Fault Tolerant Control of Hypersonic Vehicle Based on Improved Prescribed Performance

WEI Zhihua; MING Chao; YANG Kaiyuan; YAN Suyu

doi:10.15892/j.cnki.djzdxb.2025.03.010

Journal of Projectiles, Rockets, Missiles and Guidance >

2025 , Vol. 45 >Issue 3: 336 - 343

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2025.03.010

Fault Tolerant Control of Hypersonic Vehicle Based on Improved Prescribed Performance

WEI Zhihua ,
MING Chao ,
YANG Kaiyuan ,
YAN Suyu

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School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China

Received date: 2024-10-18

Online published: 2025-07-09

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Abstract

In response to the limitations of traditional prescribed performance in controller design, this paper studies a non singular terminal sliding mode fault-tolerant control method that improves prescribed performance. Aiming at the problem of control singularity caused by the convergence speed of the performance boundary of traditional prescribed performance being too fast and the tracking error exceeding the performance boundary, an improved performance function and an improved error conversion function are proposed. The converted error is introduced into the design of a non singular terminal sliding fault-tolerant controller. Simultaneously utilizing an extended state observer to accurately estimate unknown external disturbances in the system, and compensating them to the controller to solve the problem of partial failure of the actuator and suppress elastic effects, in order to obtain preset transient and asymptotic steady-state performance. The stability is proved through Lyapunov theory analysis. Finally, the effectiveness and superiority of the proposed fault-tolerant control method are verified through simulation and comparative experiments of the attitude system of air breathing hypersonic vehicle.

Key words： air breathing hypersonic vehicle; attitude control; improved prescribed performance; sliding mode control; fault tolerant control

Cite this article

WEI Zhihua , MING Chao , YANG Kaiyuan , YAN Suyu . Fault Tolerant Control of Hypersonic Vehicle Based on Improved Prescribed Performance[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2025 , 45(3) : 336 -343 . DOI: 10.15892/j.cnki.djzdxb.2025.03.010

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