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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
Legacy CDMS
Document Type
Other
Authors
Blanchard, R. C.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Montgomery, H. H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Whitlock, F.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1963
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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