Bifurcation analysis of the attitude dynamics for a magnetically controlled spacecraft

被引：0
|
作者：
Della Rossa, Fabio [1 ]
Bergamasco, Marco [1 ]
Lovera, Marco [1 ]
机构：
[1] Politecn Milan, Dipartimento Elettron & Informaz, I-20133 Milan, Italy
来源：
2012 IEEE 51ST ANNUAL CONFERENCE ON DECISION AND CONTROL (CDC) | 2012年
关键词：
SUBJECT;
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：
The dynamics of a spacecraft equipped with magnetic actuators operating under a static attitude and rate feedback control law designed using averaging theory is considered and the asymptotic behaviour of the closed-loop system as a function of the averaging scaling parameter is analysed, using bifurcation methods.
引用
收藏
页码：1154 / 1159
页数：6
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