@inproceedings{oai:jaxa.repo.nii.ac.jp:00008001,
 author = {嶋根, 愛理 and 高橋, 大祐 and 佐々木, 進 and 田中, 孝治 and 藤野, 義之 and 小紫, 公也 and Shimane, Eri and Takahashi, Daisuke and Sasaki, Susumu and Tanaka, Koji and Fujino, Yoshiyuki and Komurasaki, Kimiya},
 book = {宇宙エネルギーシンポジウム, Space Energy Symposium},
 month = {Jun},
 note = {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), The twenty-eight Space Energy Symposium (March 9, 2009. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara), 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., 資料番号: AA0064295010},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {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},
 volume = {28},
 year = {2009}
}