Global spacecraft attitude control using magnetic actuators

被引：0
|
作者：
Astolfi, A [1 ]
Lovera, M [1 ]
机构：
[1] Politecn Milan, Dipartimento Elettron & Informat, I-20133 Milan, Italy
来源：
PROCEEDINGS OF THE 2002 AMERICAN CONTROL CONFERENCE, VOLS 1-6 | 2002年 / 1-6卷
关键词：
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 problem of inertial pointing for a spacecraft with magnetic actuators is addressed. It is shown that a global solution to the problem can be obtained by means of (static) attitude and rate feedback and (dynamic) attitude feedback. Simulation results demonstrate the practical applicability of the proposed approach.
引用
收藏
页码：1331 / 1335
页数：5
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