Perturbation hollow spheres and planetary perturbation rings pursuant to the gravity assists scattering in the Solar system

G. K. Borovin, Y. Golubev, A. V. Grushevskii, A. G. Tuchin
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Abstract

One of the types of gravitational scattering in the Solar system within the framework of the model of the circular restricted three-body problem (CR3BP) are the gravity assist maneuvers of the "particles of insignificant mass" (spacecraft, asteroids, comets, etc.). For their description, a physical analogy with the beam scattering of charged α-particles in a Coulomb field is useful. However, unlike the scattering of charged particles, there are external restrictions for the possibility of gravity assists executing related from the restricted size of planet's sphere of influence. At the same time, internal restrictions for the gravity assists performance estimated by the effective radii of planets are known from the literature on CR3BP (including gravitational capture by the planet, falling into it). The limited dynamic possibilities of using gravity maneuvers require their repeated performance. Based on the formalization of the search for the GA- timetables with subsequent adaptive involvement of a large number of options, a high-precision algorithm for synthesizing chains of increasing gravity assists was built. Its use leads to a significant inclination change of the research SC's orbit without significant fuel consumption during a reasonable flight time. They depend from the particle asymptotic velocity relative the planet. For obvious reasons, their influence cuts off the possibility of effective gravity assists performance. In this work the generalized estimates of the sizes of the near-planetary regions (planar rotating "perturbation rings" or "perturbation hollow spheres" in 3D case), falling into which is a necessary condition for the implementation of gravity assists, are presented. The detailed analysis shows that Neptune and Saturn have the characteristic "perturbation rings" and the perturbation hollow spheres of the largest sizes in the Solar system, and Jupiter occupies only the fourth place in this checklist after them and the planet’ Uranus perturbation hollow sphere.
摄动空心球和行星摄动环根据引力在太阳系中辅助散射
在圆形受限三体问题(CR3BP)模型框架内的太阳系引力散射类型之一是“质量微不足道的粒子”(航天器、小行星、彗星等)的重力辅助机动。对于它们的描述,与带电α-粒子在库仑场中的光束散射的物理类比是有用的。然而,与带电粒子的散射不同,由于行星影响范围的大小有限,引力协助执行的可能性受到外部限制。同时,由行星有效半径估算的引力辅助性能的内部限制从CR3BP的文献中已知(包括行星的引力捕获,落入其中)。有限的动态可能性使用重力机动需要他们的重复表演。在将GA-时间表搜索形式化的基础上,建立了一种高精度的重力辅助链合成算法。在合理的飞行时间内,它的使用导致了研究SC轨道的显著倾斜度变化,而没有显著的燃料消耗。它们取决于粒子相对于行星的渐近速度。由于显而易见的原因,它们的影响切断了有效重力辅助性能的可能性。本文提出了近行星区域(平面旋转的“摄动环”或三维情况下的“摄动空心球”)大小的广义估计,其中落入是实现重力辅助的必要条件。详细分析表明,海王星和土星具有太阳系中最具特征的“摄动环”和尺寸最大的摄动空心球,而木星在这一清单中仅排在它们和行星天王星摄动空心球之后的第四位。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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