DocumentCode :
2048690
Title :
Global spacecraft attitude control using magnetic actuators
Author :
Astolfi, Alessandro ; Lovera, Marco
Author_Institution :
Dipt. di Elettronica e Inf., Politecnico di Milano, Italy
Volume :
2
fYear :
2002
fDate :
2002
Firstpage :
1331
Abstract :
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.
Keywords :
attitude control; electromagnetic actuators; space vehicles; stability; state feedback; attitude feedback; global solution; global spacecraft attitude control; inertial pointing; magnetic actuators; rate feedback; Actuators; Aerospace electronics; Aerospace engineering; Attitude control; Educational institutions; Equations; Output feedback; Space vehicles; State feedback; Torque control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2002. Proceedings of the 2002
ISSN :
0743-1619
Print_ISBN :
0-7803-7298-0
Type :
conf
DOI :
10.1109/ACC.2002.1023205
Filename :
1023205
Link To Document :
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