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KIAM Preprint  53, Moscow, 2019
Authors: Gavrikova N.M., Golubev Y. F.
Construction of the return trajectory from the lunar parking orbit to the Earths atmosphere reentry point
Abstract:
The practically useful algorithm for construction of the return trajectory from the lunar parking orbit to the Earths atmosphere reentry point using three-impulse maneuvering scheme for the three-body problem (the Earth, the Moon, the spacecraft) under non-central gravity field is presented. The algorithm provides fulfillment of the boundary conditions at the Earths atmosphere reentry point.
Keywords:
return trajectory, multi-impulse transfer sequence, Battins formulation of the Lambert problem
Publication language: russian,  pages: 39
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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About authors:
  • Gavrikova Nadezhda Mikhailovna,  orcid.org/0000-0003-1437-5973
  • Golubev Yury Filippovich,  orcid.org/0000-0002-2450-0224KIAM RAS