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规划固定翼阶段2-7功能分解、接口字段与验收标准。当需要扩展阻力分解/推进模型/任务剖面/稳定结构/迭代优化时调用。
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| name | fixed_wing_stage2_7_plan |
| description | 规划固定翼阶段2-7功能分解、接口字段与验收标准。当需要扩展阻力分解/推进模型/任务剖面/稳定结构/迭代优化时调用。 |
| stage | cross_stage |
| code_module | aircraft_design/class2_preliminary/advanced_design.py |
| dependencies | ["fixed_wing_overall_sizing_runbook","fixed_wing_aero_buildup_runbook","fixed_wing_propulsion_runbook","fixed_wing_performance_runbook","fixed_wing_stability_control_runbook","fixed_wing_structures_loads_runbook"] |
fixed_wing_overall_sizing_runbook 在“Class I 收敛且结果合理”后自动触发（aircraft_design.run_sizing 内部调用扩展阶段）。output/<project>_*/advanced_design_results_*.json 与 advanced_design_report.md。cd0 与可追溯分解stage2_aero.cd0、stage2_aero.cd0_breakdown 与分解表cd0 来源，且随几何变化趋势合理T_avail(h,V) 或 P_avail(h,V) 的一级模型stage3_propulsion.thrust_available_* 与余度stage4_mission.mission_breakdownstage5_stability.static_margin、stage5_stability.trim_tail_clstage6_structures.*（载荷量级、结构重量回馈）stage7_optimization 与候选集（如启用优化）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。