Robust distributed model predictive control for satellite cluster reconfiguration with collision avoidance

被引:7
|
作者
Li, Siyuan [1 ]
Ye, Dong [1 ]
Xiao, Yan [1 ]
Sun, Zhaowei [1 ]
机构
[1] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150001, Peoples R China
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
Satellite cluster reconfiguration; Distributed model predictive control; Tube; -based; Collision avoidance; Optimal allocation; RELATIVE MOTION; SPACECRAFT; ASSIGNMENT;
D O I
10.1016/j.ast.2022.107917
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article investigates a reconfiguration problem of the satellite cluster with collision avoidance. Focusing on the uncertain disturbances with upper bound, a tube-based auxiliary controller is designed, which can improve the robustness of actual satellite cluster system. Then, a distributed model predictive controller (DMPC) is proposed for the nominal system with thrust constraints. In DMPC, the terminal constraints and terminal control law based on velocity obstacle are designed to satisfy the collision avoidance. Furthermore, the stability and feasibility can be ensured by using optimized slack variable. In addition, to reduce fuel consumption and the actions of collision, an optimal allocation strategy for target points based on Hungarian algorithm is adopted. Finally, the numerical simulations are presented to verify the effectiveness and advantage of the proposed scheme.(c) 2022 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:18
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