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The utilization of an impulsive solution in solving optimum trajectory problems with bounded thrust magnitudeImpulsive solution used to solve optimum trajectory problems with bounded thrust magnitude
Document ID
19670021353
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Jezewski, D. J.
Date Acquired
September 2, 2013
Publication Date
July 1, 1967
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-4059
Report Number: NASA-TN-D-4059
Accession Number
67N30682
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRAJECTORY OPTIMIZATION
THRUST POWER
VARIATIONAL CALCULUS

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