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Implementation of an optimal adaptive guidance mode.Multivariate function approximation as basis of adaptive control systems for space flight
Document ID
19650033385
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Vance, R. J.
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Navigation
Report/Patent Number
AIAA PREPRINT 63-417
Report Number: AIAA PREPRINT 63-417
Accession Number
65A16089
Funding Number(s)
CONTRACT_GRANT: NAS8-2607
Distribution Limits
Public
Copyright
Other
Keywords
ADAPTIVE CONTROL SYSTEM
NUMERICAL INTEGRATION
OPTIMAL CONTROL
ADAPTIVE CONTROL

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