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Near-optimum guidance - an analysis of fuel penaltyNear-optimum guidance and analysis of fuel penalty - explicit solution of linear equations of motion to obtain deviations in end conditions and additional burning time
Document ID
19650025827
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dickey, L. R. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
April 23, 1965
Subject Category
Navigation
Report/Patent Number
NASA-TM-X-53249
Report Number: NASA-TM-X-53249
Accession Number
65N35428
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LINEAR EQUATION
FUEL
GUIDANCE
MOTION EQUATION

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