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Using a Three-Impulse Maneuvering Scheme for Returning from the Lunar Orbit to the Reentry Point of the Earth’s Atmosphere
Journal of Computer and Systems Sciences International ( IF 0.5 ) Pub Date : 2020-05-08 , DOI: 10.1134/s1064230720010050 N. M. Gavrikova , Yu. F. Golubev
中文翻译:
使用三脉冲机动方案从月球轨道返回地球大气的折返点
更新日期:2020-05-08
Journal of Computer and Systems Sciences International ( IF 0.5 ) Pub Date : 2020-05-08 , DOI: 10.1134/s1064230720010050 N. M. Gavrikova , Yu. F. Golubev
Abstract
A practically useful algorithm for constructing the trajectory of returning from a Lunar orbit to the Earth using one-impulse and three-impulse maneuvering schemes is presented. This algorithm forms the return trajectory to the reentry point of the atmosphere satisfying the given constraints, taking into account the current ephemeris and the fact that the gravitational fields of the Moon and Earth are noncentral. The computer simulation results make it possible to draw conclusions about the advantages and expedience of using a particular maneuvering scheme.中文翻译:
使用三脉冲机动方案从月球轨道返回地球大气的折返点