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Computer program trajectory optimization by explicit numerical methodsComputer program using numerical methods that calculates minimum time for space vehicle to meet its mission with optimum trajectory, and can maximize option if burning time is fixed
Document ID
19670008304
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hilliard, J. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
December 8, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-53552
Report Number: NASA-TM-X-53552
Accession Number
67N17633
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMPUTER PROGRAM
NUMERICAL INTEGRATION
TRAJECTORY OPTIMIZATION
BURNING RATE

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