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模型飛行機を用いた飛行運動と表面圧力場変動の解析
https://jaxa.repo.nii.ac.jp/records/49161
https://jaxa.repo.nii.ac.jp/records/491611823ede7-7f62-4967-a077-362a285d3a7c
名前 / ファイル | ライセンス | アクション |
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AA2230023030.pdf (2.6 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2023-02-17 | |||||
タイトル | ||||||
タイトル | 模型飛行機を用いた飛行運動と表面圧力場変動の解析 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Correlation Analysis of Flight Motions and Surface Flow Fields using Actual Flight Data of Model Aircraft | |||||
著者 |
関野, 秀都
× 関野, 秀都× 牧, 緑× SEKINO, Shuto× MAKI, Midori |
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著者所属 | ||||||
東京都立大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空技術部門(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Aviation Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第54回流体力学講演会/第40回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 54th Fluid Dynamics Conference / the 40th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-22-007, p. 349-361, 発行日 2023-02-17 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第54回流体力学講演会/第40回航空宇宙数値シミュレーション技術シンポジウム (2022年6月29日-7月1日. いわて県民情報交流センター(アイーナ)), 盛岡市, 岩手 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The 54th Fluid Dynamics Conference / the 40th Aerospace Numerical Simulation Symposium (June 29 - July 1, 2022. Iwate Citizen Information Exchange Center (Aiina)), Morioka, Iwate, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The authors have investigated the possibility of utilizing inflight partial pressure field sensing for flight control especially for gust alleviation in severe turbulence environments. In addition to increasing the amount of feedback information, it is important to clarify how the utilization of pressure fields contributes to improved control performance and reliability. The aim of this study is to extract some principal components of the flow field in real time according to the control objectives, and to use this for an adaptive flight control system. As a preparation, we will analyze the principal components of the flow field and correlation coefficients with various motion quantities using actual flight data of model aircraft. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA2230023030 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-22-007 |