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Research goals and an integrated approachCelestial mechanics, astrodynamics, optimization theory, and onboard computations research for trajectory analyses of space flight vehicles
Document ID
19660030100
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hoelker, R. F. (NASA Electronics Research Center Cambridge, MA, United States)
Date Acquired
August 3, 2013
Publication Date
November 17, 1965
Subject Category
Navigation
Accession Number
66N39390
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPACE FLIGHT
ONBOARD NAVIGATION
CELESTIAL MECHANICS
COMPUTER METHOD
TRAJECTORY ANALYSIS

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