Fault-Tolerant Attitude Control of Spacecraft with Dynamic Pointing Constraints

Yuan Tian; Xiaodong Shao; Qinglei Hu; Jianying Zheng

doi:10.1007/978-981-19-6613-2_32

Fault-Tolerant Attitude Control of Spacecraft with Dynamic Pointing Constraints

Yuan Tian
, Xiaodong Shao^*
, Qinglei Hu
, Jianying Zheng

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University
Beihang Hangzhou Innovation Institute Yuhang

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

Abstract

This article investigates the fault-tolerant control (FTC) strategy towards attitude reorientation for an uncertain spacecraft under dynamic pointing constraints and faulty actuators. Specifically and firstly, an artificial potential function (APF) is designed to encode both unwinding and pointing constraints according to the analytical properties of quaternions. Then, an adaptive robust FTC scheme is derived using the APF in conjunction with the adaptive backstepping method. Using the Lyapunov analysis, it is proved the designed control scheme is able to ensure that attitude error and angular velocity asymptotically approach zero, under circumstances of model uncertainties, environmental disturbances, and actuator faults. Finally, simulations showcase the effectivity of the derived strategy in terms of avoidance of the unwinding phenomenon and dynamic pointing constraints.

Original language	English
Title of host publication	Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
Editors	Liang Yan, Haibin Duan, Yimin Deng, Liang Yan
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	318-327
Number of pages	10
ISBN (Print)	9789811966125
DOIs	https://doi.org/10.1007/978-981-19-6613-2_32
State	Published - 2023
Event	International Conference on Guidance, Navigation and Control, ICGNC 2022 - Harbin, China Duration: 5 Aug 2022 → 7 Aug 2022

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	845 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	International Conference on Guidance, Navigation and Control, ICGNC 2022
Country/Territory	China
City	Harbin
Period	5/08/22 → 7/08/22

Keywords

Fault-tolerant control
Pointing constraint
Spacecraft attitude maneuver

Access to Document

10.1007/978-981-19-6613-2_32

Cite this

Tian, Y., Shao, X., Hu, Q., & Zheng, J. (2023). Fault-Tolerant Attitude Control of Spacecraft with Dynamic Pointing Constraints. In L. Yan, H. Duan, Y. Deng, & L. Yan (Eds.), Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control (pp. 318-327). (Lecture Notes in Electrical Engineering; Vol. 845 LNEE). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-19-6613-2_32

Tian, Yuan ; Shao, Xiaodong ; Hu, Qinglei et al. / Fault-Tolerant Attitude Control of Spacecraft with Dynamic Pointing Constraints. Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. editor / Liang Yan ; Haibin Duan ; Yimin Deng ; Liang Yan. Springer Science and Business Media Deutschland GmbH, 2023. pp. 318-327 (Lecture Notes in Electrical Engineering).

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title = "Fault-Tolerant Attitude Control of Spacecraft with Dynamic Pointing Constraints",

abstract = "This article investigates the fault-tolerant control (FTC) strategy towards attitude reorientation for an uncertain spacecraft under dynamic pointing constraints and faulty actuators. Specifically and firstly, an artificial potential function (APF) is designed to encode both unwinding and pointing constraints according to the analytical properties of quaternions. Then, an adaptive robust FTC scheme is derived using the APF in conjunction with the adaptive backstepping method. Using the Lyapunov analysis, it is proved the designed control scheme is able to ensure that attitude error and angular velocity asymptotically approach zero, under circumstances of model uncertainties, environmental disturbances, and actuator faults. Finally, simulations showcase the effectivity of the derived strategy in terms of avoidance of the unwinding phenomenon and dynamic pointing constraints.",

keywords = "Fault-tolerant control, Pointing constraint, Spacecraft attitude maneuver",

author = "Yuan Tian and Xiaodong Shao and Qinglei Hu and Jianying Zheng",

note = "Publisher Copyright: {\textcopyright} 2023, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.; International Conference on Guidance, Navigation and Control, ICGNC 2022 ; Conference date: 05-08-2022 Through 07-08-2022",

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doi = "10.1007/978-981-19-6613-2\_32",

language = "英语",

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Tian, Y, Shao, X , Hu, Q & Zheng, J 2023, Fault-Tolerant Attitude Control of Spacecraft with Dynamic Pointing Constraints. in L Yan, H Duan, Y Deng & L Yan (eds), Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. Lecture Notes in Electrical Engineering, vol. 845 LNEE, Springer Science and Business Media Deutschland GmbH, pp. 318-327, International Conference on Guidance, Navigation and Control, ICGNC 2022, Harbin, China, 5/08/22. https://doi.org/10.1007/978-981-19-6613-2_32

Fault-Tolerant Attitude Control of Spacecraft with Dynamic Pointing Constraints. / Tian, Yuan; Shao, Xiaodong ; Hu, Qinglei et al.
Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. ed. / Liang Yan; Haibin Duan; Yimin Deng; Liang Yan. Springer Science and Business Media Deutschland GmbH, 2023. p. 318-327 (Lecture Notes in Electrical Engineering; Vol. 845 LNEE).

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

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AB - This article investigates the fault-tolerant control (FTC) strategy towards attitude reorientation for an uncertain spacecraft under dynamic pointing constraints and faulty actuators. Specifically and firstly, an artificial potential function (APF) is designed to encode both unwinding and pointing constraints according to the analytical properties of quaternions. Then, an adaptive robust FTC scheme is derived using the APF in conjunction with the adaptive backstepping method. Using the Lyapunov analysis, it is proved the designed control scheme is able to ensure that attitude error and angular velocity asymptotically approach zero, under circumstances of model uncertainties, environmental disturbances, and actuator faults. Finally, simulations showcase the effectivity of the derived strategy in terms of avoidance of the unwinding phenomenon and dynamic pointing constraints.

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Tian Y, Shao X , Hu Q , Zheng J. Fault-Tolerant Attitude Control of Spacecraft with Dynamic Pointing Constraints. In Yan L, Duan H, Deng Y, Yan L, editors, Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. Springer Science and Business Media Deutschland GmbH. 2023. p. 318-327. (Lecture Notes in Electrical Engineering). doi: 10.1007/978-981-19-6613-2_32