Solar Radiation Pressure Effects on Stability of Periodic Orbits in Restricted Four-Body Problem

M. Ismail, A. H. Ibrahim, A. Zaghrout, S. H. Younis, F. S. Elmalky, L. E. Elmasry
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引用次数: 1

Abstract

In this work, the Hamiltonian of the four-body problem is considered under the effects of solar radiation pressure. The equations of motion of the infinitesimal body are obtained in the Hamiltonian canonical form. The libration points and the corresponding Jacobi constants are obtained with different values of the solar radiation pressure coefficient. The motion and its stability about each point are studied. A family of periodic orbits under the effects of the gravitational forces of the primaries and the solar radiation pressure are obtained depending on the pure numerical method. This purpose is applied to the Sun-Earth-Moon-Space craft system, and the results obtained are in a good agreement with the previous work such as (Kumari and Papadouris, 2013).
太阳辐射压力对受限四体问题周期轨道稳定性的影响
本文考虑了太阳辐射压力作用下的四体问题的哈密顿量。以哈密顿正则形式得到了无穷小物体的运动方程,得到了太阳辐射压力系数不同时的平动点和相应的雅可比常数。研究了每个点的运动及其稳定性。根据纯数值方法,得到了一组在初引力和太阳辐射压力作用下的周期轨道。这一目的被应用于日地月航天器系统,所获得的结果与之前的工作(Kumari和Papadouris,2013)非常一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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