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Stability and control of flexible satellites. II - ControlIt is demonstrated that by monitoring the deformations of the flexible elements of a satellite, the effectiveness of the satellite control system can be increased considerably. A simple model of a flexible satellite was analyzed in the first part of this work. The same model is used here for digital computer simulations.
Document ID
19810033952
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Huang, T. C. (Wisconsin, University Madison, Wis., United States)
Das, A. (General Electric Co., Space Div., Valley Forge Pa., United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 80-E-235
Accession Number
81A18356
Funding Number(s)
CONTRACT_GRANT: NAS5-21798
Distribution Limits
Public
Copyright
Other

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