2021
DOI: 10.1109/tcpmt.2021.3118108
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Structurally Integrated Radar in an Aerospace Composite Laminate

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Cited by 7 publications
(4 citation statements)
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“…Then, once the laminate had been cured, silver ink was additively printed onto the back surface to create the remaining parts of the control circuitry. Follow-up work by the authors also described a more complex demonstration of an integrated FMCW radar front-end transceiver using a similar approach [179].…”
Section: B Manufacturing Techniquesmentioning
confidence: 99%
See 1 more Smart Citation
“…Then, once the laminate had been cured, silver ink was additively printed onto the back surface to create the remaining parts of the control circuitry. Follow-up work by the authors also described a more complex demonstration of an integrated FMCW radar front-end transceiver using a similar approach [179].…”
Section: B Manufacturing Techniquesmentioning
confidence: 99%
“…The integration of photovoltaic cells into UAS structures has had a long-and well-established history. Review on this technology can be form in [177], [178], [179]. There are also several successful testbed platforms (such as AeroVironment/NASA HELIOS and BAE PHASA-35).…”
Section: B Eletrical Electronics and Rf Systemsmentioning
confidence: 99%
“…Over the years, several developments have been proposed in this regard such as surface antenna structures, composite smart structures and 3D integrated microstrip antenna structures to further enhance structural and electrical efficiency [ 4 , 5 , 6 , 7 , 8 ]. Recently, a frequency-modulated continuous wave (FMCW) radar front-end was embedded inside an aerospace composite [ 9 ]. The manufacturing process for highly integrated embedded antennas is very complex and can lead to irregularities.…”
Section: Introductionmentioning
confidence: 99%
“…Conformal load-bearing antenna structures (CLAS) offer the opportunity to integrate communication and sensing capabilities into load-bearing airframes [ 1 , 2 , 3 ], as illustrated in Figure 1 . Microstrip patch antennas are one simple example that can easily be integrated into typical conformal airframe structures.…”
Section: Introductionmentioning
confidence: 99%