Finite-time distributed cooperative attitude tracking control for multiple rigid spacecraft

被引：40

作者：

He, Xiaoyan ^{[1
,2
]}

Wang, Qingyun ^{[1
]}

Yu, Wenwu ^{[3
,4
]}

机构：

[1] Beihang Univ, Dept Dynam & Control, Beijing 100191, Peoples R China

[2] Inner Mongolia Univ Finance & Econ, Dept Math & Stat, Hohhot 010070, Peoples R China

[3] Southeast Univ, Dept Math, Nanjing 210096, Jiangsu, Peoples R China

[4] King Abdulaziz Univ, Fac Engn, Jeddah 21589, Saudi Arabia

来源：

APPLIED MATHEMATICS AND COMPUTATION | 2015年 / 256卷

基金：

美国国家科学基金会;

关键词：

Terminal sliding-model control (TSM); Cooperative attitude control; Finite-time tracking control; Rigid spacecrafts; MULTIAGENT SYSTEMS; STABILIZATION; CONSENSUS; ROBUST;

D O I：

10.1016/j.amc.2015.01.061

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

We investigate the finite-time cooperative attitude synchronization and tracking control for multiple rigid spacecrafts with a time-varying leader, whose attitude is represented by modified rodriguez parameters. In particular, the studied systems are composed of one dynamic leader with bounded unknown acceleration inputs and some followers with bounded disturbances. A novel nonlinear tracking control protocol is constructed via nonsingular terminal sliding mode scheme. It is shown that the proposed protocol can effectively drive the states of the followers to track the leader within the finite-time. Finally, an example is illustrated to verify the proposed protocol. (C) 2015 Elsevier Inc. All rights reserved.

引用

页码：724 / 734

页数：11

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