首页> 外文期刊>Celestial Mechanics and Dynamical Astronomy: An international journal of space dynamics >A new perturbative solution to the motion around triangular Lagrangian points in the elliptic restricted three-body problem
【24h】

A new perturbative solution to the motion around triangular Lagrangian points in the elliptic restricted three-body problem

机译:椭圆局限制三体问题三角拉格朗日点围绕三角拉格朗日点运动的新扰动解决方案

获取原文
获取原文并翻译 | 示例
           

摘要

The equations of motion of the planar elliptic restricted three-body problem are transformed to four decoupled Hill's equations. By using the Floquet theorem, a perturbative solution to the oscillator equations with time-dependent periodic coefficients are presented. We clarify the transformation details that provide the applicability of the method. The form of newly derived equations inherently comprises the stability boundaries around the triangular Lagrangian points. The analytic approach is valid for system parameters 0 < e <= 0.05 and 0 < mu <= 0.01 where e denotes the eccentricity of the primaries, while mu is the mass parameter. Possible application to known extrasolar planetary systems is also demonstrated.
机译:None

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号