Attitude control of spinning solar sail with huge membrane

Fuminori Hanaoka, Osamu Mori, Yuichi Tsuda, Ryu Funase, Jun'ichiro Kawaguchi

研究成果: Conference contribution

抄録

This paper describes the attitude dynamics and the control method of a spinning solar sail spacecraft. The solar sail considered here has no structure supporting membrane, therefore estimation of the effect of membrane flexibility is one of the problems to solve for the future validation flight. In this study, we established a dynamic model including membrane vibration to handle a coupled motion of a rigid spacecraft and a flexible membrane, and focus on the consideration of attitude control method. The result is confirmed with numerical simulation by use of Multi Particle Model(MPM).

本文言語English
ホスト出版物のタイトルSpace Flight Mechanics 2008 - Advances in the Astronautical Sciences, Proceedings of the AAS/AIAA Space Flight Mechanics Meeting
ページ1765-1776
ページ数12
出版ステータスPublished - 2008
外部発表はい

出版物シリーズ

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

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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