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Finite-time Dynamic Surface Fault-tolerant Control for Hypersonic Vehicle with Mismatched Disturbances

  • Control Theory and Applications
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Abstract

This paper studies the tracking control problem of hypersonic vehicle in the process of external disturbance, parameters uncertainties and actuator faults. Firstly, a non-triangular velocity and altitude nonlinear subsystem with mismatched disturbances and actuator faults are established based on the feedback linearization model. Secondly, adaptive dynamic surface fault-tolerant controllers are designed for velocity and altitude subsystems by combining nonlinear filter, adaptive control and back-step** method. Finally, the Lyapunov stability theory and numercial simulation are carried out to verify the availability of the proposed control strategy.

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Authors and Affiliations

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Correspondence to ** and multi-agent navigation.

Chen-Yu He received his B.S. degree in automation from Hunan Institute of Technology, **angtan, China, in 2018. He is a postgraduate student in control theory and control engineering of **angtan University, **angtan, China. His current research interests are path optimization and multiagent navigation.

**ao-Qing Liu received her B.S. degree in automation from Harbin University of Science and Technology, Harbin, China, in 2005, and her M.S. degree in control theory and control engineering from Harbin Engineering University, Harbin, China, in 2008. She is a Ph.D. student in the Department of Precision Instrument of Tsinghua University. Her current research interests are iterative learning control and integrated navigation.

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Li, P., Huang, P., He, CY. et al. Finite-time Dynamic Surface Fault-tolerant Control for Hypersonic Vehicle with Mismatched Disturbances. Int. J. Control Autom. Syst. 19, 2309–2322 (2021). https://doi.org/10.1007/s12555-020-0169-3

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  • DOI: https://doi.org/10.1007/s12555-020-0169-3

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