scale
or max(energy_densities) - min(energy_densities)
> 1.0e-9 * energy_scale
):
raise ValueError(
"Ideally coupled AMESim pipe compliances require consistent "
"initial pressure and temperature: " + ", ".join(group.names)
)
total_volume = sum(volumes)
mass_density = sum(projected[offset] for offset in offsets) / total_volume
energy_density = (
sum(projected[offset + 1] for offset in offsets) / total_volume
)
for offset, volume in zip(offsets, volumes):
projected[offset] = mass_density * volume
projected[offset + 1] = energy_density * volume
return projected
def coupled_derivatives(self, values: Sequence[float]) -> list[float]:
derivatives = [float(value) for value in values]
for group in self.groups:
volumes = [partition.volume for partition in group.partitions]
offsets = [self._global_offset(partition) for partition in group.partitions]
total_volume = sum(volumes)
total_mass_derivative = sum(derivatives[offset] for offset in offsets)
total_energy_derivative = sum(
derivatives[offset + 1] for offset in offsets
)
for offset, volume in zip(offsets, volumes):
fraction = volume / total_volume
derivatives[offset] = total_mass_derivative * fraction
derivatives[offset + 1] = total_energy_derivative * fraction
return derivatives
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from __future__ import annotations
from dataclasses import dataclass
from math import isfinite
from app.simulation.core.base import Component
from app.simulation.core.ports import PortState
from app.simulation.performance import profile_phase
from app.simulation.systems.network import Endpoint, SimulationNetwork
@dataclass(frozen=True)
class PneumaticVolumeDiagnostics:
propagated: int
output_ports: tuple[str, ...]
def as_dict(self) -> dict[str, object]:
return {
"propagated": self.propagated,
"outputPorts": list(self.output_ports),
}
@dataclass(frozen=True)
class _PneumaticVolumeConnectionBinding:
connected_endpoint: Endpoint
connected_port: PortState
class PneumaticVolumeResolver:
"""Propagate AMESim pneumatic external-volume connector variables."""
def __init__(self, network: SimulationNetwork) -> None:
self.network = network
self._pneumatic_ports = tuple(
component.get_port(definition.name)
for component in network.components.values()
for definition in component.active_port_definitions
if definition.kind == "physical" and definition.domain == "pneumatic"
)
self._output_components = tuple(
component
for component in network.components.values()
if type(component).pneumatic_volume_outputs
is not Component.pneumatic_volume_outputs
)
self._connected_endpoint = self._build_connection_map()
self.last_diagnostics: PneumaticVolumeDiagnostics | None = None
def _build_connection_map(
self,
) -> dict[Endpoint, _PneumaticVolumeConnectionBinding]:
result: dict[Endpoint, _PneumaticVolumeConnectionBinding] = {}
for connection in self.network.connections:
if connection.kind != "physical" or connection.domain != "pneumatic":
continue
first, second = connection.endpoints
result[first] = _PneumaticVolumeConnectionBinding(
connected_endpoint=second,
connected_port=self.network.components[second.component].get_port(
second.port
),
)
result[second] = _PneumaticVolumeConnectionBinding(
connected_endpoint=first,
connected_port=self.network.components[first.component].get_port(
first.port
),
)
return result
@profile_phase("simulation.pneumatic_volume", minimum_mode="audit")
def solve(self) -> PneumaticVolumeDiagnostics:
for port in self._pneumatic_ports:
port.volume = 0.0
port.volume_flow = 0.0
outputs: dict[Endpoint, tuple[float, float]] = {}
for component in self._output_components:
for port_name, raw_values in component.pneumatic_volume_outputs().items():
port = component.get_port(port_name)
definition = port.definition
if (
definition is None
or definition.kind != "physical"
or definition.domain != "pneumatic"
):
raise ValueError(
f"Component {component.name} declares pneumatic volume output "
f"on non-pneumatic port {port_name}."
)
volume, volume_flow = (float(raw_values[0]), float(raw_values[1]))
if not isfinite(volume) or not isfinite(volume_flow):
raise ValueError(
f"Component {component.name}.{port_name} produced a non-finite "
"pneumatic volume value."
)
endpoint = Endpoint(component.name, port_name)
outputs[endpoint] = (volume, volume_flow)
port.volume = volume
port.volume_flow = volume_flow
propagated = 0
for endpoint, values in outputs.items():
binding = self._connected_endpoint.get(endpoint)
if binding is None:
continue
if binding.connected_endpoint in outputs:
raise ValueError(
"A pneumatic connection cannot contain two external-volume "
f"sources: {endpoint} and {binding.connected_endpoint}."
