Relative attitude control in satellite formation flying with information delay

被引：0
|
作者：
Li, Huayi [1 ]
Zhang, Yingchun [1 ]
Qiang, Wenyi [2 ]
Li, Baohua [1 ]
机构：
[1] Res Ctr Satellite, Harbin Inst Technol, Harbin 150001, Peoples R China
[2] Harbin Inst Technol, Dept Control Sci & Engn, Harbin 150001, Peoples R China
来源：
WCICA 2006: SIXTH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION, VOLS 1-12, CONFERENCE PROCEEDINGS | 2006年
关键词：
satellite formation flying; relative attitude control; estimator; information delay;
D O I：
暂无
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 leader-follower formation flying, using the leader's rate of rotation, the follower calculate the target attitude and rate of rotation, which are necessary to relative attitude control. In the process of information collecting, computing and transmitting, time delay exist that causes information delay. To deal with it, rate and attitude estimators are presented which provide target rate and attitude real time. Then a PID control law for small satellite with reaction wheels is developed based on them. Simulation results show the approach is valid.
引用
收藏
页码：8453 / +
页数：2
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