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Trajectory optimization by steepest ascent methodSteepest ascent method for trajectory optimization based on minimum time and maximum velocity of fuel flow rate
Document ID
19670024054
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cunningham, E. P.
Date Acquired
August 3, 2013
Publication Date
March 1, 1967
Subject Category
Space Sciences
Accession Number
67N33383
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STEEPEST ASCENT METHOD
TRAJECTORY OPTIMIZATION
FUEL FLOW
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