)
binding.connected_port.volume, binding.connected_port.volume_flow = values
propagated += 1
diagnostics = PneumaticVolumeDiagnostics(
propagated=propagated,
output_ports=tuple(sorted(str(endpoint) for endpoint in outputs)),
)
self.last_diagnostics = diagnostics
return diagnostics
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from __future__ import annotations
from dataclasses import dataclass
from math import isfinite
from typing import Callable, Protocol
from app.simulation.core.base import Component
from app.simulation.core.ports import PortState
from app.simulation.performance import profile_phase
from app.simulation.systems.network import Endpoint, SimulationNetwork
class SignalOutputComponent(Protocol):
name: str
def signal_output_values(self, time: float) -> dict[str, float]:
...
class SignalEventSource(Protocol):
"""Optional contract for signal sources with known time discontinuities."""
name: str
def signal_event_times(
self,
start_time: float,
stop_time: float,
) -> tuple[float, ...]:
"""Return event times strictly inside ``(start_time, stop_time)``."""
...
@dataclass(frozen=True)
class SignalSolveDiagnostics:
propagated: int
def as_dict(self) -> dict[str, object]:
return {"propagated": self.propagated}
@dataclass(frozen=True)
class _SignalOutputBinding:
component: Component
evaluate: Callable[[float], dict[str, float]]
@dataclass(frozen=True)
class _SignalConnectionBinding:
source: PortState
target: PortState
class SignalResolver:
"""Propagate scalar signal connections from output ports to input ports."""
def __init__(self, network: SimulationNetwork) -> None:
self.network = network
self._output_bindings = tuple(
_SignalOutputBinding(component=component, evaluate=evaluate)
for component in network.components.values()
if (evaluate := getattr(component, "signal_output_values", None)) is not None
)
self._event_sources = tuple(
(component.name, source_event_times)
for component in network.components.values()
if (
source_event_times := getattr(
component,
"signal_event_times",
None,
)
)
is not None
)
self._connections = tuple(
self._connection_binding(connection.endpoints)
for connection in network.connections
if connection.kind == "signal"
)
self.last_diagnostics: SignalSolveDiagnostics | None = None
@profile_phase("simulation.signal", minimum_mode="audit")
def solve(self, time: float) -> SignalSolveDiagnostics:
for binding in self._output_bindings:
for port_name, value in binding.evaluate(time).items():
binding.component.get_port(port_name).signal = float(value)
propagated = 0
for binding in self._connections:
binding.target.signal = binding.source.signal
propagated += 1
diagnostics = SignalSolveDiagnostics(propagated=propagated)
self.last_diagnostics = diagnostics
return diagnostics
def event_times(self, start_time: float, stop_time: float) -> tuple[float, ...]:
"""Collect optional source events that can be used as integration splits.
Event discovery is deliberately duck typed so existing signal-output
components remain valid without implementing ``signal_event_times``.
"""
start = float(start_time)
stop = float(stop_time)
if not isfinite(start) or not isfinite(stop):
raise ValueError("Signal event interval must be finite.")
if stop < start:
raise ValueError("Signal event interval stop must not precede start.")
if stop == start:
return ()
events: set[float] = set()
for component_name, source_event_times in self._event_sources:
for raw_time in source_event_times(start, stop):
event_time = float(raw_time)
if not isfinite(event_time):
raise ValueError(
f"Signal event time from component '{component_name}' must be finite."
)
if start < event_time < stop:
events.add(event_time)
return tuple(sorted(events))
def _source_target(self, endpoints: tuple[Endpoint, Endpoint]) -> tuple[Endpoint, Endpoint]:
first, second = endpoints
first_port = self.network.components[first.component].get_port(first.port)
second_port = self.network.components[second.component].get_port(second.port)
if first_port.definition is not None and first_port.definition.nominal_role == "output":
return first, second
if second_port.definition is not None and second_port.definition.nominal_role == "output":
return second, first
raise ValueError("Signal connection must contain one output endpoint.")
def _connection_binding(
self,
endpoints: tuple[Endpoint, Endpoint],
) -> _SignalConnectionBinding:
source, target = self._source_target(endpoints)
return _SignalConnectionBinding(
source=self.network.components[source.component].get_port(source.port),
target=self.network.components[target.component].get_port(target.port),
)
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from __future__ import annotations
from dataclasses import dataclass
from app.simulation.core.base import Component, DynamicComponent
from app.simulation.core.ports import PortState
from app.simulation.performance import profile_phase
from app.simulation.systems.network import SimulationNetwork
class StreamSolveError(RuntimeError):
def __init__(self, message: str, diagnostics: "StreamSolveDiagnostics") -> None:
super().__init__(message)
self.diagnostics = diagnostics
@dataclass(frozen=True)
class StreamSolveDiagnostics:
converged: bool
iterations: int
max_delta: float
def as_dict(self) -> dict[str, object]:
return {
"converged": self.converged,
"iterations": self.iterations,
"maxDelta": self.max_delta,
}
@dataclass(frozen=True)
class _StreamConnectionBinding:
component_name: str
port_name: str
connected_component: Component
connected_port: PortState
class StreamResolver:
"""Resolve outflow enthalpy propagation after pressure and flow are known."""
