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非线性动态逆为非线性系统控制律的设计提供了一种重要手段。针对过失速机动飞机探讨了非线性动态逆方法在飞行控制系统设计中的应用。根据非线性动态逆的特点将飞机的动态特性分为快慢不同的状态变量。对快变量应用非线性动态逆进行控制律设计是将飞机气动控制面和推力矢量控制作为输入；慢状态变量控制律的设计是利用快状态变量作为输入。并采用伪逆的优化计算方法对各控制面的操纵权限分配进行了探讨。“Cobra”和“Herbst”两个过失速机动的实现证明该设计方法和仿真方法是成功的。
Nonlinear dynamic inverse provides an important means for the design of nonlinear system control law. The application of nonlinear dynamic inverse method in the design of flight control system is discussed in the paper. According to the characteristics of nonlinear dynamic inverse, the dynamic characteristics of the aircraft are divided into different state variables of different speeds. The control law design of fast dynamic variable with nonlinear dynamic response takes plane aerodynamic control plane and thrust vector control as input. Slow state variable control law is designed by using fast state variable as input. In addition, the optimal computing method of pseudo-inverse is used to discuss the distribution of control rights of all control surfaces. The implementation of two stalling motions, “Cobra” and “Herbst”, proves that the design method and the simulation method are successful.