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- W4360897653 abstract "A low-profile, wide-scanning phased-array antenna of vertical bowtie elements fully integrated with a structurally efficient radome and ribs of an aircraft fuselage is proposed in this article. The array is designed to simultaneously fulfill the electrical requirements of an airborne antenna sensor and the mechanical requirements of a load-carrying aircraft fuselage. The array antenna is capable of steering the beam up to <inline-formula xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink> <tex-math notation=LaTeX>$pm mathrm{80}^{circ} $ </tex-math></inline-formula> in the azimuth plane over a 20% bandwidth (2.4–3 GHz) with the active reflection coefficient ( <inline-formula xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink> <tex-math notation=LaTeX>$Gamma _{act}$ </tex-math></inline-formula> ) below −10 dB in an infinite array environment. Experimental results of a <inline-formula xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink> <tex-math notation=LaTeX>$16 times 16$ </tex-math></inline-formula> element array demonstrator agree well with the simulation results. The <inline-formula xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink> <tex-math notation=LaTeX>$16 times 16$ </tex-math></inline-formula> array antenna is capable of steering the beam up to <inline-formula xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink> <tex-math notation=LaTeX>$pm mathrm{60}^{circ} $ </tex-math></inline-formula> and <inline-formula xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink> <tex-math notation=LaTeX>$pm mathrm{75}^{circ} $ </tex-math></inline-formula> with the bandwidth of 20% and 10%, respectively, at <inline-formula xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink> <tex-math notation=LaTeX>$Gamma _{act}leq -10$ </tex-math></inline-formula> dB. The array antenna also achieved good stiffness and performed well in the vibration loads of commercial transport aircraft." @default.
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- W4360897653 date "2023-05-01" @default.
- W4360897653 modified "2023-10-16" @default.
- W4360897653 title "A Wide-Scanning Array Antenna of Connected Vertical Bowtie Elements Structurally Integrated Within an Aircraft Fuselage" @default.
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- W4360897653 doi "https://doi.org/10.1109/tap.2023.3259727" @default.
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