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Ejection-Collision orbits in the symmetric collinear four-body problem

机译:对称共线四体问题中的弹射轨道

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In this paper, we consider the collinear symmetric four-body problem, where four masses m(3) = alpha, m(1) = 1, m(2) = 1, and m(4) = alpha, alpha 0, are aligned in this order and move symmetrically about their center of mass. We introduce regularized variables to deal with binary collisions as well as McGehee coordinates to study the quadruple collision manifold for a negative value of the energy. The paper is mainly focused on orbits that eject from (or collide to) quadruple collision. The problem has two hyperbolic equilibrium points, located in the quadruple collision manifold. We use high order parametrizations of their stable/unstable manifolds to devise a numerical procedure to compute ejection-collision orbits, for any value of alpha. Some results from the explorations done for alpha = 1 are presented. Furthermore, we prove the existence of ejection-direct escape orbits, which perform a unique type of binary collisions. (C) 2018 Elsevier B.V. All rights reserved.
机译:在本文中,我们考虑共线对称四体问题,其中四个质量m(3)= alpha,m(1)= 1,m(2)= 1,m(4)= alpha,alpha> 0,按此顺序对齐并围绕其质心对称移动。我们引入正则化变量来处理二进制碰撞以及McGehee坐标,以研究四重碰撞流形的负能量。本文主要关注从四重碰撞弹出(或碰撞到四重碰撞)的轨道。该问题有两个双曲平衡点,位于四重碰撞流形中。我们使用它们的稳定/不稳定流形的高阶参数化来设计一个数值程序,以计算任何α值的喷射碰撞轨道。提出了一些针对alpha = 1进行的探索的结果。此外,我们证明了执行直接类型的二元碰撞的直接射出逃逸轨道的存在。 (C)2018 Elsevier B.V.保留所有权利。

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