使用在线参数辨识方法，对飞机的气动特性进行估计并用于舵面分配。
The aerodynamic parameters wear estimated through online parameter identification method and were used for actuator deflect allocation.
用数值优化方法取得自适应翼型最优的舵面偏角，并计算其气动特性。
An optimization method is used to obtain deflection Angle of control surface and the aerodynamic efficiency of airfoil is calculated.
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