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Sun-perturbed dynamics of a particle in the vicinity of the Earth-Moon triangular libration points.

机译:太阳在月亮-月亮三角形解放点附近的扰动动力学。

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摘要

This study focuses on the Sun's influence on the motion near the triangular libration points of the Earth-Moon system. It is known that there exists a very strong resonant perturbation near those points that produces large deviations from the libration points, with an amplitude of about 250,000 km and a period of 1,500 days. However, it has been shown that it is possible to find initial conditions that negate the effects of that perturbation, even resulting in stable, although very large, periodic orbits. Using two different models, the goal of this research is to determine the initial configurations of the Earth-Moon-Sun system that produce minimal deviations from the libration points, and to provide a better understanding of the dynamics of this highly nonlinear problem.;First, the Bicircular Problem (BCP) is considered, which is an idealized model of the Earth-Moon-Sun System. The impact of the initial configuration of the Earth-Moon-Sun system is studied for various propagation times and it is found that there exist two initial configurations that produce minimal deviations from L4 or L 5. The resulting trajectories are very sensitive to the initial configuration, as the mean deviation from the libration points can decrease by 30,000 km with less than a degree change in the initial configuration. Two critical initial configurations of the system were identified that could allow a particle to remain within 30,000 km of the libration points for as long as desired.;A more realistic model, based on JPL ephemerides, is also used, and the influence of the initial epoch on the motion near the triangular points is studied. Through the year 2007, 51 epochs are found that produce apparently stable librational motion near L4, and 60 near L5. But the motion observed depends greatly on the initial epoch. Some epochs are even found to significantly reduce the deviation from L4 and L5, with the spacecraft remaining within at most 90,000 km from the triangular points for upwards of 3,000 days. Similarly to what was observed in the BCP, these trajectories are found to be extremely sensitive to the initial epoch.
机译:这项研究的重点是太阳对月球地球系统三角形释放点附近运动的影响。众所周知,在那些点附近有一个非常强烈的共振扰动,它与解放点产生很大的偏差,其振幅约为250,000 km,周期为1,500天。但是,已经表明,有可能找到抵消这种扰动影响的初始条件,甚至可以产生稳定的,尽管很大的周期性轨道。本研究的目的是使用两个不同的模型来确定“地球-月亮-太阳”系统的初始配置,以使它们与解离点的偏差最小,并更好地理解这一高度非线性问题的动力学。 ,考虑了双圆问题(BCP),它是Earth-Moon-Sun系统的理想模型。研究了地球-月亮-太阳系统初始配置对各种传播时间的影响,发现存在两个初始配置,它们与L4或L 5的偏差最小。结果轨迹对初始配置非常敏感,因为与初始点的角度变化相比,偏离解放点的平均偏差可以减少30,000 km。确定了系统的两个关键初始配置,这些初始配置可以使粒子保持在离释放点30,000 km的范围内长达所需的时间。;还使用了基于JPL星历表的更现实的模型,并且研究了三角点附近运动的历元。到2007年,发现在L4附近产生明显稳定的自由运动的51个时期,在L5附近产生60个稳定的自由运动。但是观察到的运动很大程度上取决于初始时期。甚至发现某些时期会大大减少与L4和L5的偏离,航天器距三角点的距离最多不超过90,000 km,长达3,000天以上。与在BCP中观察到的相似,发现这些轨迹对初始时期极为敏感。

著录项

  • 作者

    Munoz, Jean-Philippe.;

  • 作者单位

    The University of Texas at Austin.;

  • 授予单位 The University of Texas at Austin.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2008
  • 页码 175 p.
  • 总页数 175
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

  • 入库时间 2022-08-17 11:38:45

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