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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
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。
更新日期:2020-08-03
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。