Affiliation:
1. School of Electrical Engineering and Automation, Tianjin University of Technology, Tianjin, China
2. Tianjin Key Laboratory for Control Theory & Applications in Complicated Industry Systems, Tianjin, China
Abstract
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.
Funder
National Natural Science Foundation of China
Subject
Mechanical Engineering,Aerospace Engineering
Cited by
2 articles.
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