def __init__(
self,
network: SimulationNetwork,
*,
relative_tolerance: float = 1e-9,
max_iterations: int = 100,
) -> None:
self.network = network
self.relative_tolerance = relative_tolerance
self.max_iterations = max_iterations
self._components = tuple(network.components.values())
self._dynamic_components = tuple(
component
for component in self._components
if isinstance(component, DynamicComponent)
)
self._non_dynamic_components = tuple(
component
for component in self._components
if not isinstance(component, DynamicComponent)
)
# State ownership and pressure-flow stream sensitivity are independent
# classifications. Compile this hook by behavior so algebraic
# components such as PNL00R receive their upstream-temperature
# references without dispatching a no-op to every component at runtime.
self._flow_temperature_reference_components = tuple(
component
for component in self._components
if type(component).update_flow_temperature_references
is not Component.update_flow_temperature_references
)
self._ports = tuple(
(component.name, port_name, port)
for component in self._components
for port_name, port in component.ports.items()
)
self._connection_bindings = self._build_connection_bindings()
self.last_diagnostics: StreamSolveDiagnostics | None = None
def _build_connection_bindings(self) -> tuple[_StreamConnectionBinding, ...]:
result: list[_StreamConnectionBinding] = []
for connection in self.network.connections:
if connection.kind != "physical":
continue
first, second = connection.endpoints
first_component = self.network.components[first.component]
second_component = self.network.components[second.component]
result.append(
_StreamConnectionBinding(
component_name=first.component,
port_name=first.port,
connected_component=second_component,
connected_port=second_component.get_port(second.port),
)
)
result.append(
_StreamConnectionBinding(
component_name=second.component,
port_name=second.port,
connected_component=first_component,
connected_port=first_component.get_port(first.port),
)
)
return tuple(result)
def connected_enthalpies(self) -> dict[str, dict[str, float]]:
values: dict[str, dict[str, float]] = {
component.name: {} for component in self._components
}
for binding in self._connection_bindings:
values[binding.component_name][binding.port_name] = (
binding.connected_port.h_outflow
)
return values
def connected_temperature_reference_enthalpies(
self,
) -> dict[str, dict[str, float]]:
"""Return connector references used for upstream temperature only."""
values: dict[str, dict[str, float]] = {
component.name: {} for component in self._components
}
for binding in self._connection_bindings:
values[binding.component_name][binding.port_name] = float(
getattr(
binding.connected_component,
"temperature_reference_h",
binding.connected_port.h_outflow,
)
)
return values
@profile_phase("simulation.refresh", minimum_mode="audit")
def refresh_flow_temperature_references(self) -> None:
"""Refresh pressure-flow property inputs without changing stream outflows."""
connected = self.connected_temperature_reference_enthalpies()
for component in self._flow_temperature_reference_components:
component.update_flow_temperature_references(
connected[component.name]
)
@profile_phase("simulation.refresh", minimum_mode="audit")
def _refresh_dynamic_components(self) -> None:
for component in self._dynamic_components:
component.refresh_thermodynamic_ports()
@profile_phase("simulation.refresh", minimum_mode="audit")
def _refresh_stream_components(
self,
connected: dict[str, dict[str, float]],
) -> None:
for component in self._non_dynamic_components:
component.update_stream_outflows(connected[component.name])
@profile_phase("simulation.stream", minimum_mode="audit")
def solve(
self,
*,
dynamic_ports_are_current: bool = False,
) -> tuple[StreamSolveDiagnostics, dict[str, dict[str, float]]]:
if not dynamic_ports_are_current:
self._refresh_dynamic_components()
max_delta = 0.0
for iteration in range(1, self.max_iterations + 1):
previous = {
(component_name, port_name): port.h_outflow
for component_name, port_name, port in self._ports
}
connected = self.connected_enthalpies()
self._refresh_stream_components(connected)
deltas = [
abs(port.h_outflow - previous[(component_name, port_name)])
for component_name, port_name, port in self._ports
]
magnitudes = [
abs(port.h_outflow)
for _component_name, _port_name, port in self._ports
]
max_delta = max(deltas, default=0.0)
scale = max(magnitudes + [1.0])
if max_delta <= self.relative_tolerance * scale:
diagnostics = StreamSolveDiagnostics(
converged=True,
iterations=iteration,
max_delta=max_delta,
)
self.last_diagnostics = diagnostics
return diagnostics, self.connected_enthalpies()
diagnostics = StreamSolveDiagnostics(
converged=False,
iterations=self.max_iterations,
max_delta=max_delta,
)
self.last_diagnostics = diagnostics
raise StreamSolveError(
"Stream enthalpy propagation did not converge.",
diagnostics,
)
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from __future__ import annotations
from collections.abc import Callable, Sequence
from copy import copy
from dataclasses import dataclass, replace
from app.simulation.core.errors import RecoverableTrialStateError
from app.simulation.core.ports import PortState
_STREAM_CACHE_ATTRIBUTE_NAMES = frozenset(
{
"_connected_h",
"temperature_reference_h",
}
)
def _is_stream_cache_attribute(name: str) -> bool:
"""Return whether an attribute belongs to the stream/temperature replay state.
