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
相关论文
共 50 条
  • [41] Capture in the circular and elliptic restricted three-body problem
    Makó, Z
    Szenkovits, F
    [J]. CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2004, 90 (1-2): : 51 - 58
  • [42] The circular restricted three-body problem in curvilinear coordinates
    Claudio Bombardelli
    Pablo Bernal Mencía
    [J]. Celestial Mechanics and Dynamical Astronomy, 2018, 130
  • [43] Flybys in the planar, circular, restricted, three-body problem
    Campagnola, Stefano
    Skerritt, Paul
    Russell, Ryan P.
    [J]. CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2012, 113 (03): : 343 - 368
  • [44] Attitude dynamics in the circular restricted three-body problem
    Davide Guzzetti
    Kathleen Connor Howell
    [J]. Guzzetti, Davide (dguzzett@mail.tsinghua.edu.cn), 2018, Tsinghua University (02) : 87 - 119
  • [45] Flybys in the planar, circular, restricted, three-body problem
    Stefano Campagnola
    Paul Skerritt
    Ryan P. Russell
    [J]. Celestial Mechanics and Dynamical Astronomy, 2012, 113 : 343 - 368
  • [46] Capture in the Circular and Elliptic Restricted Three-Body Problem
    Zoltán Makó
    Ferenc Szenkovits
    [J]. Celestial Mechanics and Dynamical Astronomy, 2004, 90 : 51 - 58
  • [47] Equilibrium points and stability in the restricted three-body problem with oblateness and variable masses
    Singh, Jagadish
    Leke, Oni
    [J]. ASTROPHYSICS AND SPACE SCIENCE, 2012, 340 (01) : 27 - 41
  • [48] GLOBAL REGULARIZATION METHOD FOR PLANAR RESTRICTED THREE-BODY PROBLEM
    Sharaf, M. A.
    Dwidar, H. R.
    [J]. SERBIAN ASTRONOMICAL JOURNAL, 2015, 191 : 39 - 49
  • [49] Hyperbolic regularization of the restricted three-body problem on curved spaces
    Sanchez-Cerritos, Juan Manuel
    Perez-Chavela, Ernesto
    [J]. ANALYSIS AND MATHEMATICAL PHYSICS, 2022, 12 (01)
  • [50] Equilibrium points and stability in the restricted three-body problem with oblateness and variable masses
    Jagadish Singh
    Oni Leke
    [J]. Astrophysics and Space Science, 2012, 340 : 27 - 41