On single-wheel configured spacecraft and the attitude stability revisited

Jun'ichiro Kawaguchi, Akifumi Kitajima, Osamu Mori, Kenichi Shirakawa

研究成果: Conference contribution

抄録

This paper presents what the Hayabusa spacecraft experienced when it restarted the three axis stabilization. Due to the loss of two wheels aboard and also due to the loss of fuel, the primary axis of inertia of the spacecraft was tilted offset to the geometrical axis. The instability was observed unexpectedly since there was little thought about the instability associated with the single wheel system. The results can be applied for other spacecraft. The flight results are shown as well.

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571-577
ページ数7
出版ステータスPublished - 2008
外部発表はい
イベント18th Annual Space Flight Mechanics Meeting - Galveston, TX, United States
継続期間: 2008 1 272008 1 31

出版物シリーズ

名前Advances in the Astronautical Sciences
130 PART 1
ISSN(印刷版)0065-3438

Conference

Conference18th Annual Space Flight Mechanics Meeting
国/地域United States
CityGalveston, TX
Period08/1/2708/1/31

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

「On single-wheel configured spacecraft and the attitude stability revisited」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