Reentry Attitude Tracking Control for Hypersonic Vehicle with Reaction Control Systems via Improved Model Predictive Control Approach

作     者：Kai Liu Zheng Hou Zhiyong She Jian Guo 无 

作者机构：School of Aeronautics and AstronauticsDalian University of TechnologyDalian116024China Key Laboratory of Advanced Technology for Aerospace VehiclesDalian116024China Beijing Institute of Aerospace TechnologyBeijing100074China 

出 版 物：《Computer Modeling in Engineering & Sciences》 (工程与科学中的计算机建模（英文）)

年 卷 期：2020年第122卷第1期

页      面：131-148页

核心收录：

学科分类：0809[工学-电子科学与技术（可授工学、理学学位）] 08[工学] 

基　　金：National Natural Science Foundation of China under grants NSFC 61603363 61703383 61603056 

主　　题：Hypersonic vehicle reentry attitude control mode predictive control jet interference factor reaction control systems 

摘      要：This paper studies the reentry attitude tracking control problem for hypersonic vehicles(HSV)equipped with reaction control systems(RCS)and aerodynamic *** attitude dynamical model of the hypersonic vehicles is established,and the simplified longitudinal and lateral dynamic models are obtained,***,the compound control allocation strategy is provided and the model predictive controller is designed for the pitch ***,considering the complicated jet interaction effect of HSV during RCS is working,an improved model predictive control approach is presented by introducing the online parameter estimation of the jet interaction coefficient for dealing with the uncertainty and ***,considering the strong coupling effect between the yaw channel and roll channel,a coupled model predictive controller is designed by introducing the feedback of sideslip angle into the roll control channel to eliminate the coupling ***,the comparison simulations using the classical control method,MPC and IMPC approach are given to demonstrate the effectiveness and efficiency of the presented IMPC scheme.