Approximate analytical theory of satellite orbit prediction presented in spherical coordinates frame / Alimov G., Greb A., Kuznetsov E., Polyakhova E. // Celestial Mechanics and Dynamical Astronomy. - 2001. - V. 81, l. 3. - P. 219-234.

ISSN:
09232958
Type:
Article
Abstract:
A comparative review of analytic theories for the motion of Earth satellites in quasicircular orbits written in the spherical coordinate frame is presented. The theory of motion is developed for satellites in quasi-circular and quasi-equatorial orbits subjected to geopotential, luni-solar and solar radiation pressure force perturbations. The intermediate orbit is Keplerian and the equations of motion are solved by the Lyapunov-Poincaré small parameter method. Both resonant and non-resonant cases are considered. The results can be useful for the development of a complete theory of weakly eccentric orbits.
Author keywords:
Earth satellite motion; Geostationary satellite; Intermediate orbit; Resonance
Index keywords:
нет данных
DOI:
10.1023/A:1013252917957
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Affiliations Astronomical Institute, St. Petersburg University, Stary Peterhof, 198504 St. Petersburg, Russian Federation; Department of Astronomy and Geodesy, Ural State University, Lenin ave. 51, 620083 Ekaterinburg, Russian Federation
Author Keywords Earth satellite motion; Geostationary satellite; Intermediate orbit; Resonance
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Correspondence Address Kuznetsov, E.; Department of Astronomy and Geodesy, Ural State University, Lenin ave. 51, 620083 Ekaterinburg, Russian Federation; email: eduard.kuznetsov@usu.ru
Language of Original Document English
Abbreviated Source Title Celest. Mech. Dyn. Astron.
Source Scopus