Analytical linear perturbation theory for highly eccentric satellite orbits View Full Text


Ontology type: schema:ScholarlyArticle     


Article Info

DATE

1995-12

AUTHORS

Eugene Brumberg, Victor A. Brumberg, Thomas Konrad, Michael Soffel

ABSTRACT

Kaula's satellite linear perturbation theory has been extended for the case of highly eccentric orbits by using elliptic function expansions.

PAGES

369-387

References to SciGraph publications

  • 1971. Handbook of Elliptic Integrals for Engineers and Scientists in NONE
  • 1979-11. Note on Lagrange's inversion formula in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1994-09. Expansions of elliptic motion based on elliptic function theory in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1971-06. Analytical methods for the orbits of artificial satellites of the Moon in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • Journal

    Author Affiliations

    Identifiers

    URI

    http://scigraph.springernature.com/pub.10.1007/bf00049516

    DOI

    http://dx.doi.org/10.1007/bf00049516

    DIMENSIONS

    https://app.dimensions.ai/details/publication/pub.1024678044


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