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Analytical linear perturbation theory for highly eccentric satellite orbits
Authors:Eugene Brumberg  Victor A. Brumberg  Thomas Konrad  Michael Soffel
Affiliation:(1) Institute of Applied Astronomy, 197042 St.-Petersburg, Russia;(2) Theoret. Astrophysics, University of Tübingen, 72076 Tübingen, FRG
Abstract:
Kaula's satellite linear perturbation theory has been extended for the case of highly eccentric orbits by using elliptic function expansions.On leave from Institute of Applied Astronomy, St.-Petersburg
Keywords:Satellite motion  Kaula's theory  elliptic anomaly
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