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关于可变质量的椭圆型限制性三体问题运动方程的再探讨 被引量:1

ON FURTHER RESEARCH FOR EQUATIONS OF MOTION FOR ELLIPTIC RESTRICTED PROBLEM OF THREE BODIES WITH VARIABLE MASS
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摘要 较近期的关于可变质量的椭圆型限制性三体问题的运动方程[5]是对于n=1的情况,本文把星序数n扩充到2,3及4,对于每一种n,分别建立了可变质量的椭圆型限制性三体问题的运动方程。 The equations of motion of elliptic restricted problem of three bodies with variable mass according to n =1(k = 0, q =1/2) were derived more recently[5]. We have expanded the main sequence star to n = 2(k = 1, q = 3/2), n = 3(k = 2, q = 6/2) and n = 4(k = 3, q = 7/2) in this paper. For each case we established each set of differential equations of motion with variable mass. On the other hand, we corrected some errors in the previous work forn=1(k = 0, q=1/2), which still possess an effect on the simplified form of differential equations of motion for problem of three bodies with variable mass although they are non-substantial. The three sets of differential equations of motion for elliptic restricted problem of three bodies are indicated in Formulae (41), (42) and (43) corresponding to n = 2, n = 3 and n = 4, respectively.
作者 潘大钑
出处 《中国科学院上海天文台年刊》 1993年第14期126-136,共11页 Annals Shanghai Astronomical Observatory Chinese Academy of Sciences
关键词 限制性三体问题 椭圆轨道 运动方程 星序数 可变质量 Three-body problem Restricted three-body problem Elliptical orbit
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  • 1Szebehely V. Theory of Orbits [ M ]. London:Academic Press, 1967.
  • 2Yamato H. Trajectory Design Methods for Restricted Problems of Three Bodies with Perturbations [ D]. Pennsylvania:The Pennsylvania State University,2003.
  • 3Ammar M K. The Effect of Solar Radiation Pressure on the Lagrangian Points in the Elliptic Restricted Three-Body Problem [ J ]. Astrophys Space Science, 2008,313 ( 4 ) : 393-408.
  • 4黄玻.考虑天体形状的椭圆型限制性三体问题的Hill稳定性.天文学报,1982,23(4):390-397.
  • 5Montenbruck O. Satellite Orbits [ M]. New York: Springer, 2000.
  • 6Richard B. An Introduction to the Mathematics and Methods of Astrodynamics [ M ]. Virginia: American Institute of Aeronautics and Astronautics,Inc, 1999.

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