Approximate analytical theory of satellite orbit prediction presented in spherical coordinates frame / Alimov G,Greb A,Kuznetsov E,Polyakhova E // CELESTIAL MECHANICS \& DYNAMICAL ASTRONOMY. - 2001. - V. 81, l. 3. - P. 219-234.

ISSN/EISSN:

0923-2958 / нет данных

Type:

Article

Abstract:

A comparative review of analytic theories for the motion of Earth satellites in quasi-circular 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-Poincare 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; intermediate orbit; resonance; geostationary satellite PERTURBED CIRCULAR MOTION; 1ST-ORDER

DOI:

10.1023/A:1013252917957

Web of Science ID:

ISI:000173685100003

Соавторы в МНС:

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Другие поля

Поле	Значение
Publisher	KLUWER ACADEMIC PUBL
Address	VAN GODEWIJCKSTRAAT 30, 3311 GZ DORDRECHT, NETHERLANDS
Language	English
Keywords-Plus	PERTURBED CIRCULAR MOTION; 1ST-ORDER
Research-Areas	Astronomy \& Astrophysics; Mathematics
Web-of-Science-Categories	Astronomy \& Astrophysics; Mathematics, Interdisciplinary Applications
Number-of-Cited-References	22
Usage-Count-Since-2013	2
Journal-ISO	Celest. Mech. Dyn. Astron.
Doc-Delivery-Number	518TZ