Menu
定义固定翼机载系统详细配置（重量/位置/技术因子）。当用户需要指定具体系统参数或覆盖重量估算默认值时调用。
The review-first prompt is selected by default. You can switch to a direct command or download a local copy.
Read SKILL.md and any companion files shown by SkillsMP before deciding whether to install.
Install with Codex or Claude Copy this prompt, paste it into Codex, Claude, or another assistant, and let it review the skill page and install it for you.
A direct command skips the review prompt. Inspect the source before running it.
npx skills add https://github.com/BaiSongt/aircraft-design-skill --skill fixed-wing-systems-specThe command stays on one line. Scroll horizontally to inspect it before copying.
Prefer a local copy? Download the files currently available to SkillsMP.
Showing SKILL.md
Based on SOC occupation classification
执行包含高级分析与机身几何的固定翼总体设计流程。初步分析收敛后调用，含高级分析、几何约束与机身外形。
固定翼总体设计唯一入口：执行 Class I 闭环并在收敛后进入阶段 2–7 扩展分析，落盘输出报告/数据/外形资产，并可选 PySide6 实时可视化。
生成固定翼总体设计方案（需求→约束→设计点→初步尺寸→重量/性能闭合）。当需要给出固定翼总体方案、关键参数范围与决策依据时调用。
| name | fixed_wing_systems_spec |
| description | 定义固定翼机载系统详细配置（重量/位置/技术因子）。当用户需要指定具体系统参数或覆盖重量估算默认值时调用。 |
| stage | cross_stage |
| code_module | aircraft_design/class2_preliminary/weights_system.py |
| dependencies | ["fixed_wing_weights_spec"] |
本 Spec 定义统一输入 JSON 中 systems 字段的配置方式，用于在总体收敛后生成更细粒度的系统重量与（可选）重心信息。
fixed_wing_overall_sizing_runbook（python -m aircraft_design.run_sizing）output/<project>_*/design_data.json.outputs.systems系统配置作为 systems 字段存在于总体输入 JSON 中。
{
"systems": {
"landing_gear": {
"type": "retractable",
"weight_fraction_override": 0.05,
"main_gear_location_x_m": 4.5,
"nose_gear_location_x_m": 0.8
},
"avionics": {
"weight_kg": 120.0,
"location_x_m": 1.5,
"power_w": 500.0
},
"flight_controls": {
"type": "mechanical",
"tech_factor": 0.9
},
"furnishings": {
"weight_kg": 80.0
},
"environmental_control": {
"present": true,
"weight_kg": 30.0
},
"anti_ice": {
"present": false
}
}
}
systems 用于覆盖或修正系统重量估算的默认假设（例如航电重量、起落架构型等）。