WEKO3
アイテム
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Analysis on touchdown dynamics of Hayabusa spacecraft
https://jaxa.repo.nii.ac.jp/records/7527
https://jaxa.repo.nii.ac.jp/records/75276e5fbe80-56a6-43a2-8b2a-b3c646e99f55
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 | Analysis on touchdown dynamics of Hayabusa spacecraft | |||||
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 | イトカワ | |||||
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 | タッチダウン | |||||
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 | 高度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 重力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ダイナミックモデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レーザ測距機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数学モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算機シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 構造振動 | |||||
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 | Itokawa | |||||
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 | touchdown | |||||
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 | altitude | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | gravitation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dynamic model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laser range finder | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mathematical model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computerized simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | structural vibration | |||||
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 | はやぶさのタッチダウンダイナミクスの解析 | |||||
著者 |
大槻, 真嗣
× 大槻, 真嗣× 久保田, 孝× 坂東, 信尚× 矢野, 創× 樋口, 健× 卯尾, 匡史× 橋本, 樹明× Otsuki, Masatsugu× Kubota, Takashi× Bando, Nobutaka× Yano, Hajime× Higuchi, Ken× Uo, Masashi× Hashimoto, Tatsuaki |
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著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 宇宙探査工学研究系 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 宇宙探査工学研究系 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 宇宙探査工学研究系 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 固体惑星科学研究系 | ||||||
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 | ||||||
NEC東芝スペースシステム 宇宙システム本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 宇宙探査工学研究系 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Dept. of Spacecraft Engineering, Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Dept. of Spacecraft Engineering, Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Dept. of Spacecraft Engineering, Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Department of Planetary Science, 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 | ||||||
NEC TOSHIBA Space Systems Ltd. Space Systems Division | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Dept. of Spacecraft Engineering, 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. 145-150, 発行日 2007-03 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 小惑星探査機「はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)」は2005年11月に小惑星イトカワへ2度に渡ってタッチダウンを行った。この論文では、探査機下部に取り付けられたLRF(Laser Range Finder)から得られた高度データに基づいて、はやぶさ探査機のタッチダウン時の挙動を解析した。まず、探査機に作用する外力を整理し、イトカワの重力を推定した。そして、6自由度の剛体運動モデル、サンプラホーンならびにソーラパネルの柔軟体モデルを構築し、それらを結合して、はやぶさの探査機ダイナミクスモデルとした。構築したモデルで1回目のタッチダウン挙動を再現し、実際に得られたデータとの比較検討を通じてその妥当性を確認した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The asteroid exploration spacecraft 'Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft)' tried to touch down twice on the asteroid 'Itokawa' in November 2005. In this paper, the motion of the Hayabusa spacecraft during the first touchdown is analyzed on the basis of the altitude data derived from the LRF (Laser Range Finder) sensors implemented at the bottom of the spacecraft. The environmental interaction for the Hayabusa spacecraft is also considered and the gravity of Itokawa in the vicinity on where Hayabusa touched down is estimated. Further, in the numerical calculation, the motion of Hayabusa spacecraft is reproduced by the combination of the motion of the rigid body with six degrees of freedom, reactive force of the sampler horn against the Itokawa surface and vibration of the solar panels. The validation of the numerical model is obtained by comparing the simulation result with the data measured by the LRF sensors. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063481026 |