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Control Augmentation System Design for Quad-Tilt-Wing Unmanned Aerial Vehicle via Robust Output Regulation Method
https://jaxa.repo.nii.ac.jp/records/22823
https://jaxa.repo.nii.ac.jp/records/22823cb1bac0a-2daf-4ae4-a967-10bdde952e05
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2017-12-14 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Control Augmentation System Design for Quad-Tilt-Wing Unmanned Aerial Vehicle via Robust Output Regulation Method | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
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 | |||||
著者 |
Tran, Anh Tuan
× Tran, Anh Tuan× 坂本, 登× 佐藤, 昌之× 村岡, 浩治× Tran, Anh Tuan× Sakamoto, Noboru× Sato, Masayuki× Muraoka, Koji |
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著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
南山大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Nanzan University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者(英) | ||||||
出版者 | Institute of Electrical and Electronics Engineers (IEEE) | |||||
書誌情報 |
en : IEEE Transactions on Aerospace and Electronic Systems 巻 53, 号 1, p. 357-369, 発行日 2017-01-16 |
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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 | 0018-9251 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00667591 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1109/TAES.2017.2650618 | |||||
関連名称 | info:doi/10.1109/TAES.2017.2650618 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1720009000 |