Attitude synchronization control for a group of flexible spacecraft

被引：154
作者：
Du, Haibo [1 ,3 ]
Li, Shihua [2 ,3 ]
机构：
[1] Hefei Univ Technol, Sch Elect Engn & Automat, Hefei 230009, Peoples R China
[2] Southeast Univ, Sch Automat, Nanjing 210096, Jiangsu, Peoples R China
[3] Southeast Univ, Key Lab Measurement & Control Complex Syst Engn, Minist Educ, Nanjing 210096, Jiangsu, Peoples R China
来源：
AUTOMATICA | 2014年 / 50卷 / 02期
基金：
中国国家自然科学基金; 中国博士后科学基金;
关键词：
Attitude synchronization; Flexible spacecraft; Distributed control; CONSENSUS; SYSTEMS;
D O I：
10.1016/j.automatica.2013.11.022
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
To solve the problem of attitude synchronization for a group of flexible spacecraft during formation maneuvers, a distributed attitude cooperative control strategy is investigated in this paper. Based on the backstepping design and the neighbor-based design rule, a distributed attitude control law is constructed step by step. Using cascaded systems' theory and graph theory, it is shown that the attitude synchronization is achieved asymptotically and the induced vibrations by flexible appendages are simultaneously suppressed under the proposed control law. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码：646 / 651
页数：6
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