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アイテム
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Lateral and directional control of winged reentry vehicles: Aileron adverse roll and yaw RCS roll
https://jaxa.repo.nii.ac.jp/records/7627
https://jaxa.repo.nii.ac.jp/records/7627743d0a37-7c08-41ac-9d66-5bc769edfed1
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 | Lateral and directional control of winged reentry vehicles: Aileron adverse roll and yaw RCS roll | |||||
言語 | ||||||
言語 | eng | |||||
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 | 方向安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御理論 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE-X | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エルロン逆効きロール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヨーRCSロール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | RCS | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エルロン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヨー | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 運動方程式 | |||||
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 | directional stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control theory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE-X | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aileron adverse roll | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | yaw RCS roll | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reaction control system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | RCS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aileron | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | yaw | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | controllability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | equation of motion | |||||
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 | 再突入宇宙機の横方向制御:エルロン逆効きロールとヨーRCSロール | |||||
著者 |
米本, 浩一
× 米本, 浩一× Yonemoto, Koichi |
|||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
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15回アストロダイナミクスシンポジウム講演後刷り集 2005 en : Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics p. 401-406, 発行日 2006-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 再突入飛行時に非常に大きな迎角で飛行する有翼式再突入機は、横方向の安定性と制御性に関する困難な問題に直面する。本論文は、我が国の宇宙往還技術試験機HOPE-X(H-2 Orbiting Plane-Exprimental)の開発で得られた知見に基づき、有翼式再突入機の厳しい飛行ダイナミックスについて解析的な理解を示すことを意図している。極超音速飛行マッハ数領域においては、横滑りのエルロンへの補償を伴うバンク角のヨーRCS(Reaction Control System)へのフィードバックが、緩やかな制御ゲインの観点から最も適切な制御方式であることが分かり、HOPE-Xの非常に長い開発を通して得られた最も重要な成果の1つとなった。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Winged reentry vehicles flying at an extremely high angle of attack during their reentry flight encounter difficulties with lateral and directional stability and controllability. This paper aims at a theoretical understanding of the critical flight dynamics of winged reentry vehicles based on the lessons learned from the development of the Japanese experimental space transportation system HOPE-X (H-2 Orbiting Plane-Exprimental). The most important conclusion from what has been gained through the very long development of HOPE-X is that the bank angle feedback to yaw RCS (Reaction Control System) associated with sideslip augmentation by aileron is the most appropriate control law for the hypersonic flight Mach numbers in view of moderate feedback gain. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480062 |