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On the optimal angular velocity control of asymmetrical space vehicles.Space vehicle angular velocities reduced to zero through linear and nonlinear optimal feedback control systems
Document ID
19690048527
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Athans, M.
Debs, A. S.
Date Acquired
August 5, 2013
Publication Date
February 1, 1969
Subject Category
Electronics
Accession Number
69A26516
Funding Number(s)
CONTRACT_GRANT: NGR-22-009/124/
Distribution Limits
Public
Copyright
Other

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