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Adaptive Methods of the Flybys Constructing in the Jovian System with the Orbiter Insertion Around the Galilean Moon
Solar System Research ( IF 0.9 ) Pub Date : 2020-08-03 , DOI: 10.1134/s0038094620040061
Yu. F. Golubev , A. V. Grushevskii , V. V. Koryanov , S. M. Lavrenov , A. G. Tuchin , D. A. Tuchin

Abstract

We consider space expeditions with a long-term spacecraft stay near the studied celestial body (artificial satellites of small bodies of the Solar System), or expeditions with a possible spacecraft landing on the surface of the celestial body (for example, the ESA Jovian Icy Moon Explorer JUICE mission, and the Russian prospective project Laplace‑P). An effective formalism is proposed for creating adaptive search scenarios for low-cost combined spacecraft trajectories, focused on the possibility of using high-performance computing resources of the computer experimentation. Examples are given of the implementation of this formalism for searching for combinations of interlunar gravitational maneuvers in the Jovian system with the aim of entering the orbit of the Jovian moon’s artificial satellite.


中文翻译:

围绕伽利略卫星的轨道插入的木星系统构造飞越的自适应方法。

摘要

我们考虑使用长期航天器进行的太空探险停留在所研究的天体附近(太阳系小型天体的人造卫星),或者考虑将可能的航天器降落在该天体表面上的探险(例如,ESA Jovian Icy Moon Explorer JUICE任务,以及俄罗斯的预期项目Laplace-P)。提出了一种有效的形式主义,以针对低成本的组合航天器轨迹创建自适应搜索方案,重点是使用计算机实验的高性能计算资源的可能性。举例说明了这种形式主义的实现方式,以寻找木星系统中月球间引力动作的组合,目的是进入木星人造卫星的轨道。
更新日期:2020-08-03
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