Orbit's Structure in the Isosceles Rectilinear Restricted Three-Body Problem

被引：0
|
作者：
J. Martínez Alfaro
R. B. Orellana
机构：
[1] Universitat de València,Department de Matemàtica Aplicada i Astronomia
[2] Observatorio Astgronómico de La Plata,CONICET (Profoeg)
来源：
Celestial Mechanics and Dynamical Astronomy | 1997年 / 67卷
关键词：
Manifold; Invariant Manifold; Celestial Mechanics; Triple Collision; Collision Orbit;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The isosceles rectilinear restricted three-body problem can be considered as the Sitnikov's problem with eccentricity one or, as the isosceles problem when the central mass is zero and the primaries move having consecutive elliptic collisions. We compactify the phase space and analyze the flow on their boundary. This allows us to separate the phase space into different regions depending on the kind of orbits.
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页码：275 / 291
页数：16
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