Distributed finite-time attitude regulation for multiple rigid spacecraft via bounded control

被引：58
|
作者：
Cheng, Yingying [1 ]
Du, Haibo [1 ]
He, Yigang [1 ]
Jia, Ruting [2 ]
机构：
[1] Hefei Univ Technol, Sch Elect Engn & Automat, Hefei 230009, Anhui, Peoples R China
[2] Calif State Univ Northridge, Dept Elect & Comp Engn, Northridge, CA 91330 USA
来源：
INFORMATION SCIENCES | 2016年 / 328卷
基金：
中国博士后科学基金;
关键词：
Spacecraft; Attitude control; Finite-time control; Distributed control; TRACKING CONTROL; SYNCHRONIZATION CONTROL; ACTUATOR SATURATION; CONTAINMENT CONTROL; SLIDING-MODE; STABILIZATION; SYSTEMS; STABILITY;
D O I：
10.1016/j.ins.2015.08.042
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The problem of finite-time attitude regulation for multiple rigid spacecraft with leader-follower architecture is studied. The desired attitude for spacecraft formation is represented by the attitude of a leader. A distributed finite-time convergent observer is first proposed to estimate the leader's attitude in a finite time. By using the technique of finite-time saturation control, a bounded finite-time attitude controller is designed to track the estimated attitude and then the leader's attitude in a finite time. A simulation example is finally given. (C) 2015 Elsevier Inc. All rights reserved.
引用
收藏
页码：144 / 157
页数：14
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