Catalog components currently use ``_connected_h`` and
``temperature_reference_h``. The name-based extension keeps conservative
third-party caches recoverable without copying an entire component graph.
Components with opaque cache names can provide the explicit hooks documented
by :class:`ThermofluidTransactionPlan`.
"""
lowered = name.lower()
return (
name in _STREAM_CACHE_ATTRIBUTE_NAMES
or lowered.startswith("_stream_")
or "connected_h" in lowered
or "connected_enthalpy" in lowered
or "temperature_reference" in lowered
)
def _copy_cache_value(value: object) -> object:
"""Shallow-copy a stream cache without traversing the component graph."""
if isinstance(value, (dict, list, set, bytearray)):
return copy(value)
return value
@dataclass(frozen=True)
class ThermofluidWorstPort:
component: str
port: str
value: float
signed_delta: float
def as_dict(self) -> dict[str, object]:
return {
"component": self.component,
"port": self.port,
"value": self.value,
"signedDelta": self.signed_delta,
}
@dataclass(frozen=True)
class ThermofluidIterationDelta:
iteration: int
max_delta: float
scale: float
tolerance: float
worst_port: ThermofluidWorstPort | None
def as_dict(self) -> dict[str, object]:
return {
"iteration": self.iteration,
"maxDelta": self.max_delta,
"scale": self.scale,
"tolerance": self.tolerance,
"worstPort": (
self.worst_port.as_dict()
if self.worst_port is not None
else None
),
}
@dataclass(frozen=True)
class ThermofluidClosureSuccess:
rhs_time: float
iterations: int
max_delta: float
scale: float
tolerance: float
worst_port: ThermofluidWorstPort | None
@classmethod
def from_iteration(
cls,
rhs_time: float,
delta: ThermofluidIterationDelta,
) -> ThermofluidClosureSuccess:
return cls(
rhs_time=float(rhs_time),
iterations=delta.iteration,
max_delta=delta.max_delta,
scale=delta.scale,
tolerance=delta.tolerance,
worst_port=delta.worst_port,
)
def as_dict(self) -> dict[str, object]:
return {
"rhsTime": self.rhs_time,
"iterations": self.iterations,
"maxDelta": self.max_delta,
"scale": self.scale,
"tolerance": self.tolerance,
"worstPort": (
self.worst_port.as_dict()
if self.worst_port is not None
else None
),
}
@dataclass(frozen=True)
class ThermofluidClosureFailure:
failed_rhs_time: float
iterations: int
delta_tail: tuple[ThermofluidIterationDelta, ...]
max_delta: float
scale: float
tolerance: float
worst_port: ThermofluidWorstPort | None
failure_count: int = 0
@classmethod
def from_iterations(
cls,
failed_rhs_time: float,
deltas: Sequence[ThermofluidIterationDelta],
*,
tail_limit: int = 8,
) -> ThermofluidClosureFailure:
if not deltas:
raise ValueError("A thermofluid failure requires iteration diagnostics.")
final = deltas[-1]
return cls(
failed_rhs_time=float(failed_rhs_time),
iterations=final.iteration,
delta_tail=tuple(deltas[-tail_limit:]),
max_delta=final.max_delta,
scale=final.scale,
tolerance=final.tolerance,
worst_port=final.worst_port,
)
def as_dict(self) -> dict[str, object]:
return {
"failedRhsTime": self.failed_rhs_time,
"iterations": self.iterations,
"deltaTail": [item.as_dict() for item in self.delta_tail],
"maxDelta": self.max_delta,
"scale": self.scale,
"tolerance": self.tolerance,
"worstPort": (
self.worst_port.as_dict()
if self.worst_port is not None
else None
),
"failureCount": self.failure_count,
}
class ThermofluidClosureError(RecoverableTrialStateError):
"""Recoverable exhaustion of the stream/pressure-flow fixed point.
