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On the micro-synthesis of the M-V rocket attitude control design
https://jaxa.repo.nii.ac.jp/records/7803
https://jaxa.repo.nii.ac.jp/records/78038022a8ab-ad46-408e-a546-4cafda1daa47
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 | On the micro-synthesis of the M-V rocket attitude control design | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3段固体燃料ロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 打上げ機姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3軸姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロバストな制御理論 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | システムエンジニアリング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道投入 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御アルゴリズム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | プラントダイナミクス | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three-staged solid propellant rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | launch vehicle attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three-axis attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | robust control theory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | systems engineering | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit injection | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control algorithm | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | plant dynamics | |||||
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設計法のM-V型ロケットへの適用 | |||||
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 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | The Institute of Space and Astronautical Science (ISAS) | |||||
書誌情報 |
平成14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 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers p. 246-251, 発行日 2003-02 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 宇宙科学研究所では、M-V型ロケットを例題として、制御理論の実システムヘの応用について継続的に研究を行っている。同ロケットのこれまでの制御則はH無限大理論に則り設計してきたが、来る11月打ち上げ予定の5号機では、第2段ロケット姿勢制御用アクチュエータが一新されると共に軌道設計上の観点からより良い応特性が要請されるに至った。これを機会に、第2段制御論理の再設計にμ設計法を適用したので、ここに報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The paper presents a methodology for applying the micro-synthesis to a real high order system: launch vehicle attitude control. The design involves 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 micro-synthesis cannot be directly applied, thus, the standard procedure is modified in a special way in order to make the approach more efficient. The methodology provided in the study will contribute to better understanding how to apply the robust control theory to complicated real problems. | |||||
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: AA0045497041 |