WEKO3
アイテム
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Hayabusa optical hybrid navigation and guidance
https://jaxa.repo.nii.ac.jp/records/7530
https://jaxa.repo.nii.ac.jp/records/75306773ef4e-8838-44e3-889e-c497ded71889
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Hayabusa optical hybrid navigation and guidance | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | はやぶさ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | MUSES-C | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小惑星探査機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | サンプルリターンミッション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 光学誘導 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | OPNAV | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 自律航法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星誘導 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道位置推定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 位置保持 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ホバリング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | タッチダウン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙航行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 光レーダ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 測距 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hayabusa | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MUSES-C | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Asteroid Sample-return Spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sample return mission | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optical navigation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | OPNAV | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | autonomous navigation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite guidance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbital position estimation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stationkeeping | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hovering | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | touchdown | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space navigation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optical radar | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rangefinding | |||||
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 | はやぶさにおける光学複合航法と誘導 | |||||
著者 |
小湊, 隆
× 小湊, 隆× 松岡, 正敏× 吉川, 真× 川口, 淳一郎× Kominato, Takashi× Matsuoka, Masatoshi× Yoshikawa, Makoto× Kawaguchi, Junichiro |
|||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
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/ISAS) | |||||
書誌情報 |
第16回アストロダイナミクスシンポジウム講演後刷り集 2006 en : Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics p. 167-172, 発行日 2007-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 2005年9月12日「はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)」はイトカワに到着し、3ヶ月間のランデブーと離着陸を実施した。探査機をイトカワに誘導航法するため、地上からの電波観測を組み合わせた光学複合航法を適用した。この他に「はやぶさ」は搭載画像処理などを含んだ自律航法誘導機能も備わっている。2005年7月末に3台のうち1目台のホイールを失い、10月初めに2台目を失ったが、技術実証および科学観測を継続することに成功した。本報告ではクルージングフェーズから近傍フェーズまでの航法誘導をどのように実施したか飛行結果を交えて述べる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft) succeeded in the rendezvous with Itokawa for three months, in the proximity observations, and succeeded in the twice landing and takeoff. In order to navigate and to guide the spacecraft to Itokawa, it made highly use of optical hybrid navigation technique combined with the radiometric information obtained on the ground. Hayabusa is also equipped with an autonomous navigation and guidance function including onboard image processing and the like. Although one of three reaction wheels failed in late July 2005, and the second wheel failed in early October, we had succeeded to continue the technology demonstrations and the science observations. This paper presents how those navigation and guidance in proximity phase were carried out, showing flight results. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063481029 |