This paper discussed the application of this method in the design of flight control system for the post stall maneuver.
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。
2
In this paper, the method of reentry maneuver guidance applying to attack the ground fixed target is described by using flight dynamics principle and modern control theory.
本文运用飞行力学原理和现代控制理论，对攻击地面固定目标的飞行器的再入机动制导方法进行了研究。
3
It will give a reference to technicians and flight crew engaging in flight test research of post tall and tactical maneuver.