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A trajectory optimization technique based upon the theory of the second variationApproximation method using Euler-Lagrange equation for trajectory optimization
Document ID
19650026535
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kelley, H. J. (ANAL. MECH. ASSOCIATES, INC.)
Kopp, R. E. (Grumman Aircraft Engineering Corp. Bethpage, NY, United States)
Moyer, H. G. (Grumman Aircraft Engineering Corp. Bethpage, NY, United States)
Date Acquired
August 2, 2013
Publication Date
July 1, 1964
Subject Category
Space Sciences
Report/Patent Number
RE-177J
NASA-CR-67576
Report Number: RE-177J
Report Number: NASA-CR-67576
Accession Number
65N36136
Funding Number(s)
CONTRACT_GRANT: AF 49/638/-1207
CONTRACT_GRANT: NAS9-1147
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRAJECTORY OPTIMIZATION
EULER-LAGRANGE EQUATION
APPROXIMATION METHOD

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