Formation flying along halo orbit of circular-restricted three-Body problem

Mai Bando, Akira Ichikawa

研究成果: ジャーナルへの寄稿学術誌査読

18 被引用数 (Scopus)

抄録

A new control strategy based on output regulation theory is proposed for formation flying along a halo orbit near a libration point in the circular-restricted three-body problem. The reference orbit is a periodic or shifted perturbation of the halo orbit generated by an exosystem, and modification of linear output regulation theory is employed. First, the station keeping problem is considered, and the total velocity change required for the halo orbit maintenance is found to be negligible. The reasonable size of a perturbation can be determined numerically, and hence the formation flying proposed in this paper is useful for the design of a reference orbit along a halo orbit. The proposed relative orbit and control strategy are independent of halo orbits and can be applied to formation flying along an arbitrary path.

本文言語英語
ページ(範囲)123-129
ページ数7
ジャーナルJournal of Guidance, Control, and Dynamics
38
1
DOI
出版ステータス出版済み - 1月 1 2015

!!!All Science Journal Classification (ASJC) codes

  • 制御およびシステム工学
  • 航空宇宙工学
  • 宇宙惑星科学
  • 電子工学および電気工学
  • 応用数学

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