Stream propagation failures and algebraic-solver failures intentionally
retain their original exception types: rollback is still applied, but a
smaller ODE step is not known to repair those structural/numerical errors.
"""
def __init__(self, diagnostics: ThermofluidClosureFailure) -> None:
super().__init__(
"Stream enthalpy and pressure-flow coupling did not converge "
f"after {diagnostics.iterations} iterations at "
f"t={diagnostics.failed_rhs_time:.17g}."
)
self.diagnostics = diagnostics
class ThermofluidClosureDiagnostics:
"""Run-level RHS outcomes; maintenance/postprocessing calls do not write it."""
def __init__(self) -> None:
self.failure_count = 0
self.last_failure: ThermofluidClosureFailure | None = None
self.last_success: ThermofluidClosureSuccess | None = None
def record_success(self, success: ThermofluidClosureSuccess) -> None:
self.last_success = success
def record_failure(
self,
failure: ThermofluidClosureFailure,
) -> ThermofluidClosureFailure:
self.failure_count += 1
recorded = replace(failure, failure_count=self.failure_count)
self.last_failure = recorded
return recorded
def as_dict(self) -> dict[str, object]:
return {
"failureCount": self.failure_count,
"lastFailure": (
self.last_failure.as_dict()
if self.last_failure is not None
else None
),
"lastSuccess": (
self.last_success.as_dict()
if self.last_success is not None
else None
),
}
@dataclass(frozen=True)
class _PortValueBinding:
component_name: str
port_name: str
state: PortState
variable: str
@dataclass(frozen=True)
class _PortFieldPlan:
variable: str
states: tuple[PortState, ...]
@dataclass(frozen=True)
class _FlowBinding:
component_name: str
port_name: str
state: PortState
@dataclass(frozen=True)
class _ComponentCacheBinding:
component: object
attribute_names: tuple[str, ...]
attribute_name_set: frozenset[str]
snapshot_hook: Callable[[], object] | None
restore_hook: Callable[[object], None] | None
@dataclass
class ThermofluidTransactionSnapshot:
plan: ThermofluidTransactionPlan
port_values: tuple[list[float], ...]
component_cache_values: tuple[list[object], ...]
custom_cache_values: list[object | None]
diagnostic_values: list[object]
def restore(self) -> None:
plan = self.plan
plan._restore_port_values(self.port_values)
for binding, values, custom_value in zip(
plan.component_cache_bindings,
self.component_cache_values,
self.custom_cache_values,
):
component = binding.component
for name in tuple(getattr(component, "__dict__", {})):
if (
name.startswith("_causal_")
or _is_stream_cache_attribute(name)
) and name not in binding.attribute_name_set:
delattr(component, name)
for name, value in zip(binding.attribute_names, values):
setattr(component, name, _copy_cache_value(value))
if binding.restore_hook is not None:
binding.restore_hook(custom_value)
for owner, value in zip(
plan.diagnostic_owners,
self.diagnostic_values,
):
owner.last_diagnostics = value
class ThermofluidTransactionPlan:
"""Compiled, lightweight rollback boundary for one Generic RHS closure.
It snapshots active physical-port values, catalog stream-temperature caches,
component ``_causal_*`` seed fields, and resolver/solver last diagnostics.
A custom stream-aware component with an opaque mutable cache can implement
both ``snapshot_thermofluid_closure_cache()`` and
``restore_thermofluid_closure_cache(snapshot)``; these hooks are invoked in
addition to the standard name-based cache capture.
