DocumentCode
3159199
Title
Global magnetic attitude control of spacecraft
Author
Lovera, Marco ; Astolfi, Alessandro
Author_Institution
Dipartimento di Elettronica e Informazione, Politecnico di Milano, Milan, Italy
Volume
1
fYear
2004
fDate
14-17 Dec. 2004
Firstpage
267
Abstract
The problem of inertial pointing for a spacecraft with magnetic actuators is addressed and an almost global solution to the problem is obtained by means of static attitude, rate feedback and of dynamic attitude feedback. Simulation results demonstrate the practical applicability of the proposed approach.
Keywords
attitude control; electromagnetic actuators; feedback; magnetic variables control; space vehicles; dynamic attitude feedback; global magnetic attitude control; magnetic actuator; rate feedback; spacecraft; static attitude; Actuators; Angular velocity; Angular velocity control; Attitude control; Coils; Earth; Equations; Magnetic analysis; Space vehicles; State feedback;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2004. CDC. 43rd IEEE Conference on
ISSN
0191-2216
Print_ISBN
0-7803-8682-5
Type
conf
DOI
10.1109/CDC.2004.1428641
Filename
1428641
Link To Document