Dynamic deployment and attitude control motion of spinning solar sail "IKAROS"

Osamu Mori, Yoji Shirasawa, Yuichi Tsuda, Ryu Funase, Takanao Saiki, Yuya Mimasu, Ryo Jifuku, Norizumi Motooka, Takayuki Yamamoto, Junichiro Kawaguchi

研究成果: Conference contribution

2 被引用数 (Scopus)

抄録

In this paper, the attitude dynamics of IKAROS, which is spinning solar sail, is presented. Multi Particle Model (MPM) and First Mode Model of out-of-plane deformation (FMM) are introduced to analyze the out-of-plane oscillation mode of spinning solar sail. Considering the thruster configuration of IKAROS, the force on main body and membrane by thruster plume as well as reaction force by thruster are integrated into MPM. The attitude motion after sail deployment or reorientation using thrusters can be analyzed by MPM numerical simulations precisely. The out-of-plane oscillation of IKAROS is governed by three modes derived from FMM. FMM is simple and valid for the design of attitude controller.

本文言語English
ホスト出版物のタイトル62nd International Astronautical Congress 2011, IAC 2011
ページ5582-5588
ページ数7
出版ステータスPublished - 2011
外部発表はい
イベント62nd International Astronautical Congress 2011, IAC 2011 - Cape Town, South Africa
継続期間: 2011 10 32011 10 7

出版物シリーズ

名前62nd International Astronautical Congress 2011, IAC 2011
7

Other

Other62nd International Astronautical Congress 2011, IAC 2011
国/地域South Africa
CityCape Town
Period11/10/311/10/7

ASJC Scopus subject areas

  • 航空宇宙工学

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