Q-learning-based practical disturbance compensation control for hypersonic flight vehicle

被引:2
|
作者
Li, Xu [1 ,2 ]
Zhang, Ziyi [1 ,2 ]
Ji, Yuehui [1 ,2 ]
Liu, Junjie [1 ,2 ]
Gao, Qiang [1 ,2 ]
机构
[1] Tianjin Univ Technol, Sch Elect Engn & Automation, Bldg 29,391 Binshuixi Rd, Tianjin, Peoples R China
[2] Tianjin Key Lab Control Theory & Applicat Complica, Tianjin, Peoples R China
基金
中国国家自然科学基金;
关键词
Hypersonic flight vehicle; attitude control; super-twisting algorithm; extended state observer; Q-learning; FAULT-TOLERANT CONTROL; SLIDING MODE CONTROL; REJECTION CONTROL; ADAPTIVE-CONTROL; ATTITUDE-CONTROL; CONTROL SCHEME; DESIGN; STRATEGY; GAME; GO;
D O I
10.1177/09544100221140242
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Aiming at the attitude control problem of hypersonic flight vehicle, a compound control strategy based on the disturbance compensation technique and Q-learning optimization is proposed. Firstly, a three-channel independent control scheme based on the super-twisting extended state observer (STESO) is proposed such that coupling among channels, uncertainties, and external disturbances can be estimated and compensated in real time. Secondly, the Q-learning mechanism is introduced to optimize the control parameters while keeping the control structure unchanged. Lastly, the convergence of the STESO is analyzed by the Lyapunov theory, and some numerical simulation results are carried out to verify the effectiveness of the proposed strategy. Compared with the traditional linear active disturbance rejection control, the proposed method can avoid a lot of manual parameter tuning process and also has better performance.
引用
收藏
页码:1916 / 1929
页数:14
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