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A TRAJECTORY OPTIMIZATION TECHNIQUE BASED UPON THE THEORY OF THE SECOND VARIATIONOptimization of a trajectory is achieved by a successive approximation method based on the second variation theory
Document ID
19630025670
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Kelly, H. J.
Kopp, R. E.
Moyer, H. G.
Date Acquired
August 1, 2013
Publication Date
August 21, 1963
Subject Category
Space Radiation
Report/Patent Number
AIAA PAPER 63-415
Report Number: AIAA PAPER 63-415
Accession Number
63A21729
Funding Number(s)
CONTRACT_GRANT: AF 49/638/-1207
CONTRACT_GRANT: NAS9-1147
Distribution Limits
Public
Copyright
Other
Keywords
TRAJECTORY CONTROL
SPACECRAFT TRAJECTORY
VARIATION METHOD

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