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Analytic short period lunar and solar perturbations of artificial satellites.The short period luni-solar theory of Kozai is generalized for arbitrary obliquity of the ecliptic and inclination of the moon's orbit to the ecliptic. Analytic first order lunar perturbations to the elements are derived. The theory is illustrated by an application to the communication satellite Intelsat 3F3.
Document ID
19730038111
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Fisher, D.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Date Acquired
August 7, 2013
Publication Date
December 1, 1972
Publication Information
Publication: Celestial Mechanics
Volume: 6
Subject Category
Space Sciences
Accession Number
73A22913
Distribution Limits
Public
Copyright
Other

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