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Full Length Article | Open Access

Distributed adaptive prescribed-time orbit containment control for satellite cluster flight

Tingting ZHANGa, Shijie ZHANGa,( ), Huayi LIa, Xiangtian ZHAOb
Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150080, China
State Key Laboratory of Networking and Switching Technology, Beijing University of Posts and Telecommunications, Beijing 100876, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

The distributed prescribed-time orbit containment control for the satellite cluster flight with multiple dynamic leaders is investigated. The directed information communication topology between followers is taken into account in the overall paper. When the satellite mass is assumed to be constant, a distributed prescribed-time orbit containment controller is, firstly, presented to drive the followers into the dynamic convex hull produced by multiple leaders. Then, the parameter uncertainty is considered, and a prescribed-time sliding mode estimator is introduced to estimate the desired velocity of each follower. Based on the estimated state, a novel distributed adaptive prescribed-time orbit containment control scheme is proposed. The Lyapunov stability theory is utilized to prove the prescribed-time stability of the closed-loop system. Finally, several numerical simulations and comparison of different control methods are provided to verify the effectiveness and superiority of the proposed control method.

Keywords

Parameter uncertaintySatellite clusterOrbit containment controlPrescribed-time controlDirected communication graph

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Chinese Journal of Aeronautics
Volume 37 Issue 8,
August 2024
Pages 342-357
DOI: 10.1016/j.cja.2024.04.020
Cite this article:
ZHANG T, ZHANG S, LI H, et al. Distributed adaptive prescribed-time orbit containment control for satellite cluster flight. Chinese Journal of Aeronautics, 2024, 37(8): 342-357. https://doi.org/10.1016/j.cja.2024.04.020

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Received: 04 September 2023
Revised: 26 October 2023
Accepted: 15 January 2024
Published: 25 April 2024
© 2024 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
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