讨论了应用非线性动态逆进行超机动飞机飞行控制系统的设计。对快变量角速率进行非线性逆控制器的设计，由此来稳定纵向短周期运动，并通过气动舵面与推力矢量的融合，来改善大迎角范围的侧向响应，对慢变量姿态角进行非线性逆控制器的设计可使飞行员控制飞机慢运动。 The design of the flight control system of the ultra-mobile aircraft using nonlinear dynamic inverse is discussed. A nonlinear inverse controller is designed for fast variable angular rate to stabilize the longitudinal short-period motion and to improve the lateral response at high angle-of-attack range through the fusion of the aerodynamic rudder surface and the thrust vector. For the slow-variable attitude angle The design of the nonlinear inverse controller allows the pilot to control the airplane’s slow motion.