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执行固定翼结构/载荷一级估算并提供结构重量回馈建议。当总体迭代需要结构可行性校核或结构重量修正时调用。
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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_structures_loads_runbook |
| description | 执行固定翼结构/载荷一级估算并提供结构重量回馈建议。当总体迭代需要结构可行性校核或结构重量修正时调用。 |
| stage | class2_preliminary |
| code_module | aircraft_design/class3_detailed/structures_loads.py, aircraft_design/class3_detailed/loads_analysis.py |
| dependencies | ["fixed_wing_structures_loads_spec"] |
fixed_wing_overall_sizing_runbook 的扩展阶段驱动。S, b, cbar，机翼/机身布置参数w0_kg 与重量分布假设n_limit、突风等级与关键工况