Wireless Power Transfer to a Microaerial Vehicle with a Microwave Active Phased Array

A wireless power transfer system using a microwave active phased array was developed. In the system, power is transferred to a circling microaerial vehicle (MAV) by a microwave beam of 5.8 GHz, which is formed and directed to the MAV using an active phased array antenna. The MAV is expected to suppo...

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Main Authors: Shotaro Nako, Kenta Okuda, Kengo Miyashiro, Kimiya Komurasaki, Hiroyuki Koizumi
Format: Article
Language:English
Published: Hindawi Limited 2014-01-01
Series:International Journal of Antennas and Propagation
Online Access:http://dx.doi.org/10.1155/2014/374543
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spelling doaj-b0cc19b780a74920872f0573daad91c22020-11-24T21:02:53ZengHindawi LimitedInternational Journal of Antennas and Propagation1687-58691687-58772014-01-01201410.1155/2014/374543374543Wireless Power Transfer to a Microaerial Vehicle with a Microwave Active Phased ArrayShotaro Nako0Kenta Okuda1Kengo Miyashiro2Kimiya Komurasaki3Hiroyuki Koizumi4Department of Aeronautics and Astronautics, The University of Tokyo, Bunkyo-ku, Tokyo 113-8656, JapanDepartment of Aeronautics and Astronautics, The University of Tokyo, Bunkyo-ku, Tokyo 113-8656, JapanDepartment of Advanced Energy, The University of Tokyo, Kashiwa-shi, Chiba 277-8561, JapanDepartment of Advanced Energy, The University of Tokyo, Kashiwa-shi, Chiba 277-8561, JapanResearch Center for Advanced Science and Technology, The University of Tokyo, Meguro-ku, Tokyo 153-8904, JapanA wireless power transfer system using a microwave active phased array was developed. In the system, power is transferred to a circling microaerial vehicle (MAV) by a microwave beam of 5.8 GHz, which is formed and directed to the MAV using an active phased array antenna. The MAV is expected to support observation of areas that humans cannot reach. The power beam is formed by the phased array with eight antenna elements. Input power is about 5.6 W. The peak power density at 1,500 mm altitude was 2.63 mW/cm2. The power is sent to a circling MAV. Therefore, the transfer beam should be polarized circularly to achieve a constant power supply independent of its yaw angle. To minimize the polarization loss, a sequentially routed antenna (SRA) was applied to the transmitter antenna. Results show that the axial ratio of 0.440 dB was accomplished and that power fluctuation was kept below 1%.http://dx.doi.org/10.1155/2014/374543
collection DOAJ
language English
format Article
sources DOAJ
author Shotaro Nako
Kenta Okuda
Kengo Miyashiro
Kimiya Komurasaki
Hiroyuki Koizumi
spellingShingle Shotaro Nako
Kenta Okuda
Kengo Miyashiro
Kimiya Komurasaki
Hiroyuki Koizumi
Wireless Power Transfer to a Microaerial Vehicle with a Microwave Active Phased Array
International Journal of Antennas and Propagation
author_facet Shotaro Nako
Kenta Okuda
Kengo Miyashiro
Kimiya Komurasaki
Hiroyuki Koizumi
author_sort Shotaro Nako
title Wireless Power Transfer to a Microaerial Vehicle with a Microwave Active Phased Array
title_short Wireless Power Transfer to a Microaerial Vehicle with a Microwave Active Phased Array
title_full Wireless Power Transfer to a Microaerial Vehicle with a Microwave Active Phased Array
title_fullStr Wireless Power Transfer to a Microaerial Vehicle with a Microwave Active Phased Array
title_full_unstemmed Wireless Power Transfer to a Microaerial Vehicle with a Microwave Active Phased Array
title_sort wireless power transfer to a microaerial vehicle with a microwave active phased array
publisher Hindawi Limited
series International Journal of Antennas and Propagation
issn 1687-5869
1687-5877
publishDate 2014-01-01
description A wireless power transfer system using a microwave active phased array was developed. In the system, power is transferred to a circling microaerial vehicle (MAV) by a microwave beam of 5.8 GHz, which is formed and directed to the MAV using an active phased array antenna. The MAV is expected to support observation of areas that humans cannot reach. The power beam is formed by the phased array with eight antenna elements. Input power is about 5.6 W. The peak power density at 1,500 mm altitude was 2.63 mW/cm2. The power is sent to a circling MAV. Therefore, the transfer beam should be polarized circularly to achieve a constant power supply independent of its yaw angle. To minimize the polarization loss, a sequentially routed antenna (SRA) was applied to the transmitter antenna. Results show that the axial ratio of 0.440 dB was accomplished and that power fluctuation was kept below 1%.
url http://dx.doi.org/10.1155/2014/374543
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