Final autonomous descent based on target marker tracking

T. Hashimoto, T. Kubota, S. Sawai, J. Kawaguchi, M. Uo

研究成果: Conference contribution

9 被引用数 (Scopus)

抄録

This paper describes the navigation, guidance, and control for the final descent phase of the Hayabusa spacecraft, a technology demonstrator aiming at the sample and return from an asteroid. To cancel the relative horizontal velocity with respect to the asteroid surface, an artificial landmark named "Target Marker" was used. The design and in-flight data of Target Marker tracking are shown In the paper, together with autonomous control scheme of the spacecraft.

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1395-1402
ページ数8
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)

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