Distributed Fixed-time Attitude Synchronization Control for Multiple Rigid Spacecraft

被引：27
|
作者：
Sui, Wei-Shun [1 ]
Duan, Guang-Ren [1 ]
Hou, Ming-Zhe [1 ]
Zhang, Mao-Rui [1 ]
机构：
[1] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, 2 Yi Kuang St, Harbin 150001, Heilongjiang, Peoples R China
来源：
INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS | 2019年 / 17卷 / 05期
基金：
中国国家自然科学基金;
关键词：
Attitude synchronization; distributed adaptive control; fixed-time-based terminal sliding mode; sliding-mode estimator;
D O I：
10.1007/s12555-017-0717-7
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper investigates the distributed fixed-time attitude synchronization control problem for multiple rigid spacecraft system with external disturbances. Based on sliding-mode estimators, the authors remove the requirement of neighbours' input control information. Using the fixed-time-based terminal sliding mode, the distributed adaptive control laws are developed to guarantee the attitude tracking errors converge to the regions in fixed time independent of initial conditions, and adaptive laws are employed to deal with external disturbances. Finally, numerical simulations are presented to illustrate the performance of the proposed controllers.
引用
收藏
页码：1117 / 1130
页数：14
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