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

无人系统技术研究院

Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

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.

源语言	英语
主期刊名	Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023
出版商	Institute of Electrical and Electronics Engineers Inc.
页	421-426
页数	6
ISBN（电子版）	9798350332162
DOI	https://doi.org/10.1109/CFASTA57821.2023.10243188
出版状态	已出版 - 2023
活动	2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 - Qingdao, 中国期限: 14 7月 2023 → 16 7月 2023

出版系列

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

会议

会议	2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023
国家/地区	中国
市	Qingdao
时期	14/07/23 → 16/07/23

访问文件

10.1109/CFASTA57821.2023.10243188

其它文件与链接

链接到 Scopus 的出版物

引用此

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. 在 Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 (页码 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 等. / 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. 页码 421-426 (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023).

@inproceedings{15ef280649bc4d619fd6c54304885260,

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. 在 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., 页码 421-426, 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023, Qingdao, 中国, 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 等.
Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc., 2023. 页码 421-426 (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Dynamic Inversion-Based Adaptive Fault Tolerant Control for Heavy Launch Vehicles with Non-lethal Actuator Faults

AU - Zhang, Ruitao

AU - Guo, Hang

AU - Yan, Tian

AU - Yang, Guangyu

AU - Fu, Wenxing

PY - 2023

Y1 - 2023

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.

KW - Adaptive Law

KW - Dynamic Inversion

KW - Fault Tolerant Control

KW - Heavy Launch Vehicles

KW - Lyapunov Function

UR - https://www.scopus.com/pages/publications/85173626778

U2 - 10.1109/CFASTA57821.2023.10243188

DO - 10.1109/CFASTA57821.2023.10243188

M3 - 会议稿件

AN - SCOPUS:85173626778

T3 - Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023

SP - 421

EP - 426

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

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023

Y2 - 14 July 2023 through 16 July 2023

ER -

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. 在 Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc. 2023. 页码 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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