Abstract

This work presents the use of a three-element radiating structure for circularly polarized Low-Power Wide Area Network (LP-WAN) communication with space. The proposed structure has a 72 mm × 72 mm × 12 mm compact size with Right-Handed Circular Polarization (RHCP) and a 120∘ wide beamwidth radiation pattern. Printed on low-cost FR4 Epoxy substrate, a feeding network circuit based on Quasi Lumped Quadrature Coupler (QLQC), it achieves a −0.6 dB insertion loss and a very compact size. The final structure has a 69% total efficiency and a 3.14 dBic realized gain.

Highlights

  • In the last decade, Low Power Wide Area Network (LPWAN) technology came out as a perfect choice for enabling longer range connections at a lower cost and more efficient power consumption [1].The number of connected objects is expected to reach 41.6 billion in 2025 [2]

  • Several Internet of Things (IoT) use cases must be deployed in isolated areas without any mobile terrestrial coverage or other forms of connectivity

  • In order to avoid polarization mismatch losses between the devices and the satellite, which are caused by their dissimilar orientations, circular polarization (CP) is preferred

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Summary

Introduction

Low Power Wide Area Network (LPWAN) technology came out as a perfect choice for enabling longer range connections at a lower cost and more efficient power consumption [1]. On the basis of this idea, several projects are developing an IoT solution that provides a connecting link between the nodes on earth and a constellation of low earth orbit (LEO) CubeSat satellites To deploy such a scenario, a terrestrial antenna with specifications such as a compact size, high efficiency, and low cost are needed [4]. The proposed structures in these references use the low-loss dielectric substrates, which are expensive for industrial application To solve this cost problem, the antenna in [15] is fabricated on FR4-Epoxy, which is a low-cost material. Due to the high-loss substrate, this design provides a −0.6 dBic gain at 915 MHz. In this paper, we propose to study a terrestrial compact antenna for LPWAN space communication on a low-cost substrate. Considering a Low-Earth-Orbit satellite constellation, a wide angle radiation pattern is desired to enable communication with the satellite even at a low-elevation angle

Radiating Elements
Tri-Fillar Antenna with Proposed Feeding System
Prototype Fabrication
Antenna Measurements
Findings
Conclusions

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