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A controllability-stabilizability result for the NASA-IEEE Spacecraft Control Laboratory Experiment (SCOLE) configurationA nonlinear distributed parameter model for the NASA-Institute of Electrical and Electronics Engineers' Spacecraft Control Laboratory Experiment (SCOLE) configuration is considered. A linear feedback control law is proposed that points the line of sight of the antenna to any given target direction and at the same time stabilizes the oscillations of the entire flexible configuration.
Document ID
19920074943
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Araya, Roberto (California Univ. Los Angeles, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1984
Publication Information
Publication: NASA. Langley Research Center, Spacecraft Control Laboratory Experiment (SCOLE) Workshop, 1984
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
92N70067
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-0318-83
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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