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A dynamic programing analysis of multiple guidance corrections of a trajectory.Adaptive guidance correction policy developed from dynamic programming point of view for perturbed trajectory of spacecraft
Document ID
19650053768
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Pfeiffer, C. G.
Date Acquired
August 2, 2013
Publication Date
September 1, 1965
Subject Category
Navigation
Accession Number
65A36472
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT TRAJECTORY
DYNAMIC PROGRAMMING
GUIDANCE AND CONTROL
OPTIMUM THRUST PROGRAMMING
TRAJECTORY CONTROL

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