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  1. シンポジウム・研究会
  2. アストロダイナミクスシンポジウム
  3. 第16回
  1. コンテンツタイプ
  2. 会議発表論文/会議発表用資料 (Conference Paper/Presentation)

Detailed guidance and navigation operations during descents and touchdowns, Hayabusa

https://jaxa.repo.nii.ac.jp/records/7531
https://jaxa.repo.nii.ac.jp/records/7531
a0f60a99-96c6-423d-9042-2a9899b5d20b
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 Detailed guidance and navigation operations during descents and touchdowns, Hayabusa
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 地表基準点航法
キーワード
主題Scheme Other
主題 GCPNAV
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 宇宙航行
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 衛星制御
キーワード
主題Scheme Other
主題 降下軌道
キーワード
主題Scheme Other
主題 小惑星
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 降下
キーワード
主題Scheme Other
主題 速度
キーワード
主題Scheme Other
主題 位置誤差
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 ground control point navigation
キーワード
言語 en
主題Scheme Other
主題 GCPNAV
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 space navigation
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 satellite control
キーワード
言語 en
主題Scheme Other
主題 descent trajectory
キーワード
言語 en
主題Scheme Other
主題 asteroid
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 descent
キーワード
言語 en
主題Scheme Other
主題 velocity
キーワード
言語 en
主題Scheme Other
主題 position error
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 はやぶさにおける小惑星接近とタッチダウンで行われた航法誘導運用の詳細
著者 森田, 秀郎

× 森田, 秀郎

WEKO 40241

森田, 秀郎

Search repository
白川, 健一

× 白川, 健一

WEKO 40242

白川, 健一

Search repository
久保田, 孝

× 久保田, 孝

WEKO 40243

久保田, 孝

Search repository
橋本, 樹明

× 橋本, 樹明

WEKO 40244

橋本, 樹明

Search repository
川口, 淳一郎

× 川口, 淳一郎

WEKO 40245

川口, 淳一郎

Search repository
Morita, Hideo

× Morita, Hideo

WEKO 40246

en Morita, Hideo

Search repository
Shirakawa, Kenichi

× Shirakawa, Kenichi

WEKO 40247

en Shirakawa, Kenichi

Search repository
Kubota, Takashi

× Kubota, Takashi

WEKO 40248

en Kubota, Takashi

Search repository
Hashimoto, Tatsuaki

× Hashimoto, Tatsuaki

WEKO 40249

en Hashimoto, Tatsuaki

Search repository
Kawaguchi, Junichiro

× Kawaguchi, Junichiro

WEKO 40250

en Kawaguchi, Junichiro

Search repository
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
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
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. 173-178, 発行日 2007-03
抄録
内容記述タイプ Abstract
内容記述 2005年11月、はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)は小惑星'いとかわ'へ5回の接近誘導を実施した。期待に反し、'いとかわ'表面はごつごつした岩で覆われ、はやぶさが安全にタッチダウンできる場所は数ヶ所しかなかった。しかも、実施前に姿勢制御装置が壊れてしまい、要求される精度での誘導は非常に難しかった。接近時の航法誘導は、搭載ソフトによる自動誘導と計画されていた。しかし、予想外にいびつな小惑星形状だった為、計画通りにいかなかった。一方、地上でリアルタイムに行う、地形参照による航法誘導が可能になり、精密な誘導が出来るようになった。本稿では、3回のタッチダウンと長時間着陸の成功に結びつけた、はやぶさプロジェクトチームによる新航法誘導ツールとその運用について述べる。
抄録(英)
内容記述タイプ Other
内容記述 In November 2005, Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft) performed descent flights to the Itokawa surface five times. The Itokawa surface is full of boulders against expectation and there are few flat areas where the spacecraft can touch down safely. With the reaction wheels lost prior to the events, it was very difficult to control translation motion accurately, since the guidance accuracy of several millimeters per second was requested. The guidance and navigation in descent phase was planned for autonomous guidance by OBS (OnBoard Software) before launch. However, it was not successful due to the highly irregular shape of the asteroid. On the other hand, the guidance and navigation on the ground based on the terrain recognition in quasi real time well worked. The Hayabusa project team devised and built the special tools on the ground and had tuned it before the successful three touch downs and one long landing on the surface.
資料番号
内容記述タイプ Other
内容記述 資料番号: AA0063481030
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