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軽量フレキシブルレクテナ搭載MAVへのマイクロ波自動追尾送電
https://jaxa.repo.nii.ac.jp/records/7958
https://jaxa.repo.nii.ac.jp/records/795838986179-2e54-4e35-8dad-c528100f19eb
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 軽量フレキシブルレクテナ搭載MAVへのマイクロ波自動追尾送電 | |||||
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 | |||||
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(英) | ||||||
その他のタイトル | Auto-Tracking and Transmitting to MAV mounting Light-Weight Flexible Rectenna for Microwave Wireless Power Transmission | |||||
著者 |
澤原, 弘憲
× 澤原, 弘憲× 小田, 章徳× 石場, 舞× 小紫, 公也× 荒川, 義博× 田中, 孝治× Sawahara, Hironori× Oda, Akinori× Ishiba, Mai× Komurasaki, Kimiya× Arakawa, Yoshihiro× Tanaka, Koji |
|||||
著者所属 | ||||||
東京大学大学院新領域創成科学研究科先端エネルギー工学専攻 | ||||||
著者所属 | ||||||
東京大学大学院新領域創成科学研究科先端エネルギー工学専攻 | ||||||
著者所属 | ||||||
東京大学大学院新領域創成科学研究科先端エネルギー工学専攻 | ||||||
著者所属 | ||||||
東京大学大学院新領域創成科学研究科先端エネルギー工学専攻 | ||||||
著者所属 | ||||||
東京大学大学院工学系研究科航空宇宙工学専攻 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Advanced Energy, Graduate School of Frontier Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Advanced Energy, Graduate School of Frontier Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Advanced Energy, Graduate School of Frontier Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Advanced Energy, Graduate School of Frontier Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aeronautics and Astronautics, School of Engineering, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
第30回宇宙エネルギーシンポジウム en : 30th ISAS Space Energy Symposium 発行日 2011-05-17 |
|||||
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30回宇宙エネルギーシンポジウム(2011年2月25日, 宇宙航空研究開発機構宇宙科学研究所相模原キャンパス), 相模原市, 神奈川県 | |||||
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 thirtieth Space Energy Symposium (February 25, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | To realize wireless power feeding to Micro Aerial vehicles, the auto-tracking phased array system was developed. This system consists of three sub-systems, transmitting system, tracking system, and receiving system. At the transmitting system, a 5.8GHz beam was radiated from an active phased array antenna. Transmitting power was 5W and the beam divergence angle was 9deg.. At the tracking system, a position of the MAV was detected by a software-retro-directive function using a 2.45GHz pilot signal and its maximum error was alpha(sub rad)=-1.79deg., alpha(sub azi)=-1.97deg.. At the receiving system, a light-weight flexible patch rectenna was developed. The maximum RF-DC conversion efficiency was 58% at the 100Omega road resistance and 63mW input power. With these systems, the demonstration of auto-tracking wireless power transmission is done. The MAV model with a 10 elements rectenna array was circling using a motor and a supporting bar at the altitude of 1500mm and the rotation radius was 237mm. The motor was rotated constantly. | |||||
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 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: CD-ROM1枚 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Note: One CD-ROM | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324356 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0065107007 |