WEKO3
アイテム
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Guidance and control for High Speed Flight Demonstration Phase 2
https://jaxa.repo.nii.ac.jp/records/7722
https://jaxa.repo.nii.ac.jp/records/772296e527df-b083-40f1-85d5-23ea81ce6123
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 | Guidance and control for High Speed Flight Demonstration Phase 2 | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 誘導・制御システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行実証 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高速 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙往還技術試験機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再突入機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 成層圏気球 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行シミュレーション | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | guidance and control system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight demonstration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high speed | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE aerospace plane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reentry vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic speed | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stratospheric balloon | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight simulation | |||||
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 | 高速飛行実証フェーズ2の誘導制御系 | |||||
著者 |
塚本, 太郎
× 塚本, 太郎× 鈴木, 広一× 西澤, 剛志× 大野, 正博× Tsukamoto, Taro× Suzuki, Hirokazu× Nishizawa, Takeshi× Ono, Masahiro |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
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(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
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. 130-135, 発行日 2004-02 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 高速飛行実証(その2)は宇宙往還機の遷音速領域での空力特性を取得するための飛行実験である。本実験においては、実験機は高層気球によって高度20から30kmに打ち上げられ、分離されて加速し、遷音速での滑空飛行を実現する。有用な空力データを取得するために誘導制御系に対しては実験機のマッハ数を一定に保ちつつ迎角を準性的に変化させることが要求される。また、データ取得後は、選択された回収目標点に適切な終端条件で到達するように機体を誘導しなければならない。ここでは、このような要求を満足するための誘導制御系の設計および飛行試験結果について紹介する | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The High-Speed Flight Demonstration Phase 2 is a night experiment program to investigate the transonic aerodynamic characteristics of the HOPE-X winged re-entry vehicle. A vehicle based on a scaled HOPE-X configuration is lifted by stratospheric balloon to an altitude of 20 to 30 km from where it is released and accelerates to transonic speeds in free-fall. To acquire useful aerodynamic data, the guidance and control system must maintain vehicle's Mach number at a constant value while varying its angle of attack quasi-statically. After data acquisition, the vehicle must be guided to a selected recovery point and attain suitable recovery parameters. In this paper, the design of a guidance and control law to achieve these requirements is described, and its evaluation by non-linear flight simulation is presented. | |||||
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: AA0046652021 |