用该方法解决飞机总体参数优化问题。
These methods are applied to optimizing the overall parameters of an aircraft.
该模型包含了起落架系统特性和全机气动力特性，根据飞机总体设计参数可仿真给出其起飞性能指标。
On the basis of the vehicle oriented parameters and the aerodynamic characteristics, the history of takeoff is emulated. Simulation studies show that the model is useful in the aircraft design.
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