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KIAM Preprint № 56, Moscow, 2016
Authors: Samotokhin A. S., Tuchin A. G.
Optimization of one impulse return trajectory from Moon orbit
Abstract:
The one impulse return trajectory from Moon orbit is considered. The right point of the return trajectory is entry point to Earth atmosphere. The purpose of considered method is to calculate optimal impulse that ensures limitations in right point of the trajectory. These limitations must provide landing of reentry vehicle in specified area of Earth surface. Several tasks with different sets are considered. The results of mathematic simulation for several Moon orbits are presented.
Keywords:
satellite of the Moon, transfer trajectory from Moon to Earth, numerical method, conditional minimization
Publication language: russian,  pages: 24
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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About authors:
  • Samotokhin Alexander Sergeevich,  orcid.org/0000-0003-1523-7644KIAM RAS
  • Tuchin Andrey Georgievich,  orcid.org/0000-0002-9099-3100KIAM RAS