Satellite encounters. [In circular orbits]
Satellite encounters. [In circular orbits]
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卫星相遇。
DOI:
10.1016/0019-1035(86)90089-8
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发表时间:
1986
期刊:
影响因子:
--
通讯作者:
M. Hénon
中科院分区:
文献类型:
--
作者:
J. Petit;M. Hénon
We study numerically the interaction of two small satellites, initially on circular orbits with slightly different radii. We show first that by going to Hill's limit of vanishing masses, one can reduce the problem to a simpler form in which only one dimensionless parameter remains: the reduced impact parameter. We present then a detailed study of the family obtained when this parameter is varied. Each orbit consists of three phases: approach of the two small bodies, interplay, and departure. Fourth-order series are used to represent the asymptotic motion of the two small bodies in the approach and departure phases; these series are matched with a numerical integration of the interplay phase to give an accurate representation of the entire orbit. For each orbit, we compute the net effect of the encounter, essentially characterized by an increase of the separation of the satellite orbits. We compute also the minimal distance of approach of the two satellites. In the limiting cases of large and small impact parameters, the results are compared with the predictions of perturbation theories. Finally we study the “transitions,” which are apparent discontinuities of the family with a sudden change of the direction of departure. We show that they can be explained by the asymptotic approach of the orbit to an unstable periodic solution of Hill's problem. Transitions take place for infinitely many values of the parameter, forming a Cantor-like set.