KIAM Main page Web Library  •  Publication Searh  Русский 

KIAM Preprint № 56, Moscow, 2016
Authors: Samotokhin A. S., Tuchin A. G.
Optimization of one impulse return trajectory from Moon orbit
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.
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:
Export link to publication in format:   RIS    BibTeX
View statistics (updated once a day)
over the last 30 days — 5 (-1), total hit from 01.09.2019 — 318
About authors:
  • Samotokhin Alexander Sergeevich, RAS
  • Tuchin Andrey Georgievich, RAS