Regularization of circular restricted three-body problem accounting radiation pressure and oblateness

被引:9
|
作者
Srivastava, Vineet K. [1 ,2 ]
Kumar, Jai [3 ]
Kushvah, Badam Singh [2 ]
机构
[1] ISRO Telemetry Tracking & Command Network, Flight Dynam Grp, Bangalore 560058, Karnataka, India
[2] Indian Sch Mines Dhanbad, Indian Inst Technol, Dept Appl Math, Dhanbad 826004, Bihar, India
[3] ISRO Satellite Ctr, Mission Dev Grp, Bangalore 560017, Karnataka, India
关键词
Three-body problem; Solar radiation; Oblate spheroid; Regularization; SUN-EARTH SYSTEM; HALO ORBITS; POINTS;
D O I
10.1007/s10509-017-3021-3
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
In this paper, a time- and space-coordinate transformation, commonly known as the Kustaanheimo-Stiefel (KS)-transformation, is applied to reduce the order of singularities arising due to the motion of an infinitesimal body in the vicinity of a smaller primary in the three-body system. In this work, the Sun-Earth system is considered assuming the Sun to be a radiating body and the Earth as an oblate spheroid. The study covers motion around collinear Lagrangian L-1 and L-2 points. Numerical computations are performed for both regularized and non-regularized equations of motion and results are compared for non-periodic as well as periodic motion. In the transformed space, time is also computed as a function of solar radiation pressure (q) and oblateness of the Earth (A2). The two parameters (q, A2) have a significant impact on time in the transformed space. It is found that KS-regularization reduces the order of the pole from five to three at the point of singularity of the governing equations of motion.
引用
收藏
页数:12
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