首页> 外文期刊>Celestial Mechanics and Dynamical Astronomy: An international journal of space dynamics >Doubly symmetric periodic orbits around one oblate primary in the restricted three-body problem
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Doubly symmetric periodic orbits around one oblate primary in the restricted three-body problem

机译:在限制的三体问题中围绕一个赋予授权的双重定期轨道

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It is shown that there exists a class of doubly symmetric periodic solutions of Lunar type around one oblate primary in the restricted three-body problem. A small parameter is introduced as the closeness of the infinitesimal body to the oblate primary. The radius of the oblate primary is even smaller compared to the distance from the infinitesimal body to this primary, such that the order of magnitudes of the oblate perturbation and that of the third-body perturbation are comparable. The proof is based on the perturbation techniques and a corollary of Arenstorf's fixed-point theorem, where the error estimates are settled by averaging the first-order system and using the Gronwall's inequality.
机译:结果表明,在限制的三体问题中存在一类围绕一个扁平初级的月球类型的双对称周期解。 将一个小参数作为无穷小的身体的近距离引入扁平的初级。 与距离无限内身对该初级的距离相比,弓粒的半径甚至更小,使得扁平扰动的大小阶数和第三体扰动的阶数是可比的。 证据基于扰动技术和ArenStorf的定理定理的推论,其中错误估计通过平均一阶系统并使用GronWALL的不等式来解决。

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