Distributed prescribed-time coordinated control of spacecraft formation flying under input saturation

被引:0
|
作者
Xu, Chuang [1 ]
Zelazo, Daniel [2 ]
Wu, Baolin [3 ]
机构
[1] Aerosp Time Feipeng Co Ltd, Suzhou 215000, Peoples R China
[2] Technion Israel Inst Technol, IL-3100000 H_efa, Israel
[3] Harbin Inst Technol, Harbin 150080, Peoples R China
基金
中国国家自然科学基金;
关键词
Spacecraft formation flying; Distributed control; Prescribed-time control; Input saturation; TRACKING CONTROL; SYNCHRONIZATION CONTROL; MULTIPLE SPACECRAFT; RELATIVE MOTION;
D O I
10.1016/j.asr.2024.05.077
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper studies the prescribed-time relative motion control problem of spacecraft formation flying under input saturation. Using prescribed-time theory, a prescribed-time sliding mode is designed such that the states on the sliding mode converge to the equilibrium in the prescribed time. Based on the prescribed-time sliding mode, a prescribed-time relative motion tracking controller is developed, which guarantees fast formation maneuvers with feasible fuel consumption and strong robustness under input saturation. Furthermore, a simulation example is carried out to verify the effectiveness of the proposed controller. (c) 2024 COSPAR. Published by Elsevier B.V. All rights are reserved, including those for text and data mining, AI training, and similar technologies.
引用
收藏
页码:2302 / 2315
页数:14
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