从前期高超声速飞行器基础理论以及关键技术的研究到现今的飞行试验可以看出,高超声速飞行器在总体设计阶段过晚考虑飞行器动力学特性和控制性能会给后期控制系统设计带来极大的困难。在对两类高超声速飞行器试飞与控制相关问题分析的基础上,提出了面向控制的高超声速飞行器总体优化设计方法,给出了面向控制的总体优化设计研究方法、思路和模块框架。 From the previous research on the basic theory and key technologies of hypersonic vehicles to the current flight tests, it can be seen that the hypersonic vehicle too late considering the aircraft dynamics and control performance in the overall design phase will bring great difficulties to the design of the post-control system . Based on the analysis of flight control and flight-related problems of two types of hypersonic vehicles, a total control-oriented optimization design method of hypersonic vehicle is proposed. The control-oriented overall optimization design research method, train of thought and module framework are given.