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On determining the secular and critical effects in the motion of satellites by means of a nonsingular set of vectorial elementsCombination of Halphen and Liouville methods for determining secular and critical effects in satellite orbit behavior
Document ID
19660022730
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Musen, P.
(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
66N32020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SATELLITE ORBIT
HALPHEN METHOD
LIOUVILLE EQUATION
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