Discrete Mathematical Model for GNSS Interference Detection Using ADS-B Quality Parameters

Jakub Steiner, Ivan Nagy
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Abstract

The growing dependence of critical infrastructure on Global Navigation Satellite Systems (GNSS) as an accurate and reliable positioning, navigation and timing (PNT) source gives rise to the importance of GNSS interference detection. Although jamming detection capabilities are present in the current market, predominately in the form of specialised GNSS interference detectors or GNSS receivers add-ons. These provide a limited coverage area and their implementation into critical infrastructure operations is rather slow. Therefore, this paper focuses on the detection of GNSS interference using widespread Automatic Dependent Surveillance-Broadcast (ADS-B) technology. The research builds upon previous work and addresses some of its limitations by developing a discrete mathematical model for GNSS jamming detection based on ADS-B quality parameters. To develop and validate the model, a series of experiments involving GNSS jamming in live-sky environments were conducted. The controlled experiments enabled close monitoring of the aircraft navigation systems allowing for precise determination of the aircraft’s jammed/unjammed status. Approximately 75% of the jamming experiment data was used for model development and tuning, while the remaining 25% was reserved for evaluation. The model evaluation leveraging the confusion matrix showed a positive jamming detection rate of over 99% and a false positive jamming detection rate of under 1%. Additionally, the model was tested on ADS-B data from the Atlantic Ocean where no GNSS jamming is expected. Using this data set the model exhibited an under 1% false positive jamming detection rate.
基于ADS-B质量参数的GNSS干扰检测离散数学模型
关键基础设施越来越依赖全球导航卫星系统(GNSS)作为准确可靠的定位、导航和授时(PNT)源,从而提高了GNSS干扰检测的重要性。虽然目前市场上存在干扰检测能力,但主要以专门的GNSS干扰探测器或GNSS接收器附加组件的形式存在。它们提供的覆盖范围有限,在关键基础设施操作中的实施相当缓慢。因此,本文重点研究了利用广泛的广播自动相关监视(ADS-B)技术检测GNSS干扰。该研究建立在先前工作的基础上,并通过开发基于ADS-B质量参数的GNSS干扰检测的离散数学模型来解决其一些局限性。为了开发和验证该模型,进行了一系列涉及实时天空环境下GNSS干扰的实验。控制实验使飞机导航系统的密切监测能够精确确定飞机的堵塞/非堵塞状态。大约75%的干扰实验数据用于模型开发和调整,而剩余的25%用于评估。利用混淆矩阵的模型评价表明,干扰正检出率大于99%,干扰假正检出率小于1%。此外,该模型还在来自大西洋的ADS-B数据上进行了测试,该数据预计不会受到GNSS干扰。使用该数据集,该模型显示出低于1%的误报干扰检测率。
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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