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Minimax control of large launch boostersOptimal control theory applied to piecewise constant approximation of large launch booster for first 84 seconds of flight
Document ID
19660022567
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Graham, K. D. (Honeywell, Inc. Saint Paul, MN, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1966
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-546
Report Number: NASA-CR-546
Accession Number
66N31857
Funding Number(s)
CONTRACT_GRANT: NAS8-11206
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
OPTIMAL CONTROL
LAUNCH VEHICLE

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