A miniaturized airplane blade antenna for ...
Document type :
Compte-rendu et recension critique d'ouvrage
Title :
A miniaturized airplane blade antenna for radio navigation and communication systems
Author(s) :
Hamouda, Z. [Auteur]
Faculté des Sciences [Blida]
Azaizia, S. [Auteur]
Faculté des Sciences [Blida]
Nehaoua, M. [Auteur]
Faculté des Sciences [Blida]
Hammouche, M. [Auteur]
Faculté des Sciences [Blida]
Lasri, Tuami [Auteur]
Institut d’Électronique, de Microélectronique et de Nanotechnologie - UMR 8520 [IEMN]
Microtechnology and Instrumentation for Thermal and Electromagnetic Characterization - IEMN [MITEC - IEMN]
Faculté des Sciences [Blida]
Azaizia, S. [Auteur]
Faculté des Sciences [Blida]
Nehaoua, M. [Auteur]
Faculté des Sciences [Blida]
Hammouche, M. [Auteur]
Faculté des Sciences [Blida]
Lasri, Tuami [Auteur]
Institut d’Électronique, de Microélectronique et de Nanotechnologie - UMR 8520 [IEMN]
Microtechnology and Instrumentation for Thermal and Electromagnetic Characterization - IEMN [MITEC - IEMN]
Journal title :
Journal of Electromagnetic Waves and Applications
Pages :
1-16
Publisher :
Taylor & Francis
Publication date :
2024-03-11
ISSN :
0920-5071
HAL domain(s) :
Physique [physics]
Sciences de l'ingénieur [physics]
Sciences de l'ingénieur [physics]
English abstract : [en]
Blade antennas are preferred antenna structures for airborne applications due to their compact size, lightweight and drag-reducing aerodynamic shape. In this paper, we present the design, simulation and realization of a ...
Show more >Blade antennas are preferred antenna structures for airborne applications due to their compact size, lightweight and drag-reducing aerodynamic shape. In this paper, we present the design, simulation and realization of a miniaturized blade antenna requiring a small ground plane and covering the frequency band 0.8–1.1 GHz. To reduce air drag, the proposed antenna is placed inside an aerodynamically optimized airborne radome. The return loss, the radiation patterns and the realized gain of the proposed antenna are studied using HFSS simulations. The comparison of the simulated return loss and radiation patterns to their measured counterpart demonstrates a good agreement. A minimum realized gain of 3.6 dB was achieved at the frequency of 0.9 GHz.Show less >
Show more >Blade antennas are preferred antenna structures for airborne applications due to their compact size, lightweight and drag-reducing aerodynamic shape. In this paper, we present the design, simulation and realization of a miniaturized blade antenna requiring a small ground plane and covering the frequency band 0.8–1.1 GHz. To reduce air drag, the proposed antenna is placed inside an aerodynamically optimized airborne radome. The return loss, the radiation patterns and the realized gain of the proposed antenna are studied using HFSS simulations. The comparison of the simulated return loss and radiation patterns to their measured counterpart demonstrates a good agreement. A minimum realized gain of 3.6 dB was achieved at the frequency of 0.9 GHz.Show less >
Language :
Anglais
Popular science :
Non
Source :