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固定翼性能快算方案：巡航配平、所需推力、爬升率等一级性能校核。当需要对总体方案做快速性能余度检查时调用。
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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_performance_spec |
| description | 固定翼性能快算方案：巡航配平、所需推力、爬升率等一级性能校核。当需要对总体方案做快速性能余度检查时调用。 |
| stage | class2_preliminary |
| code_module | aircraft_design/class2_preliminary/performance.py |
| dependencies | ["fixed_wing_overall_sizing_runbook"] |
fixed_wing_overall_sizing_runbook 统一调用，典型字段来源：
requirements.cruise_altitude_m、requirements.cruise_machinitial_guess.cd0、initial_guess.oswald_e、initial_guess.aspect_ratioinitial_guess.thrust_to_weight、initial_guess.wing_loading_paoutputs.mtow_kg、outputs.wing_area_m2CD0 与诱导阻力项cruise_required_thrust_nclimb_rate_m_s