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A trajectory optimization technique based upon the theory of the second variation.Optimization of trajectory achieved by successive approximation method based on second variation theory
Document ID
19640040321
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kelley, H. J.
Kopp, R. E.
Moyer, H. G.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Space Radiation
Report/Patent Number
AIAA PAPER 63-415
Report Number: AIAA PAPER 63-415
Accession Number
64A26214
Funding Number(s)
CONTRACT_GRANT: AF 49/638/-1207
CONTRACT_GRANT: NAS9-1147
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT TRAJECTORY
VARIATION METHOD
TRAJECTORY CONTROL

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