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地月低能轨道转移的混沌控制方法
引用本文:郑越,泮斌峰,唐硕. 地月低能轨道转移的混沌控制方法[J]. 宇航学报, 2018, 39(7): 751-759. DOI: 10.3873/j.issn.1000-1328.2018.07.006
作者姓名:郑越  泮斌峰  唐硕
作者单位:1. 西北工业大学航天学院,西安 710072;2. 陕西省空天飞行器设计重点实验室,西安 710072
基金项目:国家自然科学基金(11672234)
摘    要:针对航天器在混沌区域的滑行时间过长,提出一种低能地月轨道转移的混沌控制方法。首先通过地月圆形限制性三体问题(CRTBP)的庞加莱截面图,将混沌区域进行分层并分析其规律,再利用混沌轨道对初始状态高度敏感的特性,在尽可能减少运送时间的前提下实现地月低能轨道转移。该方法的优点是利用混沌区域的固有规律,不需要依靠周期轨道特性。仿真结果表明,本文提出方法仅需施加2~4次脉冲,明显缩短混沌区域的滑行时间,从而实现地月低能转移。

关 键 词:庞加莱截面  混沌  混沌控制  圆形限制性三体问题  轨道转移  
收稿时间:2017-10-12

Chaos Control Method of Earth Moon Low Energy Orbit Transfer
ZHENG Yue,PAN Bin feng,TANG Shuo. Chaos Control Method of Earth Moon Low Energy Orbit Transfer[J]. Journal of Astronautics, 2018, 39(7): 751-759. DOI: 10.3873/j.issn.1000-1328.2018.07.006
Authors:ZHENG Yue  PAN Bin feng  TANG Shuo
Affiliation:1. School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China; 2. Shanxi Key Laboratory of Aerospace Flight Vehicle Design, Xi’an 710072, China
Abstract:A new chaos control method of Earth-Moon orbit transfer is proposed to reduce the transfer time of a spacecraft wandering in the chaotic region. Considering the circular restricted three-body problem (CRTBP), the chaotic region is divided into several layers according to the Poincaré section map, and the rules of each layer are analyzed. Besides, the properties that the chaotic orbit is highly sensitive to the initial conditions are fully utilized, and the chaotic orbits are constructed to meet the requirement of minimizing the transfer time. The proposed method takes advantage of the rules in the chaotic region, which is not necessary to rely on the location of the periodic orbits. Finally, the numerical results are provided to reveal that the transport time in the chaotic region can be significantly reduced with only 2-4 impulses.
Keywords:Poincaré  section  Chaos  Chaos control  Circular restricted three body problem  Orbit transfer  
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