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Analysis and evaluation of H-2A launch vehicle control system
https://jaxa.repo.nii.ac.jp/records/7775
https://jaxa.repo.nii.ac.jp/records/77752d070879-d463-41da-9c72-6fbb2cac8a0d
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 and evaluation of H-2A launch vehicle control system | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2Aロケット | |||||
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 | 制御系 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行後解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 安定性解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 慣性計測装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動的特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Nyquistプロット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 周波数解析 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H-2A rocket | |||||
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 | control system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | postflight analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stability analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | inertial measurement unit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Nyquist plot | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | frequency analysis | |||||
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 | H-2Aロケット制御系の解析評価 | |||||
著者 |
鈴木, 秀人
× 鈴木, 秀人× 西平, 慎太郎× 池田, 佳起× 松田, 里香× 中川, 寛文× 服部, 和恵× Suzuki, Hideto× Nishihira, Shintaro× Ikeda, Yoshiki× Matsuda, Rika× Nakagawa, Hirofumi× Hattori, Kazue |
|||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
三菱スペース・ソフトウエア | ||||||
著者所属 | ||||||
三菱スペース・ソフトウエア | ||||||
著者所属 | ||||||
三菱スペース・ソフトウエア | ||||||
著者所属 | ||||||
三菱スペース・ソフトウエア | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Space Software Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Space Software Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Space Software Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Space Software 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. 73-78, 発行日 2003-02 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | H-2Aロケットは2001年8月初号機の打上に成功した。H-2Aは高さ約50メートル質量約300トンの日本最大のロケットである。その姿勢制御系は急激に変化する機体特性や構造の柔軟性、液体燃料の揺動などに対処する必要がある。飛行後解析により制御系は正常に機能したことが確認された。本論文はH-2Aロケットの制御系の概要、機体ダイナミクス、安定性解析、飛行後のデータ解析結果について報告するものである。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The first H-2A Launch Vehicle, the largest launch vehicle in Japan (50 m high and weighing 300 tons) was successfully launched in August 2001. Its control system should accommodate rapidly changing vehicle characteristics as well as structural elasticity and liquid-fuel sloshing. Post-flight analysis showed that the H-2A control system functioned properly. This paper outlines the H-2A control system, vehicle dynamics, stability analysis, and the post-flight telemetry data analysis. | |||||
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: AA0045497013 |