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On manifolds of initial conditions leading to intersection of orbits of satellites with planet under weak gravitational perturbations

机译:关于初始条件的流形,在弱引力扰动下导致卫星轨道与行星相交

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We consider the problem of initial conditions that lead to the intersection of a satellite orbit with planetocentric sphere of a radius R. The problem is considered in frame of the satellite version of the double-averaged restricted three body problem with taking into account gravitational perturbations caused by the polar oblateness of the planet. For some integrable cases we provide the boundaries of the manifolds of the initial orbital elements leading (or not leading) to the intersection of the satellite orbit with the planet surface.
机译:我们考虑了导致卫星轨道与半径为R的平面中心球相交的初始条件的问题。在考虑到重力扰动的情况下,在双倍受限三体问题的卫星版本框架中考虑了该问题通过地球的极扁度。对于某些可积情况,我们提供了导致(或未导致)卫星轨道与行星表面相交的初始轨道元素的流形边界。

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