首页> 外文会议>AAS/AIAA Space Flight Mechanics Meeting Feb 11-15, 2001, Santa Barbara, California >EQUILIBRIUM CONFIGURATIONS OF TETHERED THREE-BODY SYSTEMS AND THEIR STABILITY
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EQUILIBRIUM CONFIGURATIONS OF TETHERED THREE-BODY SYSTEMS AND THEIR STABILITY

机译:三体系统的平衡构型及其稳定性

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The paper considers planar motion of a three-body tethered system whose center of mass moves in a circular orbit around the Earth. The equilibrium configurations of the system and their stability are examined. It is observed that there are four classes of equilibrium configurations of tethered three-body systems: in two of them the bodies are collinear, while in the other two, the bodies lie in a triangular configuration. Analysis of the stability of these equilibrium configurations shows that the triangular configurations are unstable, while one of the collinear configurations (the one along the local vertical) is stable. An integral of motion is obtained, which turns out to be the Hamiltonian of the system per unit mass. The zero-velocity curves based on this Hamiltonian are presented.
机译:本文考虑了一个三体系留系统的平面运动,该系统的质心沿地球的圆形轨道运动。检查系统的平衡构型及其稳定性。可以观察到,系留三体系统的平衡构型有四类:在其中两种体中共线,而在另两种中,体处于三角形构型。对这些平衡构型的稳定性分析表明,三角形构型是不稳定的,而共线构型之一(沿局部垂直方向的一种)是稳定的。获得运动积分,结果是单位质量的系统的哈密顿量。给出了基于该哈密顿量的零速度曲线。

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