Trajectory and stability of Lagrangian point L2 in the Sun-Earth system

被引：6
|
作者：
Kushvah, Badam Singh [1 ]
机构：
[1] Indian Sch Mines, Dept Appl Math, Dhanbad 826004, Jharkhand, India
来源：
ASTROPHYSICS AND SPACE SCIENCE | 2011年 / 332卷 / 01期
关键词：
Trajectory; Stability; Radiation pressure; Rtbp; Celestial mechanics; RESTRICTED 3-BODY PROBLEM; CHERMNYKH-LIKE PROBLEMS; EQUILIBRIUM POINTS; LINEAR-STABILITY; MASS;
D O I：
10.1007/s10509-010-0493-9
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
This paper describes design of the trajectory and analysis of the stability of collinear point L-2 in the Sun-Earth system. The modified restricted three body problem with additional gravitational potential from the belt is used as the model for the Sun-Earth system. The effect of radiation pressure of the Sun and oblate shape of the Earth are considered. The point L-2 is asymptotically stable up to a specific value of time t correspond to each set of values of parameters and initial conditions. The results obtained from this study would be applicable to locate a satellite, a telescope or a space station around the point L-2.
引用
收藏
页码：99 / 106
页数：8
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