Periodic orbits of a collinear restricted three-body problem

被引：21
|
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
收藏
页码：163 / 183
页数：21
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