"""
def __init__(
self,
*,
port_value_bindings: tuple[_PortValueBinding, ...],
port_field_plans: tuple[_PortFieldPlan, ...],
flow_bindings: tuple[_FlowBinding, ...],
component_cache_bindings: tuple[_ComponentCacheBinding, ...],
component_count: int,
diagnostic_owners: tuple[object, ...],
) -> None:
self.port_value_bindings = port_value_bindings
self.port_field_plans = port_field_plans
self.flow_bindings = flow_bindings
self.component_cache_bindings = component_cache_bindings
self.component_count = component_count
self.diagnostic_owners = diagnostic_owners
self._snapshot = ThermofluidTransactionSnapshot(
plan=self,
port_values=tuple(
[0.0] * len(field.states)
for field in port_field_plans
),
component_cache_values=tuple(
[None] * len(binding.attribute_names)
for binding in component_cache_bindings
),
custom_cache_values=[None] * len(component_cache_bindings),
diagnostic_values=[None] * len(diagnostic_owners),
)
@classmethod
def compile(
cls,
network: object,
*,
diagnostic_owners: Sequence[object] = (),
) -> ThermofluidTransactionPlan:
components = tuple(getattr(network, "components").values())
port_value_bindings: list[_PortValueBinding] = []
port_states_by_variable: dict[str, list[PortState]] = {}
flow_bindings: list[_FlowBinding] = []
component_cache_bindings: list[_ComponentCacheBinding] = []
for component in components:
active_definitions = tuple(
definition
for definition in component.active_port_definitions
if definition.kind == "physical"
)
for definition in active_definitions:
state = component.get_port(definition.name)
flow_bindings.append(
_FlowBinding(component.name, definition.name, state)
)
for variable in definition.variables:
port_states_by_variable.setdefault(variable.name, []).append(state)
port_value_bindings.append(
_PortValueBinding(
component.name,
definition.name,
state,
variable.name,
)
)
attribute_names = tuple(
name
for name in getattr(component, "__dict__", {})
if name.startswith("_causal_")
or _is_stream_cache_attribute(name)
)
snapshot_hook = getattr(
component,
"snapshot_thermofluid_closure_cache",
None,
)
restore_hook = getattr(
component,
"restore_thermofluid_closure_cache",
None,
)
hooks_are_available = callable(snapshot_hook) and callable(restore_hook)
if attribute_names or hooks_are_available:
component_cache_bindings.append(
_ComponentCacheBinding(
component=component,
attribute_names=attribute_names,
attribute_name_set=frozenset(attribute_names),
snapshot_hook=(snapshot_hook if hooks_are_available else None),
restore_hook=(restore_hook if hooks_are_available else None),
)
)
owners = tuple(
dict.fromkeys(
owner
for owner in diagnostic_owners
if hasattr(owner, "last_diagnostics")
)
)
return cls(
port_value_bindings=tuple(port_value_bindings),
port_field_plans=tuple(
_PortFieldPlan(variable, tuple(states))
for variable, states in port_states_by_variable.items()
),
flow_bindings=tuple(flow_bindings),
component_cache_bindings=tuple(component_cache_bindings),
component_count=len(components),
diagnostic_owners=owners,
)
def capture(self) -> ThermofluidTransactionSnapshot:
# GenericFluidSystem executes one RHS serially. Reuse one compiled
# workspace rather than allocating a snapshot object and several outer
# tuples at every successful trial point.
snapshot = self._snapshot
self._capture_port_values(snapshot.port_values)
for binding, values in zip(
self.component_cache_bindings,
snapshot.component_cache_values,
):
for position, name in enumerate(binding.attribute_names):
values[position] = _copy_cache_value(
getattr(binding.component, name)
)
for position, binding in enumerate(self.component_cache_bindings):
snapshot.custom_cache_values[position] = (
binding.snapshot_hook()
if binding.snapshot_hook is not None
else None
)
for position, owner in enumerate(self.diagnostic_owners):
snapshot.diagnostic_values[position] = owner.last_diagnostics
return snapshot
def _capture_port_values(
self,
workspaces: tuple[list[float], ...],
) -> None:
for field, values in zip(self.port_field_plans, workspaces):
variable = field.variable
states = field.states
if variable == "p":
for position, state in enumerate(states):
values[position] = state.p
elif variable == "m_flow":
for position, state in enumerate(states):
values[position] = state.m_flow
elif variable == "h_outflow":
for position, state in enumerate(states):
values[position] = state.h_outflow
elif variable == "volume":
for position, state in enumerate(states):
values[position] = state.volume
elif variable == "volume_flow":
for position, state in enumerate(states):
values[position] = state.volume_flow
elif variable == "x":
for position, state in enumerate(states):
values[position] = state.x
elif variable == "v":
for position, state in enumerate(states):
values[position] = state.v
elif variable == "f":
for position, state in enumerate(states):
values[position] = state.f
else:
for position, state in enumerate(states):
values[position] = getattr(state, variable)
def _restore_port_values(
self,
workspaces: tuple[list[float], ...],
) -> None:
for field, values in zip(self.port_field_plans, workspaces):
