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Computation of optimal interplanetary low- thrust trajectories with bounded thrust magnitude by means of the generalized newton- raphson methodComputation of optimal interplanetary low thrust trajectories, orbital transfer problems by means of generalized Newton-Raphson method
Document ID
19650023461
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kenneth, P. (Grumman Aircraft Engineering Corp. Bethpage, NY, United States)
Taylor, G. E. (Grumman Aircraft Engineering Corp. Bethpage, NY, United States)
Date Acquired
August 2, 2013
Publication Date
July 12, 1965
Subject Category
Space Sciences
Accession Number
65N33062
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMPUTATION
INTERPLANETARY TRAJECTORY
NEWTON-RAPHSON METHOD
TRAJECTORY OPTIMIZATION
ORBITAL TRANSFER
LOW THRUST PROPULSION
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