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Application of Optimal Control Theory to Launch Vehicles Final Technical ReportApplication of optimal control theory to design of launch vehicle attitude control systems
Document ID
19680024178
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Harvey, C. A. (Honeywell, Inc. Saint Paul, MN, United States)
Date Acquired
August 4, 2013
Publication Date
July 1, 1968
Subject Category
Electronics
Report/Patent Number
REPT.-12073-FR1
NASA-CR-61939
Report Number: REPT.-12073-FR1
Report Number: NASA-CR-61939
Accession Number
68N33650
Funding Number(s)
CONTRACT_GRANT: NAS8-21063
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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