Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults

Ruitao Zhang; Hang Guo; Tian Yan; Guangyu Yang; Wenxing Fu

doi:10.1109/CFASTA57821.2023.10243188

Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults

Ruitao Zhang, Hang Guo, Tian Yan, Guangyu Yang, Wenxing Fu

Unmanned System Research Institute

Northwestern Polytechnical University Xian

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

This paper proposes the dynamic inversion-based adaptive fault tolerant control for heavy launch vehicles with non-lethal actuator faults. Firstly, the attitude dynamics model and fault model of heavy launch vehicles are formulated. Secondly, based on the dynamic inversion theory, the ideal controller is designed. Then, the controller and adaptive law are designed for actuator gain faults and bias faults. Meanwhile, the Lyapunov function is constructed to prove that all signals in the closed-loop system are uniformly convergent. Finally, numerical simulation results show the effectiveness and the satisfactory performance of the proposed control algorithm.

Original language	English
Title of host publication	Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	421-426
Number of pages	6
ISBN (Electronic)	9798350332162
DOIs	https://doi.org/10.1109/CFASTA57821.2023.10243188
State	Published - 2023
Event	2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 - Qingdao, China Duration: 14 Jul 2023 → 16 Jul 2023

Publication series

Name	Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023

Conference

Conference	2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023
Country/Territory	China
City	Qingdao
Period	14/07/23 → 16/07/23

Keywords

Adaptive Law
Dynamic Inversion
Fault Tolerant Control
Heavy Launch Vehicles
Lyapunov Function

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10.1109/CFASTA57821.2023.10243188

Cite this

Zhang, R., Guo, H., Yan, T., Yang, G., & Fu, W. (2023). Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults. In Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 (pp. 421-426). (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CFASTA57821.2023.10243188

Zhang, Ruitao ; Guo, Hang ; Yan, Tian et al. / Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults. Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc., 2023. pp. 421-426 (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023).

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title = "Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults",

abstract = "This paper proposes the dynamic inversion-based adaptive fault tolerant control for heavy launch vehicles with non-lethal actuator faults. Firstly, the attitude dynamics model and fault model of heavy launch vehicles are formulated. Secondly, based on the dynamic inversion theory, the ideal controller is designed. Then, the controller and adaptive law are designed for actuator gain faults and bias faults. Meanwhile, the Lyapunov function is constructed to prove that all signals in the closed-loop system are uniformly convergent. Finally, numerical simulation results show the effectiveness and the satisfactory performance of the proposed control algorithm.",

keywords = "Adaptive Law, Dynamic Inversion, Fault Tolerant Control, Heavy Launch Vehicles, Lyapunov Function",

author = "Ruitao Zhang and Hang Guo and Tian Yan and Guangyu Yang and Wenxing Fu",

note = "Publisher Copyright: {\textcopyright} 2023 IEEE.; 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 ; Conference date: 14-07-2023 Through 16-07-2023",

year = "2023",

doi = "10.1109/CFASTA57821.2023.10243188",

language = "英语",

series = "Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "421--426",

booktitle = "Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023",

}

Zhang, R, Guo, H, Yan, T, Yang, G & Fu, W 2023, Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults. in Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023, Institute of Electrical and Electronics Engineers Inc., pp. 421-426, 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023, Qingdao, China, 14/07/23. https://doi.org/10.1109/CFASTA57821.2023.10243188

Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults. / Zhang, Ruitao; Guo, Hang; Yan, Tian et al.
Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc., 2023. p. 421-426 (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Yan, Tian

AU - Yang, Guangyu

AU - Fu, Wenxing

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N2 - This paper proposes the dynamic inversion-based adaptive fault tolerant control for heavy launch vehicles with non-lethal actuator faults. Firstly, the attitude dynamics model and fault model of heavy launch vehicles are formulated. Secondly, based on the dynamic inversion theory, the ideal controller is designed. Then, the controller and adaptive law are designed for actuator gain faults and bias faults. Meanwhile, the Lyapunov function is constructed to prove that all signals in the closed-loop system are uniformly convergent. Finally, numerical simulation results show the effectiveness and the satisfactory performance of the proposed control algorithm.

AB - This paper proposes the dynamic inversion-based adaptive fault tolerant control for heavy launch vehicles with non-lethal actuator faults. Firstly, the attitude dynamics model and fault model of heavy launch vehicles are formulated. Secondly, based on the dynamic inversion theory, the ideal controller is designed. Then, the controller and adaptive law are designed for actuator gain faults and bias faults. Meanwhile, the Lyapunov function is constructed to prove that all signals in the closed-loop system are uniformly convergent. Finally, numerical simulation results show the effectiveness and the satisfactory performance of the proposed control algorithm.

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KW - Dynamic Inversion

KW - Fault Tolerant Control

KW - Heavy Launch Vehicles

KW - Lyapunov Function

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Zhang R, Guo H, Yan T, Yang G, Fu W. Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults. In Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc. 2023. p. 421-426. (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023). doi: 10.1109/CFASTA57821.2023.10243188

Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults

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