DocumentCode
488338
Title
Satellite Stabilization using Space Leeches
Author
Walker, Michael W. ; Kim, Dong-Min
Author_Institution
Artificial Intelligence Laboratory, Department of Electrical Engineering and Computer Science, The University of Michigan, Ann Arbor, Michigan 48109
fYear
1990
fDate
23-25 May 1990
Firstpage
1314
Lastpage
1319
Abstract
This paper presents the control algorithm for a satellite stabilization using a space leech. The space leech is assumed to have n reaction wheels with known moments of inertia about their axis of rotation. All mass properties of the satellite are assumed unknown The proposed control algorithm brings the satellite to a specified attitude trajectory.
Keywords
Adaptive control; Angular velocity control; Artificial intelligence; Artificial satellites; Attitude control; Kinetic energy; Laboratories; Robot kinematics; Weight control; Wheels;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1990
Conference_Location
San Diego, CA, USA
Type
conf
Filename
4790954
Link To Document