Magnetic attitude control of spacecraft with flexible appendages

被引：4
|
作者：
Schiavo, Francesco [1 ]
Lovera, Marco [1 ]
Astolfi, Alessandro [2 ,3 ]
机构：
[1] Politecn Milan, Dipartimento Elettr Informaz, Piazza Leonardo da Vinci 32, I-20133 Milan, Italy
[2] Imperial Coll London, Dept Elect & Elect Engn, London SW7 2AZ, England
[3] Univ Roma Tor Vergata, Dipartimento Informat Sist & Produzione, I-00133 Rome, Italy
来源：
PROCEEDINGS OF THE 45TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-14 | 2006年
关键词：
D O I：
10.1109/CDC.2006.377766
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A mathematical model for the attitude dynamics of a spacecraft with flexible appendages is derived and the problem of inertial pointing for a flexible spacecraft equipped with magnetic actuators is addressed. An almost global solution to the problem is obtained by means of static rigid body attitude and rate feedback. Simulation results demonstrate the practical applicability of the proposed approach.
引用
收藏
页码：1545 / +
页数：2
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