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Halo-orbit formation in the Earth-Moon system by the electric propulsion spacecraft

  • Olga Starinova
  • , Vyacheslav Kupczov
  • , Changsheng Gao
  • , Yudon Hu
  • , Maksim Fain*
  • , Roman Khabibullin
  • *Corresponding author for this work
  • Samara National Research University
  • Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The problem of control laws, allowing the formation and maintenance of the required halo-orbit, is considered. The motion of the electric propulsion spacecraft is considered in the vicinity of the collinear libration points of the Earth-Moon system. The gravitational effects of the Earth, the Moon and the Sun are taken into account. The results are based on the simplified linearized models of the gravitational potential.

Original languageEnglish
Title of host publicationICNPAA 2018 World Congress
Subtitle of host publication12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences
EditorsSeenith Sivasundaram
PublisherAmerican Institute of Physics Inc.
ISBN (Electronic)9780735417724
DOIs
StatePublished - 4 Dec 2018
Event12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2018 - Yerevan, Armenia
Duration: 3 Jul 20186 Jul 2018

Publication series

NameAIP Conference Proceedings
Volume2046
ISSN (Print)0094-243X
ISSN (Electronic)1551-7616

Conference

Conference12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2018
Country/TerritoryArmenia
CityYerevan
Period3/07/186/07/18

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