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A general method for selection and optimization of trajectories.Space mission trajectory optimization by iterative minimizing of residual vector, using linear correction
Document ID
19650051003
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Campbell, J.
Moore, W. E.
Wolf, H.
Date Acquired
August 2, 2013
Publication Date
September 1, 1965
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 65-697
Report Number: AIAA PAPER 65-697
Accession Number
65A33707
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT TRAJECTORY
ITERATIVE SOLUTION
TRAJECTORY OPTIMIZATION

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