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Image based navigation and guidance for approach phase to the asteroid utilizing captured images at the rehearsal approach
https://jaxa.repo.nii.ac.jp/records/7362
https://jaxa.repo.nii.ac.jp/records/7362ba3b506a-d82a-4885-892c-1f9020c50874
Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Image based navigation and guidance for approach phase to the asteroid utilizing captured images at the rehearsal approach | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | 小惑星着陸のための近傍観測データを利用した画像航法誘導 | |||||
著者 |
照井, 冬人
× 照井, 冬人× 尾川, 順子× 小田, 賢治× 卯尾, 匡史× Terui, Fuyuto× Ogawa, Naoko× Oda, Kenji× Uo, Masahi |
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著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
日本電気 | ||||||
著者所属 | ||||||
NEC東芝スペースシステム | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
NEC | ||||||
著者所属(英) | ||||||
en | ||||||
NEC TOSHIBA Space Systems | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
アストロダイナミクスシンポジウム講演後刷り集 en : Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics 巻 2009, 発行日 2010-03 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部)) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 小惑星上への高精度のサンプリング/着陸には、航法の目印になるクレータなどのポイント(GCP: Ground ControlPoints)を使用する必要がある。しかし、GCPの分布や形状は、小惑星に到着してからでないと明らかにはならないため、事前に航法降下戦略を確定することが困難である。本論文では、小惑星近傍到着後に搭載カメラで撮像したGCP情報を用いて、高精度かつ確実に小惑星表面に航法誘導を行う方式とその評価結果について報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | It is necessary to use Ground Control Points (GCP) in real time in order to precisely guide the spacecraft to desired landing/sampling position. It is not possible to determine the navigation strategy before launch because the characteristics such as shape, size and distribution of GCPs are revealed when the spacecraft reaches the asteroid. This paper proposes a method to precisely and safely navigate the spacecraft to asteroid surface utilizing the asteroid information gathered by in-situ observation by onboard cameras. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11567475 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064734057 |