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执行固定翼约束校核并给出设计点调整建议。当用户关心起降/失速/巡航/爬升约束是否满足或要定位卡点时调用。
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npx skills add https://github.com/BaiSongt/aircraft-design-skill --skill fixed-wing-constraints-runbookThe command stays on one line. Scroll horizontally to inspect it before copying.
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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。
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| name | fixed_wing_constraints_runbook |
| description | 执行固定翼约束校核并给出设计点调整建议。当用户关心起降/失速/巡航/爬升约束是否满足或要定位卡点时调用。 |
| stage | class1_conceptual |
| code_module | aircraft_design/class2_preliminary/constraints.py |
| dependencies | ["fixed_wing_constraints_spec"] |
fixed_wing_overall_sizing_runbook 驱动：约束用于修正/验证设计点（W/S、T/W）。output/<project>_*/design_report_v2.md：可读的约束/设计点总结（若对应章节已输出）output/<project>_*/design_data.json：设计点与迭代信息（inputs.initial_guess、outputs）stall_ws 裕度不足：降低 wing_loading_pa 或提高 cl_maxcruise 余度不足：降低 cd0、提高 e/AR 或提高推重比climb_gradient 余度不足：提高推重比或降低重量/阻力takeoff_distance 裕度不足：提高推重比或提高起飞构型 CLmaxlanding_distance 裕度不足：提高着陆构型 CLmax 或放宽着陆距离除了性能约束外，还应校核几何约束。调用 aircraft_design/geometry_constraints.py 进行检查：
from aircraft_design.geometry_constraints import GeometryConstraintChecker
# ... 实例化 checker ...
results = checker.check_all()