Nonlinear attitude tracking control for spacecraft formation with multiple delays

被引：27
|
作者：
Yang, Hongjiu [1 ]
You, Xiu [1 ]
Xia, Yuanqing [2 ]
Liu, Zhixin [1 ]
机构：
[1] Yanshan Univ, Coll Elect Engn, Qinhuangdao 066004, Peoples R China
[2] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
来源：
ADVANCES IN SPACE RESEARCH | 2014年 / 54卷 / 04期
基金：
中国国家自然科学基金;
关键词：
Spacecraft formulation; Attitude tracking; Nonlinear control; Adaptive control; Multiple delays; DISTURBANCE REJECTION CONTROL; SLIDING MODE CONTROL; FLEXIBLE SPACECRAFT; SYNCHRONIZATION; SYSTEMS; COORDINATION; CONSENSUS;
D O I：
10.1016/j.asr.2014.04.026
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper addresses the attitude tracking control for spacecraft formation with delay free and communication delays. With help of the idea of sliding control, an adaptive attitude synchronization control architecture is established. Furthermore, by introducing a nonsmooth feedback function, a new class of nonlinear controllers for the attitude tracking of spacecraft is developed. Both parameter uncertainties and unknown external disturbances are dealt with via the kind of controllers. Finally, some simulation results are given to demonstrate the effectiveness and advantages of the proposed results. (C) 2014 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：759 / 769
页数：11
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