An electric propulsion configured small halo orbit around L2

研究成果: Paper査読

抄録

For future applications, a Lagrange point of Sun-Earth system, L1 or L2 is conceived one of the best point for astronomy and connection ports for outer planets. This paper describes a new useful control method for realizing and keeping small circular Halo orbits around the L2 point, The resulted Halo orbit obtained is compact and circular realized with satisfactorily small thrust. The paper concludes the strategy is applied to many kinds of missions.

本文言語English
ページ3089-3096
ページ数8
出版ステータスPublished - 2005
外部発表はい
イベントInternational Astronautical Federation - 56th International Astronautical Congress 2005 - Fukuoka, Japan
継続期間: 2005 10 172005 10 21

Other

OtherInternational Astronautical Federation - 56th International Astronautical Congress 2005
国/地域Japan
CityFukuoka
Period05/10/1705/10/21

ASJC Scopus subject areas

  • 宇宙惑星科学
  • 航空宇宙工学

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