Ionospheric Error Models for Satellite-Based Navigation—Paving the Road towards LEO-PNT Solutions

IF 2.6 Q2 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS
Majed Imad, Antoine Grenier, Xiaolong Zhang, J. Nurmi, Elena Simon Lohan
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Abstract

Low Earth Orbit (LEO) constellations have ecently gained tremendous attention in the navigational field due to their arger constellation size, faster geometry variations, and higher signal power evels than Global Navigation Satellite Systems (GNSS), making them favourable for Position, Navigation, and Timing (PNT) purposes. Satellite signals are heavily attenuated from the atmospheric ayers, especially from the ionosphere. Ionospheric delays are, however, expected to be smaller in signals from LEO satellites than GNSS due to their ower orbital altitudes and higher carrier frequency. Nevertheless, unlike for GNSS, there are currently no standardized models for correcting the ionospheric errors in LEO signals. In this paper, we derive a new model called Interpolated and Averaged Memory Model (IAMM) starting from existing International GNSS Service (IGS) data and based on the observation that ionospheric effects epeat every 11 years. Our IAMM model can be used for ionospheric corrections for signals from any satellite constellation, including LEO. This model is constructed based on averaging multiple ionospheric data and eflecting the electron content inside the ionosphere. The IAMM model’s primary advantage is its ability to be used both online and offline without needing eal-time input parameters, thus making it easy to store in a device’s memory. We compare this model with two benchmark models, the Klobuchar and International Reference Ionosphere (IRI) models, by utilizing GNSS measurement data from 24 scenarios acquired in several European countries using both professional GNSS eceivers and Android smartphones. The model’s behaviour is also evaluated on LEO signals using simulated data (as measurement data based on LEO signals are still not available in the open-access community; we show a significant eduction in ionospheric delays in LEO signals compared to GNSS. Finally, we highlight the remaining open challenges toward viable ionospheric-delay models in an LEO-PNT context.
卫星导航电离层误差模型--为低地轨道-全球导航解决方案铺平道路
与全球导航卫星系统(GNSS)相比,低地球轨道(LEO)星座具有更大的星座规模、更快的几何形状变化和更高的信号功率水平,因而有利于定位、导航和授时(PNT)目的,最近在导航领域获得了极大的关注。卫星信号受到大气层,特别是电离层的严重衰减。不过,由于低地轨道卫星的轨道高度较高,载波频率较高,预计其电离层延迟会小于全球导航卫星系统。然而,与全球导航卫星系统不同,目前还没有校正低地轨道信号电离层误差的标准化模型。在本文中,我们从现有的国际全球导航卫星系统服务(IGS)数据出发,根据电离层效应每 11 年重复一次的观测结果,推导出了一个新模型,称为插值和平均记忆模型(IAMM)。我们的 IAMM 模型可用于对包括低地轨道在内的任何卫星星座的信号进行电离层校正。该模型的构建基于多个电离层数据的平均值和电离层内部的电子含量。IAMM 模型的主要优点是能够在线和离线使用,无需实时输入参数,因此易于存储在设备内存中。我们利用在多个欧洲国家使用专业 GNSS 接收器和安卓智能手机获取的 24 个场景的 GNSS 测量数据,将该模型与两个基准模型(Klobuchar 和国际参考电离层 (IRI) 模型)进行了比较。我们还利用模拟数据对模型在低地轨道信号上的表现进行了评估(因为基于低地轨道信号的测量数据在开放获取社区中仍然不可用;我们显示,与全球导航卫星系统相比,低地轨道信号的电离层延迟显著减少。最后,我们强调了在 LEO-PNT 背景下建立可行的电离层延迟模型仍面临的挑战。
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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来源期刊
Computers
Computers COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS-
CiteScore
5.40
自引率
3.60%
发文量
153
审稿时长
11 weeks
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