Finite-time distributed hierarchical control for satellite cluster with collision avoidance

被引:17
|
作者
Li, Siyuan [1 ]
Liu, Chuang [1 ,2 ]
Sun, Zhaowei [1 ]
机构
[1] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150001, Peoples R China
[2] Northwestern Polytech Univ, Sch Astronaut, Xian 710072, Peoples R China
基金
中国博士后科学基金;
关键词
Satellite cluster; Hierarchical control; Collision avoidance; Multiple disturbances; Input constraints; SLIDING MODE CONTROL; ATTITUDE STABILIZATION; OBSTACLE AVOIDANCE; SPACECRAFT; DESIGN; FLIGHT;
D O I
10.1016/j.ast.2021.106750
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, a novel distributed hierarchical control method for small satellites with multiple disturbances and input constraints is investigated by combining formation flying and satellite cluster. First, a finite-time convergent extended state observer (FTCESO) is developed to estimate the external disturbance with high precision, and a non-singular fast terminal sliding mode controller (NFTSMC) is proposed to maintain the specific configuration of leader-satellites and the finite time convergence is theoretically proved. Then, an improved artificial potential field method with collision avoidance and damping characteristics is proposed for the follower-satellite, so that the follower-satellite can keep a collision-avoidance relative distance from corresponding leader-satellite with the desired communication range. Finally, numerical simulations are performed to demonstrate the effectiveness of the proposed method. (C) 2021 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:18
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