vault backup: 2025-03-10 16:27:57

.obsidian/plugins/copilot/data.json

@@ -43,24 +43,30 @@
       "provider": "openai",
       "enabled": true,
       "isBuiltIn": true,
-      "core": true
+      "core": true,
+      "baseUrl": "",
+      "apiKey": ""
     },
     {
       "name": "gpt-4o-mini",
       "provider": "openai",
       "enabled": true,
       "isBuiltIn": true,
-      "core": true
+      "core": true,
+      "baseUrl": "",
+      "apiKey": ""
     },
     {
       "name": "claude-3-5-sonnet-latest",
       "provider": "anthropic",
       "enabled": true,
       "isBuiltIn": true,
-      "core": true
+      "core": true,
+      "baseUrl": "",
+      "apiKey": ""
     },
     {
-      "name": "phi4:latest",
+      "name": "llama3.2:latest",
       "provider": "ollama",
       "baseUrl": "https://possibly-engaged-filly.ngrok-free.app",
       "apiKey": "",
@@ -70,9 +76,9 @@
       "isEmbeddingModel": false
     },
     {
-      "name": "llama3.2:latest",
+      "name": "phi4:latest",
       "provider": "ollama",
-      "baseUrl": "https://possibly-engaged-filly.ngrok-free.app",
+      "baseUrl": "http://localhost:11434",
       "apiKey": "",
       "enabled": true,
       "isBuiltIn": false,

多体+耦合求解器/steady power curve Operational loads 控制.md

@@ -0,0 +1,30 @@
+
+## Theory manual
+![[Pasted image 20250310105322.png]]Once `Demanded Generator Torque` is reached at point D, the torque demand is kept constant for all higher wind speeds. Once the `Demanded Generator Speed` is reached the pitch control regulates the rotor speed. This is know as the full load regime. A small (optional) margin is allowed between points D (where the torque reaches maximum) and E (where pitch control begins) to prevent excessive mode switching between below and above rated control modes. However, this margin may not be required, in which case points D and E coincide. The line CD may collapse to a point if also desired.
+
+In the full load regime, the blade pitch is adjusted to maintain the chosen operating point, designated E. Effectively, changing the pitch alters the lines of constant wind speed, forcing them to pass through the desired operating point.
+
+```
+```
+**The pitch angle is limited to the `Minimum pitch angle` the lower limit of pitch or aileron deployment angle. The `Maximum pitch angle` that is the upper limit of pitch or aileron deployment angle. There is also an option to [schedule pitch angle against hub wind speed](https://dnvgldocs.azureedge.net/BladedManual/4_17/modelling/controlSystems/ControlStrategy/VariableSpeedPitchReg.html#minimum-pitch-angle-scheduling-for-initial-conditions) during the initial condition calculation.**
+
+The user can select between `Pitch feathering` or `Assisted stall` to specify the direction of pitching. **If pitch feathering is selected, the Minimum pitch angle will be set for normal operation below rated wind speed, and the pitch (or aileron) angle will increase above rated.** If `Assisted Stall` is selected, the maximum pitch setting is used below rated, and the pitch (or aileron) angle decreases (or moves to more negative values) above rated.
+
+
+The feature allows the user to **easily specify pitch angles below rated wind speed for initial conditions.** This is useful for model linearisation calculations. **For above rated wind speeds, the initial condition algorithm finds a pitch angle that maintains maximum rotor speed.** However, the minimum pitch angle set by the pitch scheduling routine is still used as the minimum angle even though a smaller angle might be needed to maintain the maximum rotor speed. Furthermore, it provides a convenient method for matching the behaviours in the initial condition algorithm and a time domain pitch scheduling routine implemented in a [User-Defined Controller](https://dnvgldocs.azureedge.net/BladedManual/4_17/modelling/controlSystems/Controller/UserDefinedControllers.html). Note that this feature only supports VSPR control strategies, and does not support the “Assisted Stall” type controller. In addition, this option only applies when the turbine is in power production mode.
+
+The user can specify hub wind speeds and minimum pitch angles in a lookup table. During the initial condition calculation, a linear interpolation of the data points is utilized to calculate the minimum pitch angle for the current hub wind speed (both above and below rated wind speed conditions). The points in the lookup table must be in a monotonic ascending order and if the current hub wind speed is out of range of the specified lookup table the nearest value will be used.
+
+## user manual
+
+The **steady state parameters** define the operating envelope of the turbine, and are **required for calculation of the steady power curve and steady operational loads.** Click on Controller Dynamics to define additional parameters which model the dynamic action of the controller, such as controller gains and transducer and actuator time constants.
+
+![[Pasted image 20250310144609.png]]
+
+Steady state parameters
+- Demanded electrical power: the power set-point, i.e. the electrical power output required above rated wind speed.
+- Minimum pitch angle: the lower limit of pitch or aileron deployment angle.
+- Maximum pitch angle: the upper limit of pitch or aileron deployment angle.
+- Select Pitch feathering or Assisted stall: to specify the direction of pitching. If Pitch Feathering is selected, the Minimum pitch angle will be set for normal operation below rated wind speed, and the pitch (or aileron) angle will increase above rated. If Assisted Stall is selected, the Maximum pitch setting is used below rated, and the pitch (or aileron) angle decreases (or moves to more negative values) above rated.
+
+![[Pasted image 20250310162659.png]]

工作OKRs/25.2-5 OKR.canvas

@@ -1,7 +1,7 @@
 {
 	"nodes":[
 		{"id":"b698e88ca5fb9c51","type":"text","text":"状态指标：\n推进OKR的时候也要关注这些事情，它们是完成OKR的保障。\n\n\n效率状态  green","x":-96,"y":80,"width":456,"height":347},
-		{"id":"58be7961ae7275a7","type":"text","text":"# 计划\n这周要做的3~5件重要的事情，这些事情能有效推进实现OKR。\n\nP1 必须做。P2 应该做\n\nP1 多体原理学习 YouTube课程 ing\nP1 公共模块整理与探讨 已有初步方案 \nP1 气动模块联合调试，跑通 no\nP1 梳理Steady Operational Load计算条件，方法及输出结果，确定技术路线 70%\nP1 专利答通一稿 done\n","x":-620,"y":-307,"width":450,"height":347},
+		{"id":"58be7961ae7275a7","type":"text","text":"# 计划\n这周要做的3~5件重要的事情，这些事情能有效推进实现OKR。\n\nP1 必须做。P2 应该做\n\nP1 多体原理学习 YouTube课程 ing\nP1 根据公共mesh模块调整代码\nP1 气动模块联合调试，跑通 no\nP1 梳理Steady Operational Load计算条件，方法及输出结果，确定变桨角度技术路线\n\n","x":-620,"y":-307,"width":450,"height":347},
 		{"id":"2b068bfe5df15a72","type":"text","text":"# 目标：多体动力学模块完善\n### 每周盘点一下它们\n\n\n关键结果：建模原理、建模方法掌握    （6.5/10）\n\n关键结果：对标Bladed模块完成  （6.5/10）\n\n关键结果：风机多体动力学文献调研情况完成 （5/10）","x":-96,"y":-307,"width":456,"height":347},
 		{"id":"01ee5c157d0deeae","type":"text","text":"# 推进计划\n未来四周计划推进的重要事情\n\n文献调研启动\n\n建模重新推导\n\n\n","x":-620,"y":80,"width":456,"height":347}
 	],