Electronics and Electrical Engineering and Control

ADP-based intelligent attitude fault-tolerant control for launch vehicles

  • LIANG Xiaohui ,
  • HU Changhua ,
  • ZHOU Zhijie ,
  • WANG Qing
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  • 1. School of Automation, Northwestern Polytechnical University, Xi'an 710072, China;
    2. College of Missile Engineering, Rocket Force University of Engineering, Xi'an 710025, China;
    3. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China

Received date: 2020-10-22

  Revised date: 2020-12-18

  Online published: 2021-01-26

Supported by

National Natural Science Foundation of China (61833016, 61873295, 61933010)

Abstract

This paper investigates the problem of attitude control for the launch vehicle with actuator faults. An Adaptive Dynamic Programming (ADP) based intelligent fault-tolerant control scheme is developed, which mainly includes two parts: the stable control part and optimization supplementary part. For the stable control part, the adaptive control technology and the sliding mode variable structure control are used to maintain stability of the fault-tolerant controller, so as to guarantee the stalibilty of the close-loop system and finite-time convergence of the tracking errors. An optimization supplementary controller with the actor-critic structure is also designed to further improve the attitude tracking performance and provide additional compensation control according to the tracking errors caused by actuator faults or external disturbances. The simulation results show that the proposed method can ensure the system stablility and accurate tacking of commands even when there exist malfunctions.

Cite this article

LIANG Xiaohui , HU Changhua , ZHOU Zhijie , WANG Qing . ADP-based intelligent attitude fault-tolerant control for launch vehicles[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021 , 42(4) : 524915 -524915 . DOI: 10.7527/S1000-6893.2020.24915

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