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Satellite stabilization using space leechesA control algorithm for satellite stabilization using a space leech is presented. 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 to be unknown. The algorithm brings the satellite to a specified attitude trajectory. Simulations were performed to demonstrate the controller. The model parameters and specific algorithm used and the results obtained are presented.
Document ID
19910045494
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Walker, Michael W.
(Michigan Univ. Ann Arbor, MI, United States)
Kim, Dong-Min
(Michigan, University Ann Arbor, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91A30117
Distribution Limits
Public
Copyright
Other

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