Design of Aircraft On-Glass Antennas Using a Coupled Feed Structure

This communication proposes a glass-integrated antenna using a coupled feed structure for military FM radio communications on aircraft. The proposed antenna consists of a feed strip and two radiators, printed on the left-side window of the cockpit. The proposed antenna structure is optimized with th...

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Veröffentlicht in:IEEE transactions on antennas and propagation 2012-04, Vol.60 (4), p.2088-2093
Hauptverfasser: BYUN, Gangil, SEO, Chulhun, JANG, Byung-Jun, CHOO, Hosung
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container_issue 4
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container_title IEEE transactions on antennas and propagation
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creator BYUN, Gangil
SEO, Chulhun
JANG, Byung-Jun
CHOO, Hosung
description This communication proposes a glass-integrated antenna using a coupled feed structure for military FM radio communications on aircraft. The proposed antenna consists of a feed strip and two radiators, printed on the left-side window of the cockpit. The proposed antenna structure is optimized with the genetic algorithm in conjunction with the FEKO EM simulator. The optimized antenna is built and installed on a 1/10-sized KUH-Surion mock-up and antenna performance, such as reflection coefficient and bore-sight gain, is measured in a semi-anechoic chamber. The optimized antenna shows a half-power matching bandwidth of 28% at the center frequency of the military FM radio band and an average bore-sight gain of about -2.60 dBi. The results show that the proposed antenna is suitable for use as a military FM antenna for aircraft applications.
doi_str_mv 10.1109/TAP.2012.2186234
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The proposed antenna consists of a feed strip and two radiators, printed on the left-side window of the cockpit. The proposed antenna structure is optimized with the genetic algorithm in conjunction with the FEKO EM simulator. The optimized antenna is built and installed on a 1/10-sized KUH-Surion mock-up and antenna performance, such as reflection coefficient and bore-sight gain, is measured in a semi-anechoic chamber. The optimized antenna shows a half-power matching bandwidth of 28% at the center frequency of the military FM radio band and an average bore-sight gain of about -2.60 dBi. The results show that the proposed antenna is suitable for use as a military FM antenna for aircraft applications.</description><subject>Aircraft</subject><subject>Aircraft antenna</subject><subject>Aircraft antennas</subject><subject>Aircraft components</subject><subject>Antenna measurements</subject><subject>Antennas</subject><subject>Applied sciences</subject><subject>Broadcasting. 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identifier ISSN: 0018-926X
ispartof IEEE transactions on antennas and propagation, 2012-04, Vol.60 (4), p.2088-2093
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1558-2221
language eng
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source IEEE Electronic Library (IEL)
subjects Aircraft
Aircraft antenna
Aircraft antennas
Aircraft components
Antenna measurements
Antennas
Applied sciences
Broadcasting. Videocommunications. Audiovisual
coupled feed structure
Couplings
Exact sciences and technology
Feeds
FM antenna
Frequency modulation
Gain
Genetic algorithms
glass-integrated antenna
Military
Military aircraft
Miscellaneous
Radio communications
Radiocommunications
Reflection coefficient
Telecommunications
Telecommunications and information theory
title Design of Aircraft On-Glass Antennas Using a Coupled Feed Structure
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