Guidance and navigation of hayabusa spacecraft for asteroid exploration and sample return mission

Takashi Kubota, Tatsuaki Hashimoto, Ju N.Ichiro Kawaguchi, Masashi Uo, Ke N.Ichi Shirakawa

研究成果: Conference contribution

27 被引用数 (Scopus)

抄録

The Japanese asteroid exploration spacecraft Hayabusa autonomously performed touchdown two times in November 2005. The autonomous guidance and navigation capability is installed aboard the spacecraft. The GNC system collects the laser altimeter, laser range finders and navigation cameras information aboard and is designed to estimate where the spacecraft is and to decide the path correction maneuvers. The programmed function includes the image processing designed to detect an artificial target marker location to approach and cancel the relative velocity. A terrain alignment maneuver is also accomplished by both altitude and attitude control. This paper presents how autonomous guidance and navigation was performed in Hayabusa mission.

本文言語English
ホスト出版物のタイトル2006 SICE-ICASE International Joint Conference
ページ2793-2796
ページ数4
DOI
出版ステータスPublished - 2006
外部発表はい
イベント2006 SICE-ICASE International Joint Conference - Busan, Korea, Republic of
継続期間: 2006 10 182006 10 21

出版物シリーズ

名前2006 SICE-ICASE International Joint Conference

Other

Other2006 SICE-ICASE International Joint Conference
国/地域Korea, Republic of
CityBusan
Period06/10/1806/10/21

ASJC Scopus subject areas

  • コンピュータ サイエンスの応用
  • 制御およびシステム工学
  • 電子工学および電気工学

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