研究了高超声速飞行器的姿态运动间的强耦合问题并设计了姿态协调控制器,首先基于状态变量间耦合度推导了耦合熵,再基于耦合分析设计了协调因子,其中将状态变量间的耦合熵作为协调因子的参数,然后引入协调因子设计了姿态控制器。仿真结果表明,所设计的协调控制器可有效应对高超声速飞行器姿态运动间的强耦合问题,在保证姿态稳定的前提下,实现了姿态角之间的协调控制。 The strong coupling problem of hypersonic vehicles is studied and the attitude coordination controller is designed. Firstly, the coupling entropy is deduced based on the coupling degree of the state variables, then the coordination factor is designed based on the coupling analysis. The coupling entropy As a coordination factor of the parameters, and then the introduction of coordination factor design attitude controller. The simulation results show that the designed controller can effectively deal with the strong coupling problem of the hypersonic aircraft attitude and attitude, and achieve the coordinated control of the attitude angles under the premise of ensuring the attitude stability.