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Orbit prediction accuracy theoryEquations for estimating orbit prediction accuracy theory, with partial derivatives calculated from two-body elliptical orbit theory
Document ID
19660022729
Acquisition Source
Goddard Space Flight Center
Document Type
Other
Authors
H E Montgomery (Goddard Space Flight Center Greenbelt, United States)
R C Blanchard (Goddard Space Flight Center Greenbelt, United States)
F Whitlock (Goddard Space Flight Center Greenbelt, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1963
Publication Information
Publication: Publications of Goddard Space Flight Center, 1963 Volume I - Space Sciences
Publisher: National Aeronautics and Space Administration
Subject Category
Space Sciences
Accession Number
66N32019
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ORBIT EQUATION
PREDICTION THEORY
TWO-BODY ORBIT
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IDRelationTitle19660022716Collected WorksPublications of Goddard Space Flight Center, 1963 Volume I - Space sciences19660022716Collected WorksPublications of Goddard Space Flight Center, 1963 Volume I - Space sciencesN66-32006 18-30Collected Works
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