Modified equations of motion around circular trajectory and its application to formation flying control

研究成果: Conference contribution

抄録

Usually, the formation flying associated with a circular orbit is discussed through the well-known Hill's equations of motion. This paper presents and discusses the formation-fixed coordinate to discuss about the formation behavior. The resulted equations take the non-autonomous form and will depict some interesting characteristics. The paper will also present the application of decentralized formation control strategy that stabilizes and enables a quick reaction to the command.

本文言語English
ホスト出版物のタイトルAmerican Astronautical Society - Space Flight Mechanics 2007 - Advances in the Astronautical Sciences, Proceedings of the AAS/AIAA Space Flight Mechanics Meeting
ページ1429-1434
ページ数6
出版ステータスPublished - 2007
外部発表はい
イベント17th Annual Space Flight Mechanics Meeting - Sedona, AZ, United States
継続期間: 2007 1 282007 2 1

出版物シリーズ

名前Advances in the Astronautical Sciences
127 PART 2
ISSN(印刷版)0065-3438

Conference

Conference17th Annual Space Flight Mechanics Meeting
国/地域United States
CitySedona, AZ
Period07/1/2807/2/1

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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