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Application of a finite-difference Newton- Raphson algorithm to problems of low-thrust trajectory optimization.Low thrust trajectory optimization, using Newton- Raphson method to solve nonlinear two-point boundary value problem
Document ID
19660056614
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Edelbaum, T. N.
Fimple, W. R.
Van Dine, C. P.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 65-698
Report Number: AIAA PAPER 65-698
Accession Number
66A35904
Funding Number(s)
CONTRACT_GRANT: NAS8-11309
Distribution Limits
Public
Copyright
Other
Keywords
TRAJECTORY OPTIMIZATION
BOUNDARY VALUE
NEWTON-RAPHSON METHOD
HOHMANN ORBITAL TRANSFER
NONLINEAR EQUATION

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