Menu
执行固定翼 Class I 重量闭合（W0/We/Wf）并输出收敛信息。当总体闭环需要重量结果或燃油/空重异常时调用。
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-weights-runbookThe command stays on one line. Scroll horizontally to inspect it before copying.
Prefer a local copy? Download the files currently available to SkillsMP.
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。
Showing SKILL.md
| name | fixed_wing_weights_runbook |
| description | 执行固定翼 Class I 重量闭合（W0/We/Wf）并输出收敛信息。当总体闭环需要重量结果或燃油/空重异常时调用。 |
| stage | class1_conceptual |
| code_module | aircraft_design/class1_conceptual/weights_class1.py |
| dependencies | ["fixed_wing_weights_spec"] |
fixed_wing_overall_sizing_runbook 闭环驱动，不建议作为独立入口。fixed_wing_overall_sizing_runbook（内部完成重量闭合）requirements.range_m、巡航点（Mach/高度）initial_guess.sfc_cruise_1_s（以及推进类型假设）initial_guess.cd0、initial_guess.oswald_e、initial_guess.aspect_ratiorun_sizing 闭环中为内置假设（后续可扩展为显式参数）output/<project>_*/design_data.json。outputs.mtow_kg / empty_weight_kg / fuel_weight_kg 与迭代历史（若有）。L/D（cd0/e/AR）→ 任务指标是否过激。完成重量闭合后，调用 aircraft_design/weight_balance.py 进行重心包线分析：
from aircraft_design.weight_balance import WeightBalanceAnalyzer
# ... 实例化 analyzer ...
envelope = analyzer.analyze()