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