Massive MIMO Beam ID-Based Positioning Method With Low Earth Orbit Satellite Mega Constellations

IF 3.4 Q2 ENGINEERING, ELECTRICAL & ELECTRONIC
Mahmoud Elsanhoury;Janne Koljonen;Fabricio S. Prol;Mohammed S. Elmusrati;Heidi Kuusniemi
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引用次数: 0

Abstract

The growth of satellite-based positioning methods has revolutionized global navigation by providing reliable geolocation capabilities. However, traditional Global Navigation Satellite Systems (GNSS) are increasingly vulnerable to threats like jamming, spoofing, and interception, undermining their reliability in critical applications such as in-flight navigation and emergency services. To address these challenges, Low Earth Orbit (LEO) satellite constellations have emerged as a promising complement to GNSS infrastructure. LEO satellites, orbiting at lower altitudes with higher density, offer improved signal availability, reduced degradation, and better reception on Earth. This paper presents a LEO satellite-based positioning method via massive multiple-input multiple-output (mMIMO) beamforming antennas. The proposed technique not only mitigates GNSS vulnerabilities but also introduces a passive sensing mechanism that facilitates positioning without complex timing synchronization, improving resilience in jamming-prone environments. By utilizing LEO satellite beam identifiers as geographic pointers, our method enables precise positioning through LEO satellite ephemeris and beam pattern data. We validate this beam-based method through simulations, LEO constellation data, vehicular drive-test datasets, and probabilistic positioning models. Positioning results from the first dataset show a mean absolute error (MAE) of 9.15 meters and a 95th percentile error (p95%) of 19.07 meters when combining LEO satellite data with inertial motion data from a moving vehicle. Meanwhile, GNSS accuracy was MAE = 26.6 meters and p95% = 56.6 meters. The second dataset showed consistent results with accuracy improvements in MAE from 18.55 to 9.42 meters, RMSE from 22.24 to 12.05 meters, and p95% from 36.38 to 21.18 meters, compared to GNSS. These findings highlight the potential of LEO satellite positioning to improve accuracy and reliability in challenging environments, with implications for critical applications such as remote sensing, emergency response, search and rescue, and situational awareness.
基于大规模MIMO波束id的低地球轨道卫星巨型星座定位方法
卫星定位方法的发展通过提供可靠的地理定位能力,彻底改变了全球导航。然而,传统的全球导航卫星系统(GNSS)越来越容易受到干扰、欺骗和拦截等威胁,从而破坏了其在飞行导航和应急服务等关键应用中的可靠性。为了应对这些挑战,低地球轨道(LEO)卫星星座已经成为全球导航卫星系统基础设施的一个有希望的补充。低轨道卫星的轨道高度较低,密度较高,可以提供更好的信号可用性,减少退化,并在地球上获得更好的接收。提出了一种基于低轨道卫星的大规模多输入多输出(mMIMO)波束形成天线定位方法。所提出的技术不仅减轻了GNSS的漏洞,而且还引入了一种被动感知机制,使定位无需复杂的定时同步,从而提高了在容易干扰的环境中的恢复能力。通过利用LEO卫星波束标识符作为地理指针,我们的方法可以通过LEO卫星星历和波束模式数据进行精确定位。我们通过仿真、LEO星座数据、车辆驾驶测试数据集和概率定位模型验证了这种基于波束的方法。第一个数据集的定位结果显示,将LEO卫星数据与移动车辆的惯性运动数据相结合,平均绝对误差(MAE)为9.15米,第95百分位误差(p95%)为19.07米。同时,GNSS精度MAE = 26.6 m, p95% = 56.6 m。与GNSS相比,第二个数据集的MAE精度从18.55米提高到9.42米,RMSE从22.24米提高到12.05米,p95%从36.38米提高到21.18米。这些发现突出了低轨道卫星定位在具有挑战性的环境中提高准确性和可靠性的潜力,对遥感、应急响应、搜索和救援以及态势感知等关键应用具有重要意义。
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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CiteScore
5.70
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