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Analytic short period lunar and solar perturbations of artificial satellites

Author
Fisher, D.
Published
Mar 1, 1972.
Physical Description
1 electronic document
Online Version

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Summary
A short period luni-solar theory was generalized for application to arbitrary obliquity of the ecliptic and inclination of the moon's orbit to the ecliptic. Analytic first order lunar perturbations to the elements were derived. The theory is illustrated by an application to the communication satellite Intelsat 3F3.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19720016238.
Accession ID: 72N23888.
NASA-TM-X-65869.
X-552-72-83.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15946800