Cascade Control and Stability Analysis of Spacecraft Formation

被引：0
|
作者：
Cui, Shihang [1 ]
Li, Yong [1 ]
机构：
[1] China Acad Space Technol, Qian Xuesen Lab Space Technol, Beijing, Peoples R China
来源：
2019 CHINESE AUTOMATION CONGRESS (CAC2019) | 2019年
基金：
国家重点研发计划; 中国国家自然科学基金;
关键词：
spacecraft formation; cascade system; stability analysis;
D O I：
10.1109/cac48633.2019.8996881
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, a dynamic model for leader-follower spacecraft formation flying is established, and the attitude control algorithm of the leader spacecraft and the relative position control algorithm between the leader and the follower spacecraft are calculated respectively. According to the stability theory of cascade system, the asymptotic stability of the whole closed-loop system is proved.
引用
收藏
页码：3020 / 3024
页数：5
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