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Preprints of the Keldysh Institute of Applied Mathematics, 2016, 056, 24 pp.
DOI: https://doi.org/10.20948/prepr-2016-56
(Mi ipmp2132)
 

This article is cited in 5 scientific papers (total in 5 papers)

Optimization of one impulse return trajectory from Moon orbit

A. S. Samotokhin, A. G. Tuchin
Full-text PDF (831 kB) Citations (5)
References:
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 of limitations 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.
Document Type: Preprint
Language: Russian
Citation: A. S. Samotokhin, A. G. Tuchin, “Optimization of one impulse return trajectory from Moon orbit”, Keldysh Institute preprints, 2016, 056, 24 pp.
Citation in format AMSBIB
\Bibitem{SamTuc16}
\by A.~S.~Samotokhin, A.~G.~Tuchin
\paper Optimization of one impulse return trajectory from Moon orbit
\jour Keldysh Institute preprints
\yr 2016
\papernumber 056
\totalpages 24
\mathnet{http://mi.mathnet.ru/ipmp2132}
\crossref{https://doi.org/10.20948/prepr-2016-56}
Linking options:
  • https://www.mathnet.ru/eng/ipmp2132
  • https://www.mathnet.ru/eng/ipmp/y2016/p56
  • This publication is cited in the following 5 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    Препринты Института прикладной математики им. М. В. Келдыша РАН
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    Abstract page:118
    Full-text PDF :60
    References:14
     
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