A fresh method on the condition of hypersonic speed, based on disturbance observer and dynamic inversioncontrol is introduced in this paper in order to solve the stability of flight control system.

• 文中介绍了在高超音速条件下,基于干扰观测器和非线性动态逆控制的方法,对飞行器姿态控制系统的稳定性的研究。