期刊文献+

圆型限制性三体问题的动力学特征

Dynamics characteristics of circular restricted three-body problem
下载PDF
导出
摘要 禁行域在圆型限制性三体问题中对第三体的运动有极为重要的影响.利用零速度曲线讨论天体禁行域与系统参数之间的关系.禁行域与雅可比常数有关,且能影响天体的运动区域和轨道构型.利用最大李雅普诺夫指数寻找该模型的混沌轨道,给出混沌轨道在不同系统参数下随天体初始位置的分布.这些分布说明,当第三天体从两主天体连线的中点处释放时,容易产生混沌运动;当质量参量足够小时,体系无法产生混沌现象. The forbidden zone has a significantly important influence on the motion of the third body in the circular restricted three-body problem.Based on zero-velocity curves,the relationship between the forbidden zone of celestial bodies and dynamical parameters was discussed.It was obtained that the forbidden zones are related to the Jacobian constant,and can affect motion areas of celestial bodies and dynamical types of orbits.The maximum Lyapunov exponents were used to find chaotic orbits,and the distributions of chaotic orbits with respect to the initial positions of the celestial bodies for different dynamical parameters were given.These distributions indicate that when the third celestial body is released from the midpoint of the two main celestial bodies,chaos easily occurs.However,there is no chaos when the mass parameter is small sufficiently.
作者 刘文芳 胡诗杨 刘福窑 LIU Wenfang;HU Shiyang;LIU Fuyao(School of Mathematics,Physics and Statistics,Shanghai University of Engineering Science,Shanghai 201620,China;School of Physical Science and Technology,Guangxi University,Nanning 530004,China)
出处 《上海工程技术大学学报》 CAS 2021年第3期272-280,共9页 Journal of Shanghai University of Engineering Science
基金 国家自然科学基金资助项目(U2031145) 上海工程技术大学科普专项资助项目(KP2105)。
关键词 限制性三体问题 哈密顿系统 数值模拟 轨道 混沌 restricted three-body problem Hamiltonian system numerical simulation orbit chaos
  • 相关文献

参考文献6

二级参考文献33

  • 1刘林,侯锡云.深空探测器运行轨道的基本性态[J].飞行器测控学报,2009,28(2):1-8. 被引量:2
  • 2张燕,荆武兴.基于日地月方位信息的月球卫星自主导航[J].宇航学报,2005,26(4):495-498. 被引量:7
  • 3匙玉华,刘学深,丁培柱.啁啾激光场中HF分子的经典解离[J].物理学报,2006,55(12):6320-6325. 被引量:5
  • 4罗香怡,刘学深,丁培柱.立方非线性Schrdinger方程的动力学性质研究及其解模式的漂移[J].物理学报,2007,56(2):604-610. 被引量:8
  • 5Farquhar R W, Dunham D W, Guo Y, et al. Utilization of li bration points for human exploration in the Sun-Earth-Moon system and beyond[J]. Acta Astronautica, 2004, 55 (3): 687-700.
  • 6Atessi E M, G6mez G, Masdemont J J. Leaving the Moon by means of invariant manifolds of libration point orbits [J]. Communications in Nonlinear Science and Numerical Simula- tions, 2009, 14(12): 4153-4167.
  • 7Parker J S, Born G H. Direct lunar halo orbit transfers[J]. The Journal of the Astronautical Sciences, 2008, 56 (4): 441-476. P.
  • 8arker J S. Families of low-energy lunar halo transfers[C]// AAS/AIAA Spaceflight Dynamics Conference. Keystone, Colorado, 2006.
  • 9Li M, Zheng J. Indirect transfer to the Earth-Moon L1 libra- tion point[J]. Celestial Mechanics and Dynamical Astrono- my, 2010, 108(2): 203 213.
  • 10Szebehely V. Theory of orbits: the restricted problem of three bodies[M]. New York: Academic Press, 1967: 13-22.

共引文献24

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部