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Analysis of Advanced RAIM Performance Degradation Caused by Integrity Support Message Parameter Errors and Neglecting Nominal Bias Errors

机译:通过完整性支持消息参数错误和忽略标称偏差错误引起的高级RAIM业绩劣化分析

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Advanced Receiver Autonomous Integrity Monitoring (ARAIM) has recently emerged as a promising candidate for future Global Navigation Satellite Systems (GNSS) that has the potential to achieve worldwide Localizer Performance with Vertical Guidance approach operations capability with a decision height as low as 200 ft (LPV-200). A major challenge to enabling ARAIM service is the definition and provision of the ARAIM Integrity Support Message (ISM) that provides statistical characterization of the core GNSS constellations as a priori information to the airborne ARAIM algorithm. This paper presents the results of an analysis of the continuity and integrity, specifically the false alert probability (Pfa) and the probability of hazardous misleading information (Pr{HMI}), of the ARAIM algorithm as a result of core GNSS constellation performance deviation from the performance reflected in broadcast ISM parameter values. A brief summary of the key elements of the current baseline ARAIM algorithm is described to facilitate the presentation of the results of the analysis. This baseline algorithm was developed by the EU-US Cooperative Satellite Navigation Working Group C (WG-C) ARAIM Technical Subgroup (TSG). The analysis shows that both the continuity and integrity degrades with the deviation of true ISM values (i.e., values reflecting actual constellation performance) from the broadcast ISM values. This paper also investigates the sensitivity of Pfa depending on how the ranging signal bias errors in nominal conditions are characterized. The underlying causes of high sensitivity are investigated and explained. Uncovering these underlying causes points to potential solutions that fine-tune the baseline ARAIM algorithm to overcome the high Pfa. A summary of the analysis results and proposed future work are provided at the end of the paper.
机译:高级接收方自主完整性监测(Asaim)最近成为未来全球导航卫星系统(GNSS)的有希望的候选人,这些系统具有垂直指导方法的全球定位性能,具有低至200英尺的决策高度(LPV) -200)。为实现ARAIM服务提供的主要挑战是ABRAIM诚信支持消息(ISM)的定义和提供,该核心GNSS星座的统计表征为空中ARAIM算法的先验信息。本文提出了核心GNSS星座性能偏差的危险算法的危险警报概率(PFA)和危险误导性信息(PR {HMI})的危险误导信息(PR {HMI})的概率结果的结果广播ISM参数值中反映的性能。描述了当前基线Araim算法的关键要素的简要概述,以便于介绍分析结果。该基线算法是由欧盟美国合作卫星导航工作组C(WG-C)Asaim技术亚组(TSG)开发的。该分析表明,连续性和完整性都逐渐降低了来自广播ISM值的真实ISM值(即,反映实际星座性能的值)的偏差。本文还根据标称条件中的测距信号偏差误差的表征方式来研究PFA的灵敏度。研究和解释了高灵敏度的潜在原因。揭示这些潜在的原因指向微调基线Araim算法克服高PFA的潜在解决方案。分析结果摘要和拟议的未来工作在纸张结束时提供。

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