variable = field.variable
states = field.states
if variable == "p":
for state, value in zip(states, values):
state.p = value
elif variable == "m_flow":
for state, value in zip(states, values):
state.m_flow = value
elif variable == "h_outflow":
for state, value in zip(states, values):
state.h_outflow = value
elif variable == "volume":
for state, value in zip(states, values):
state.volume = value
elif variable == "volume_flow":
for state, value in zip(states, values):
state.volume_flow = value
elif variable == "x":
for state, value in zip(states, values):
state.x = value
elif variable == "v":
for state, value in zip(states, values):
state.v = value
elif variable == "f":
for state, value in zip(states, values):
state.f = value
else:
for state, value in zip(states, values):
setattr(state, variable, value)
def flow_values(self) -> tuple[float, ...]:
return tuple(float(binding.state.m_flow) for binding in self.flow_bindings)
def measure_flow_delta(
self,
previous: Sequence[float],
*,
iteration: int,
relative_tolerance: float,
) -> ThermofluidIterationDelta:
current = self.flow_values()
scale = max(
(abs(value) for value in (*previous, *current)),
default=1.0,
)
scale = max(scale, 1.0)
worst_index = -1
worst_signed_delta = 0.0
max_delta = 0.0
for index, (old, new) in enumerate(zip(previous, current)):
signed_delta = new - old
magnitude = abs(signed_delta)
if magnitude > max_delta:
worst_index = index
worst_signed_delta = signed_delta
max_delta = magnitude
worst_port = None
if worst_index >= 0:
binding = self.flow_bindings[worst_index]
worst_port = ThermofluidWorstPort(
component=binding.component_name,
port=binding.port_name,
value=current[worst_index],
signed_delta=worst_signed_delta,
)
return ThermofluidIterationDelta(
iteration=int(iteration),
max_delta=max_delta,
scale=scale,
tolerance=float(relative_tolerance) * scale,
worst_port=worst_port,
)
def diagnostics(self) -> dict[str, int]:
stream_cache_slot_count = sum(
len(binding.attribute_names)
for binding in self.component_cache_bindings
)
return {
"physicalPortValueSlotCount": len(self.port_value_bindings),
"physicalFlowPortCount": len(self.flow_bindings),
"componentCount": self.component_count,
"cacheBindingCount": len(self.component_cache_bindings),
"streamAndCausalCacheSlotCount": stream_cache_slot_count,
"customCacheHookCount": sum(
binding.snapshot_hook is not None
for binding in self.component_cache_bindings
),
"diagnosticOwnerCount": len(self.diagnostic_owners),
}
File diff suppressed because it is too large. Load diff
+12 -62
View File
@@ -3,7 +3,7 @@ from __future__ import annotations
from dataclasses import dataclass
from app.simulation.core.base import Component, DynamicComponent
from app.simulation.core.equations import EquationResidual
from app.simulation.core.equations import EquationDefinition
from app.simulation.core.metadata import ResultVariableMetadata
from app.simulation.core.ports import PortState
@@ -182,62 +182,25 @@ class SimulationNetwork:
)
return component.get_port(endpoint.port)
def connection_equation_residuals(self) -> tuple[EquationResidual, ...]:
"""Evaluate connector equations that have a direct scalar residual.
Stream variables are resolved by the stream-mixing layer and therefore do
not incorrectly appear here as an equality between outflow properties.
"""
residuals: list[EquationResidual] = []
def connection_equation_definitions(self) -> tuple[EquationDefinition, ...]:
equations=[]
for connection in self.connections:
if connection.kind != "physical":
continue
first_port = self._port_for(connection.endpoint_a)
second_port = self._port_for(connection.endpoint_b)
definition = first_port.definition
if definition is None:
raise ValueError(
f"Connected port {connection.endpoint_a} has no interface definition."
)
if connection.kind!='physical':continue
definition=self._port_for(connection.endpoint_a).definition
for variable in definition.variables:
if variable.connection_rule == "equal":
value = float(getattr(first_port, variable.name)) - float(
getattr(second_port, variable.name)
)
elif variable.connection_rule == "sumToZero":
value = float(getattr(first_port, variable.name)) + float(
getattr(second_port, variable.name)
)
else:
continue
residuals.append(
EquationResidual(
id=f"{connection.id}:{variable.name}",
owner="connection",
owner_id=connection.id,
relation=variable.connection_rule,
variables=(
f"{connection.endpoint_a}.{variable.name}",
f"{connection.endpoint_b}.{variable.name}",
),
role=variable.role,
value=value,
)
)
return tuple(residuals)
if variable.connection_rule not in ('equal','sumToZero'):continue
equations.append(EquationDefinition(id=f'{connection.id}:{variable.name}',owner='connection',owner_id=connection.id,relation=variable.connection_rule,variables=(f'{connection.endpoint_a}.{variable.name}',f'{connection.endpoint_b}.{variable.name}'),role=variable.role))
return tuple(equations)
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
def equation_definitions(self) -> tuple[EquationDefinition, ...]:
"""Evaluate the complete algebraic pressure-flow equation subsystem."""
