Optimal spin rate control of a spinning solar sail for the maximum-radius orbit transfer problem

Go Ono, Yuya Mimasu, Jun'ichiro Kawaguchi

研究成果: Conference contribution

抄録

The attitude and orbit of a spinning solar sail can be controlled by the spin rate of the spacecraft. In this paper, an optimal spin rate control law of a spinning solar sail for the maximum-radius orbit transfer problem is derived. An optimal control problem is solved analytically and numerically, and the comparison of the analytical and numerical solutions proves their validity. The control method proposed in this paper extends the possibilities of spinning solar sails.

本文言語English
ホスト出版物のタイトルAdvances In The Astronautical Sciences
編集者Donald L. Mackison, Ossama Abdelkhalik, Roby S. Wilson, Renato Zanetti
出版社Univelt Inc.
ページ2661-2676
ページ数16
ISBN(電子版)9780877036111
出版ステータスPublished - 2014
外部発表はい
イベント24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, United States
継続期間: 2014 1 262014 1 30

出版物シリーズ

名前Advances in the Astronautical Sciences
152
ISSN(印刷版)0065-3438

Conference

Conference24th AAS/AIAA Space Flight Mechanics Meeting, 2014
国/地域United States
CityMexico
Period14/1/2614/1/30

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

フィンガープリント

「Optimal spin rate control of a spinning solar sail for the maximum-radius orbit transfer problem」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル