Attitude control challenges and solutions for Hayabusa spacecraft

Masashi Uo, Kenichi Shirakawa, Tatsuaki Hashimoto, Takashi Kubota, Jun'ichiro Kawaguchi

研究成果: Conference contribution

7 被引用数 (Scopus)

抄録

Hayabusa attempted to touch-down two times in November, 2005 after two years of cruising and two months of proximity observation around ITOKAWA. One of three reaction wheels failed in late July of 2005, and the second wheel failed in early October. While the attitude stabilization logic with two wheels was inherent in the onboard system, the stabilization with one wheel required the use of onboard re-programming function and special ground support operations. This paper describes how the attitude control system and operation were adapted to cope with the loss of reaction wheels, along with the introduction of attitude control system that was designed to realize various attitude functions with minimum onboard resources.

本文言語English
ホスト出版物のタイトルCollection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006
ページ1342-1351
ページ数10
出版ステータスPublished - 2006
外部発表はい
イベントAIAA/AAS Astrodynamics Specialist Conference, 2006 - Keystone, CO, United States
継続期間: 2006 8 212006 8 24

出版物シリーズ

名前Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006
2

Conference

ConferenceAIAA/AAS Astrodynamics Specialist Conference, 2006
国/地域United States
CityKeystone, CO
Period06/8/2106/8/24

ASJC Scopus subject areas

  • 工学(全般)

フィンガープリント

「Attitude control challenges and solutions for Hayabusa spacecraft」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