Adaptive Beam Size Design for LEO Satellite Networks with Doppler Shift Compensation

S. Han, W. Lee, W. Shin, Jae-Hyun Kim
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引用次数: 1

Abstract

Over the last few years, Low Earth Orbit (LEO) satellite communication systems have been gaining much attention for fulfilling seamless global coverage requirements for 5G and beyond networks. One of the critical issues in the LEO satellite links is large Doppler shift caused by extremely high mobility of the LEO satellites. Motivated by this, LEO satellite beam size problems are tackled in this paper regarding Doppler shift and the LEO satellite altitudes. We make use of a simple Doppler shift calculation method, and assume a practical Doppler shift compensation scenario to reduce the burden at the ground user terminal. Two STARLINK satellites orbital planes which are in the range of LEO and Very-Low Earth Orbit (VLEO) altitudes are used. We evaluate the bit error rate (BER) performance versus the beam size according to the satellite altitudes, carrier frequency, and subcarrier spacing of Orthogonal Frequency Division Multiplexing (OFDM). The reliable LEO satellite beam size can be decided from the simulation results. Notably, it can help design the beam size of the LEO satellite networks based on 5G standard.
基于多普勒频移补偿的低轨道卫星网络自适应波束设计
在过去几年中,低地球轨道(LEO)卫星通信系统因满足5G及以上网络的无缝全球覆盖要求而备受关注。低轨卫星链路的关键问题之一是由于低轨卫星极高的机动性所引起的大多普勒频移。基于此,本文从多普勒频移和低轨卫星高度两个方面研究了低轨卫星波束尺寸问题。我们采用了一种简单的多普勒频移计算方法,并假设了一个实用的多普勒频移补偿场景,以减轻地面用户终端的负担。使用了两个位于近地轨道和极低地球轨道(VLEO)高度范围内的STARLINK卫星轨道平面。我们根据卫星高度、载波频率和正交频分复用(OFDM)的子载波间隔来评估误码率(BER)性能与波束大小的关系。根据仿真结果可以确定可靠的低轨道卫星波束大小。值得注意的是,它可以帮助设计基于5G标准的低轨道卫星网络的波束大小。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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