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Flight performance of the mu-controller for the M-V rocket
https://jaxa.repo.nii.ac.jp/records/7755
https://jaxa.repo.nii.ac.jp/records/77552efdc93d-b0ab-4fbc-b7b4-7aecc93eb1dc
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 | Flight performance of the mu-controller for the M-V rocket | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行性能 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | M-Vロケット | |||||
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 | 惑星間軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アルゴリズム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 重み関数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御理論 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight performance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | M-V rocket | |||||
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 | interplanetary orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | algorithm | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | weighting function | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control theory | |||||
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 | μ制御理論のM-V型ロケットへの適用とフライト結果 | |||||
著者 |
森田, 泰弘
× 森田, 泰弘× 後藤, 晋一× Morita, Yasuhiro× Goto, Shinichi |
|||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
三菱プレシジョン | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Precision Co. Ltd. | ||||||
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 |
平成15年度アストロダイナミクスシンポジウム:講演後刷り集 en : ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers p. 333-338, 発行日 2004-02 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | さる5月にわが国初の小惑星探査機「はやぶさ」を計画通りの惑星間軌道に投入したM-Vロケット5号機の第2段ステージ姿勢制御アルゴリズムの設計においては、制御アクチュエータの更新を動機に、これまで実績を積んできたH(sub infinity)制御にかわり新たにμ設計法を適用した。ここでは、飛行結果をもとに設計の有効性を検証する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The performance of the M-V rocket attitude control has been validated by the flight results obtained at the first launch of its renewed version, which was successfully conducted in May 2003 to inject Japan's first asteroid sample returner 'HAYABUSA' into the planned inter-planetary orbit. The mu-synthesis was applied for the first time ever to the design beyond the reliable H(sub infinity) control to get better robust characteristics against uncertainties of the system parameters as well as precise tracking performance under the limited rigidity. As the plant dynamics has an extremely high order and unstable character, the standard mu-synthesis cannot be directly applied, thus, the standard procedure is modified in a special way in order to make the approach more efficient. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0918-8053 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0046652054 |