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Analysis of kinematics of flapping wing MAV using optitrack systems
https://jaxa.repo.nii.ac.jp/records/3425
https://jaxa.repo.nii.ac.jp/records/3425301bf838-40cc-4d43-9de5-3aa95d39ee23
名前 / ファイル | ライセンス | アクション |
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AA1630046032.pdf (951.7 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2017-04-27 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Analysis of kinematics of flapping wing MAV using optitrack systems | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Motion-capturing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Optitrack | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Kinematics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Fluid-Structure Interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ornithopter MAV | |||||
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 | |||||
著者 |
Rongfa, Matthew NG
× Rongfa, Matthew NG× Pantuphag, Teppatat× Srigrarom, Sutthiphong× Thipyopas, Chinnapat |
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著者所属(英) | ||||||
en | ||||||
University of Glasgow Singapore | ||||||
著者所属(英) | ||||||
en | ||||||
Kasertsart University | ||||||
著者所属(英) | ||||||
en | ||||||
University of Glasgow Singapore | ||||||
著者所属(英) | ||||||
en | ||||||
Kasertsart University | ||||||
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 en : JAXA Special Publication: Proceedings of the First International Symposium on Flutter and its Application 巻 JAXA-SP-16-008E, p. 313-320, 発行日 2017-03-15 |
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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 | First International Symposium on Flutter and its Application (May 15-17, 2016. Mielparque-tokyo), Minato-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents the kinematics of the wing of the ornithopter-like MAV by means of motion-capturing technique (Optitrack). The positions of the marker(s) of one complete oscillation are presented with respect to time in a two-dimensional plane and understand the wing dynamic behaviour of an ornithopter through these graphs. Specifically the wing geometry and kinematics with time in three dimensional space is analysed on the kinematic data of the wing tip path, leading edge bending and trailing edge flap. With the wing geometry obtained, fluid-structure interaction of this flapping wing MAV, by means of CFD. The commercial software ANSYS Fluent is used. | |||||
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 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1630046032 | |||||
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-16-008E |