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关于共线平动点的特征及其在深空探测中的应用
引用本文:刘林,侯锡云,王海红. 关于共线平动点的特征及其在深空探测中的应用[J]. 天文学进展, 2006, 24(2): 174-182
作者姓名:刘林  侯锡云  王海红
作者单位:南京大学,天文系,南京,210093;南京大学,空间环境与航天动力学研究所,南京,210093
基金项目:国家自然科学基金重大国际合作资助项目(10073009)
摘    要:系统阐述了小天体运动对应的圆型限制性三体问题共线平动点的强不稳定性特征,以及其附近的条件周期轨道——晕轨道(Halo Orbit)的存在、相应解的构造。这种特殊的轨道形式和共线平动点附近的弱稳定走廊,可分别用于在深空特殊位置附近定点有各种科学探测目标的探测器和向节能轨道过渡的通道。

关 键 词:天体力学  共线平动点  航天器轨道力学  深空探测  晕轨道  引力加速
文章编号:1000-8349(2006)01-0174-09
收稿时间:2005-10-08
修稿时间:2005-10-082005-11-20

Their Applications in Deep Space Exploration
LIU Lin,HOU Xi-yun,WANG Hai-hong. Their Applications in Deep Space Exploration[J]. Progress In Astronomy, 2006, 24(2): 174-182
Authors:LIU Lin  HOU Xi-yun  WANG Hai-hong
Affiliation:1. Astronomy Department, Nanjing University, Nanjing 210093, China; 2. Institute of Space Environment and Astronautics, Nanjing Univerity, Nanjing 210093, China
Abstract:In this paper we give a systematic formulation of the special position and strongly unstable dynamical characteristics of the coilinear libration points of the Circular Restricted Three-Body Problem which is useful in the study of motion of small bodies. We state t he possibility of existence of conditionally periodic orbits (Halo Orbits) and give out these orbits. including lower order solutions and higher order solutions. These special periodic orbits can be used as nominal orbits for kinds of spacecrafts with different scientific goals. while the weak stability corridors associated with the coilinear libration points can be used as ones for spacecrafts with less fuel demand.
Keywords:celestial mechanics  collinear libration point  spacecraft orbit dynamics  deep space exploration  Halo Orbit  gravity assist
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