component_residuals = tuple(
residual
for component in self.components.values()
for residual in component.pressure_flow_equation_residuals()
for residual in component.equation_definitions()
)
return component_residuals + self.connection_equation_residuals()
return component_residuals + self.connection_equation_definitions()
def pressure_flow_unknowns(self) -> tuple[str, ...]:
return tuple(
@@ -251,7 +214,7 @@ class SimulationNetwork:
def pressure_flow_structure_dict(self) -> dict[str, object]:
unknowns = self.pressure_flow_unknowns()
equations = self.pressure_flow_equation_residuals()
equations = self.equation_definitions()
return {
"unknownCount": len(unknowns),
"equationCount": len(equations),
@@ -269,20 +232,7 @@ class SimulationNetwork:
if isinstance(component, DynamicComponent)
]
def initial_state_vector(self) -> list[float]:
values: list[float] = []
for component in self.dynamic_components():
values.extend(component.get_state_vector())
return values
def apply_state_vector(self, values: list[float]) -> None:
cursor = 0
for component in self.dynamic_components():
next_cursor = cursor + component.state_size
component.set_state_vector(values[cursor:next_cursor])
cursor = next_cursor
if cursor != len(values):
raise ValueError("State vector length does not match dynamic components.")
def result_variable_metadata(self) -> tuple[ResultVariableMetadata, ...]:
return tuple(
+15 -59
View File
@@ -39,68 +39,19 @@ def simulation_warmup_enabled() -> bool:
)
def _run_numerical_warmup() -> None:
"""Exercise only in-memory SciPy paths used by real simulations."""
import numpy as np
from scipy.integrate import BDF, DOP853, LSODA, RK23, RK45, Radau, solve_ivp
from scipy.optimize import brentq, least_squares
from scipy.optimize._numdiff import group_columns
from scipy.sparse import csc_matrix, csr_matrix
# Importing these classes is intentional even though the micro solve below
# uses BDF: the stepwise solver selects them dynamically at runtime.
solver_types = (BDF, DOP853, LSODA, RK23, RK45, Radau)
if len(solver_types) != 6:
raise RuntimeError("SciPy solver warm-up did not load every supported method.")
def _run_native_warmup() -> None:
"""Check the native toolchain and XML schema without running SciPy solvers.
sparsity = csc_matrix(np.array([[1.0]], dtype=float))
groups = group_columns(sparsity)
if groups.shape != (1,):
raise RuntimeError("SciPy Jacobian grouping warm-up returned an invalid shape.")
integration = solve_ivp(
lambda _time, state: -state,
(0.0, 1.0e-4),
np.array([1.0], dtype=float),
method="BDF",
t_eval=np.array([0.0, 1.0e-4], dtype=float),
jac_sparsity=sparsity,
rtol=1.0e-6,
atol=1.0e-9,
)
if not integration.success or not np.isfinite(integration.y).all():
raise RuntimeError("SciPy integration warm-up did not complete successfully.")
algebraic_sparsity = csr_matrix(np.eye(2, dtype=bool))
algebraic = least_squares(
lambda state: np.array(
[state[0] - 1.0, state[1] - 2.0],
dtype=float,
),
np.array([0.5, 0.5], dtype=float),
bounds=(
np.array([0.0, 0.0], dtype=float),
np.array([3.0, 3.0], dtype=float),
),
jac_sparsity=algebraic_sparsity,
tr_solver="lsmr",
)
if (
not algebraic.success
or not np.isfinite(algebraic.x).all()
or not np.allclose(algebraic.x, np.array([1.0, 2.0]), atol=1.0e-8)
):
raise RuntimeError("SciPy algebraic warm-up did not complete successfully.")
root = brentq(lambda value: value - 0.5, 0.0, 1.0)
if abs(root - 0.5) > 1.0e-12:
raise RuntimeError("SciPy scalar root warm-up returned an invalid result.")
# Compile the cached v3 XSD through the same public validation path. The
# intentionally incomplete document is never accepted or persisted.
The model-specific executable is generated when a model is submitted.
"""
from app.simulation.native_codegen.build import toolchain
from app.system_xml import validate_system_xml_document
if os.name != "nt":
raise RuntimeError("Native v1 currently supports Windows x64 build packaging only.")
toolchain()
validate_system_xml_document(b"<System/>")
@@ -114,6 +65,10 @@ def warm_up_simulation_runtime() -> SimulationWarmupReport:
global _WARMUP_REPORT
from app.simulation.backends import numeric_engine_name
engine = numeric_engine_name()
with _WARMUP_LOCK:
if _WARMUP_REPORT is not None:
return _WARMUP_REPORT
@@ -126,7 +81,7 @@ def warm_up_simulation_runtime() -> SimulationWarmupReport:
started = perf_counter()
try:
_run_numerical_warmup()
_run_native_warmup()
except MemoryError:
raise
except Exception as exc:
@@ -142,7 +97,8 @@ def warm_up_simulation_runtime() -> SimulationWarmupReport:
duration_ms=(perf_counter() - started) * 1000.0,
)
LOGGER.info(
"Simulation runtime warm-up completed in %.1f ms.",
"Simulation runtime warm-up (%s) completed in %.1f ms.",
engine,
_WARMUP_REPORT.duration_ms,
)
return _WARMUP_REPORT