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Control System Optimization for Saturn 5 Launch Vehicles Using Gradient Techniques Final ReportControl system optimization for Saturn 5 launch vehicles using gradient techniques
Document ID
19700020370
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Connor, C. L. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Trautwein, W. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
August 5, 2013
Publication Date
February 1, 1970
Subject Category
Navigation
Report/Patent Number
HREC-0515-1
LMSC/HREC-D162122-I
NASA-CR-102712
Report Number: HREC-0515-1
Report Number: LMSC/HREC-D162122-I
Report Number: NASA-CR-102712
Accession Number
70N29680
Funding Number(s)
CONTRACT_GRANT: NAS8-30515
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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