A simple intermediary orbit for the J2 problem

被引：2

作者：

Oberti, P ^{[1
]}

机构：

[1] Observ Cote Azur, F-06304 Nice, France

来源：

ASTRONOMY & ASTROPHYSICS | 2005年 / 437卷 / 01期

关键词：

planets and satellites : general; celestial mechanics;

D O I：

10.1051/0004-6361:20042406

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

A simple precessing ellipse suitable for satellites with moderate eccentricities and inclinations is built in the Hamiltonian context of the J(2) problem. Easy to use as a first intermediary orbit, it provides a substantially closer starting point for series expansions than the regular Keplerian ellipse.

引用

页码：333 / 338

页数：6

共 7 条

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Floria, Luis
[J]. CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 1993, 57 (1-2) : 203 - 223
[5] HENRARD J, 1989, MODERN METHODS CELES
[6] NON INTEGRABILITY OF THE J(2) PROBLEM
Irigoyen, Maylis
Simo, Carles
[J]. CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 1993, 55 (03) : 281 - 287
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