WEKO3
アイテム
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小型飛行体のマイクロ波ソフトウェアリトロディレクティブ追尾システムとその高度化の研究
https://jaxa.repo.nii.ac.jp/records/8001
https://jaxa.repo.nii.ac.jp/records/8001134d0d5f-6c27-4871-a2e0-503950075dd4
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 | 小型飛行体のマイクロ波ソフトウェアリトロディレクティブ追尾システムとその高度化の研究 | |||||
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 | Research of software retro directive tracking system for MAV and sophisticated system | |||||
著者 |
嶋根, 愛理
× 嶋根, 愛理× 高橋, 大祐× 佐々木, 進× 田中, 孝治× 藤野, 義之× 小紫, 公也× Shimane, Eri× Takahashi, Daisuke× Sasaki, Susumu× Tanaka, Koji× Fujino, Yoshiyuki× Komurasaki, Kimiya |
|||||
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 | ||||||
東京大学工学部航空宇宙工学科 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究本部 | ||||||
著者所属 | ||||||
情報通信研究機構 | ||||||
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(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, Faculty of Engineering, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
National Institute of Information and Communications Technology (NICT) | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Advanced Energy, Graduate School of Frontier Science, University of Tokyo | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙エネルギーシンポジウム en : Space Energy Symposium 巻 28, 発行日 2009-06 |
|||||
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28回宇宙エネルギーシンポジウム(2009年3月9日, 宇宙航空研究開発機構宇宙科学研究本部相模原キャンパス) | |||||
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 twenty-eight Space Energy Symposium (March 9, 2009. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Software retro directive tracking system of energy transmission for Micro Aerial Vehicle called MAV has been studied. This system has the battery charge of MAV without landing and take-off enabled. The system is consisted of three subsystems; detecting phase difference system using pilot signal, power transmission system using phased array antenna, and rectenna system. The direction of transmitter antenna was detected in 2D in the detecting phase difference system while the antenna was circling over the system and transmitting pilot signal for simulation of an MAV flight. The accuracy of detecting direction was not over 2 deg. This value was enough because the beam width of the power transmission system is 9 deg. And flexible rectenna made from polymide film and copper foil was developed. The weight of the new rectenna was one-tenth of previous one and it had lower air resistance. Moreover the flexible rectenna was operated with high efficiency when the resistance which is equal to an electric motor for the MAV model was loaded and received enough power for running of it. | |||||
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: AA0064295010 |