Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft

Ling Mao; Bing Cui; Xifei Chen; Yuanqing Xia

doi:10.1109/CFASTA57821.2023.10243389

Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft

Ling Mao^*, Bing Cui, Xifei Chen, Yuanqing Xia

^*Corresponding author for this work

School of Automation

Beijing Institute of Technology

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

Abstract

In this paper, distributed prescribed-Time fault-Tolerant attitude tracking control problem for multiple spacecraft is investigated under a directed communication topology. Each follower spacecraft is subject to unknown nonidentical and unpredictable actuation faults. By using time transformation approach, a distributed prescribed-Time attitude tracking protocol is designed for each follower to track the states of the leader. By using the uniformly bounded time-varying gains, the numerical implementation problem arising from infinite time-varying gain is avoided, and the prescribed time can be determined in advance, irrespective of the initial conditions of the followers, which is deemed favorable in practice. Simulation results are provided to validate the effectiveness of the developed distributed attitude control scheme.

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	296-301
Number of pages	6
ISBN (Electronic)	9798350332162
DOIs	https://doi.org/10.1109/CFASTA57821.2023.10243389
Publication status	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

Directed Topology
Distributed Attitude Control
Multiple spacecraft systems
Prescribed-Time Control

Access to Document

10.1109/CFASTA57821.2023.10243389

Cite this

Mao, L., Cui, B., Chen, X., & Xia, Y. (2023). Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft. In Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 (pp. 296-301). (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/CFASTA57821.2023.10243389

Mao, Ling ; Cui, Bing ; Chen, Xifei et al. / Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft. Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc., 2023. pp. 296-301 (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023).

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title = "Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft",

abstract = "In this paper, distributed prescribed-Time fault-Tolerant attitude tracking control problem for multiple spacecraft is investigated under a directed communication topology. Each follower spacecraft is subject to unknown nonidentical and unpredictable actuation faults. By using time transformation approach, a distributed prescribed-Time attitude tracking protocol is designed for each follower to track the states of the leader. By using the uniformly bounded time-varying gains, the numerical implementation problem arising from infinite time-varying gain is avoided, and the prescribed time can be determined in advance, irrespective of the initial conditions of the followers, which is deemed favorable in practice. Simulation results are provided to validate the effectiveness of the developed distributed attitude control scheme.",

keywords = "Directed Topology, Distributed Attitude Control, Multiple spacecraft systems, Prescribed-Time Control",

author = "Ling Mao and Bing Cui and Xifei Chen and Yuanqing Xia",

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/CFASTA57821.2023.10243389",

language = "English",

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

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

pages = "296--301",

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

address = "United States",

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Mao, L, Cui, B, Chen, X & Xia, Y 2023, Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft. 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. 296-301, 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023, Qingdao, China, 14/07/23. https://doi.org/10.1109/CFASTA57821.2023.10243389

Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft. / Mao, Ling; Cui, Bing; Chen, Xifei 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. 296-301 (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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T1 - Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft

AU - Mao, Ling

AU - Cui, Bing

AU - Chen, Xifei

AU - Xia, Yuanqing

PY - 2023

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N2 - In this paper, distributed prescribed-Time fault-Tolerant attitude tracking control problem for multiple spacecraft is investigated under a directed communication topology. Each follower spacecraft is subject to unknown nonidentical and unpredictable actuation faults. By using time transformation approach, a distributed prescribed-Time attitude tracking protocol is designed for each follower to track the states of the leader. By using the uniformly bounded time-varying gains, the numerical implementation problem arising from infinite time-varying gain is avoided, and the prescribed time can be determined in advance, irrespective of the initial conditions of the followers, which is deemed favorable in practice. Simulation results are provided to validate the effectiveness of the developed distributed attitude control scheme.

AB - In this paper, distributed prescribed-Time fault-Tolerant attitude tracking control problem for multiple spacecraft is investigated under a directed communication topology. Each follower spacecraft is subject to unknown nonidentical and unpredictable actuation faults. By using time transformation approach, a distributed prescribed-Time attitude tracking protocol is designed for each follower to track the states of the leader. By using the uniformly bounded time-varying gains, the numerical implementation problem arising from infinite time-varying gain is avoided, and the prescribed time can be determined in advance, irrespective of the initial conditions of the followers, which is deemed favorable in practice. Simulation results are provided to validate the effectiveness of the developed distributed attitude control scheme.

KW - Directed Topology

KW - Distributed Attitude Control

KW - Multiple spacecraft systems

KW - Prescribed-Time Control

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

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

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Mao L, Cui B, Chen X, Xia Y. Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft. In Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc. 2023. p. 296-301. (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023). doi: 10.1109/CFASTA57821.2023.10243389

Distributed prescribed-Time fault-Tolerant attitude tracking control for multiple rigid spacecraft

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