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Flow control with pitching motion of UAV using MEMS flow sensors
https://jaxa.repo.nii.ac.jp/records/5531
https://jaxa.repo.nii.ac.jp/records/5531012d9abc-8578-44f8-a52b-04ba67b7cbf8
名前 / ファイル | ライセンス | アクション |
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63908010.pdf (807.1 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Flow control with pitching motion of UAV using MEMS flow sensors | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 無人航空機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ピッチングモーメント | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ピッチ角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 自動飛行制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風速 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | MEMS | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | トリム飛行 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unmanned aerial vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pitching moment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pitch angle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | automatic flight control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind velocity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MEMS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trimmed flight | |||||
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 |
得竹, 浩
× 得竹, 浩× 砂田, 茂× 藤永, 仁× 大塚, 有企朗× Tokutake, Hiroshi× Sunada, Shigeru× Fujinaga, Jin× Otsuka, Yukio |
|||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
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: 境界層遷移の解明と制御研究会講演論文集 第40回 en : JAXA Special Publication: Proceedings of the 40th JAXA Workshop on Investigation and Control of Boundary-Layer Transition 巻 JAXA-SP-07-026E, p. 31-34, 発行日 2008-02-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A new pitch controller for our developed small airplane was designed, and its ability was confirmed by simulation. In the pitch controller, outputs from the MEMS (Micro Electro Mechanical System) flow sensor and the transfer function determined by the results of the wind tunnel tests are used. MEMS technology is a key technology of this pitch controller. | |||||
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: AA0063908010 | |||||
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-07-026E |