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Stream/Area:
-
Subject:
-
Paper ID:
IJSREM65903
Volume:
10 |
7 |
Jul 2026
Pages:
1-6
Publication Frequency:
Monthly (12 issues per year)
License:International Journal of Scientific Research in Engineering and Management follows the Creative Commons Attribution 4.0 (CC BY 4.0) License, allowing free use and distribution with proper attribution.

Department of Electronics and Communication Engineering
JNTUGV- CEV

Department of Electronics and Communication Engineering
JNTUGV- CEV

Department of Electronics and Communication Engineering
JNTUGV- CEV
Unmanned Aerial Vehicle (UAV) increasingly demand compact, lightweight, and multifunctional antennas capable of supporting both wireless power transfer (WPT) and communication networks across multiple frequency bands. This paper presents the design, simulation, fabrication, and performance evaluation of a multi-band microstrip patch antenna targeting operation at 2.4 GHz, 3.5 GHz and 5.8 GHz frequency channels. The proposed antenna architecture integrates slot-loaded patch techniques on a single substrate to achieve distinct multi-band resonance while maintaining radiation characteristics suitable for localized RF energy harvesting and data links. Full-wave electromagnetic simulation conducted in CST Microwave Studio confirms strong impedance matching below the standard -10 dB return loss threshold, yielding simulated resonant frequencies at 2.32 GHz (-21 dB), 3.52 GHz (-15 dB) and 5.75 GHz (-16.7 dB). To validate the design, a physical prototype was fabricated on a low-profile dielectric substrate using an inset-fed microstrip transmission line and an SMA connector. Experimental evaluation of the hardware via a Vector Network Analyzer (VNA) demonstrates successful practical deployment, exhibiting actual resonances at 2.31 GHz (-13.6 dB), 3.65 GHz (-20.8 dB), and 6.09 GHz (-16.8 dB). The resulting single-element design offers a compact, lightweight, and highly integrated RF front-end solution for modern UAV platforms requiring simultaneous power reception and wireless communication.
KEYWORDS
This paper successfully demonstrated the design, optimization, and hardware realization of a compact, low-profile, tri-band microstrip patch antenna engineered for modern Unmanned Aerial Vehicle (UAV) platforms. By utilizing a slot-loaded patch architecture on an FR4 dielectric substrate, the design overcomes the single-resonance limitations of conventional patches to enable concurrent operation across 2.4 GHz, 3.5 GHz, and 5.8 GHz within a single, lightweight radiating element. Full-wave electromagnetic simulations conducted in CST Microwave Studio established a solid baseline with strong impedance matching (S11 < -10 dB). Subsequent fabrication and hardware testing using a Vector Network Analyzer (VNA) validated the physical feasibility of the design, yielding prominent measured resonances at 2.31 GHz, 3.65 GHz, and 6.09 GHz. Minor deviations between the numerical models and the experimental prototype are reasonably attributed to practical fabrication tolerances, SMA connector soldering effects, and slight variations in the substrate's dielectric constant. Ultimately, this single-element, multi-band configuration minimizes the aerodynamic drag and structural footprint on the aircraft fuselage that would otherwise be caused by mounting multiple single-band antennas. By effectively accommodating both localized RF wireless power transfer (WPT) and high-throughput communication data links simultaneously, the proposed antenna front-end serves as a highly integrated, self-sustaining solution for next-generation drone infrastructures and long-endurance aerial operations. Future work will focus on characterizing the absolute far-field radiation patterns in an anechoic chamber, integrating the prototype into a complete rectenna network to evaluate RF-to-DC conversion efficiencies, and exploring advanced aerodynamic optimization techniques to further enhance platform stability without degrading electromagnetic performance.
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Publication Date
7/9/2026
Peer Review Type
Double-Blind Peer Review
Review Rounds: 2
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