Periodic orbits of a collinear restricted three-body problem

被引：22

作者：

Corbera, M

Llibre, J

机构：

[1] Univ Vic, Dept Informat & Matemat, Escola Poltecn Super, E-08500 Barcelona, Spain

[2] Univ Autonoma Barcelona, Dept Matemat, E-08193 Barcelona, Spain

来源：

CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY | 2003年 / 86卷 / 02期

关键词：

periodic orbits; collinear restricted three-body problem; analytic continuation method;

D O I：

10.1023/A:1024183003251

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

In this paper we study symmetric periodic orbits of a collinear restricted three-body problem, when the middle mass is the largest one. These symmetric periodic orbits are obtained from analytic continuation of symmetric periodic orbits of two collinear two-body problems.

引用

页码：163 / 183

页数：21

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