Precise landing of space probe on asteroid using multiple markers

Naoko Ogawa, Fuyuto Terui, Jun'ichiro Kawaguchi

研究成果: Conference contribution

7 被引用数 (Scopus)

抄録

We propose a novel strategy for precise landing of a space probe on an asteroid surface. In Hayabusa mission, a Japanese asteroid sample-return spacecraft launched in 2003, a small marker was dropped onto the ground and utilized as a landmark for landing. In this paper, we propose two scenarios to drop multiple markers one by one, with a view to more precise landing. Preliminary Monte Carlo simulation of guidance using multiple markers with assumption of some control errors are presented. It was indicated that more than one markers allow us to increase the landing accuracy compared to the conventional method using a single marker.

本文言語English
ホスト出版物のタイトル18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings
出版社IFAC Secretariat
ページ172-177
ページ数6
PART 1
ISBN(印刷版)9783902661968
DOI
出版ステータスPublished - 2010
外部発表はい
イベント18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Nara, Japan
継続期間: 2010 9 62010 9 10

出版物シリーズ

名前IFAC Proceedings Volumes (IFAC-PapersOnline)
番号PART 1
18
ISSN(印刷版)1474-6670

Other

Other18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010
国/地域Japan
CityNara
Period10/9/610/9/10

ASJC Scopus subject areas

  • 制御およびシステム工学

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