Analytic short period lunar and solar perturbations of artificial satellites View Full Text


Ontology type: schema:ScholarlyArticle      Open Access: True


Article Info

DATE

1972-12

AUTHORS

David Fisher

ABSTRACT

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.

PAGES

447-467

Identifiers

URI

http://scigraph.springernature.com/pub.10.1007/bf01227758

DOI

http://dx.doi.org/10.1007/bf01227758

DIMENSIONS

https://app.dimensions.ai/details/publication/pub.1013514405


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