地表自动相关监视-广播应用中不同电离层条件下的全球定位系统精度

B. Bian, P. Moertl
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引用次数: 4

摘要

基于飞行甲板的广播自动相关监视(ADS-B)的新应用为机场地面操作提供了满足改进的关键安全和经济目标的潜力。具体来说,已经制定了ADS-B应用标准,以减少和防止使用飞行甲板设备的飞机在机场表面上的跑道碰撞。这种应用需要95%的时间内定位精度在10到30米之间的监视信息。没有广域增强系统(WAAS)的全球定位系统(GPS)信息在大多数情况下提供足够的位置精度;然而,显著的太阳耀斑活动可以改变大气层上层的电离特性,从而改变GPS信号的传播,导致定位精度下降,可能使信息无法用于ADS-B的地面应用。本文描述了电离层扰动对单频GPS接收机在一系列假定工作条件下定位精度影响的分析结果。预计研究结果将有助于评估ADS-B地面应用的单频GPS技术,并有助于确定缓解措施。该分析假设了GPS标准定位服务(SPS)性能标准(PS)中定义的标称GPS星座和一组GPS接收器误差模型。这些模型包括对流层、多路径和接收机噪声误差模型,它们要么被GPS WAAS航空接收机性能标准所采用,要么在公开文献中作为实际GPS接收机误差的代表。假定干扰误差为零,假定机场运营当局已降低干扰风险。电离层误差是基于最小、最大和平均太阳活动周期条件下实际GPS导航电文广播值的误差建模的。结果显示了这些活动对各种定位精度参数和水平位置的影响,并包括最坏情况。在假设的模型下,现代GPS接收机在全视场模式下的精度要求总是超过ADS-B地面应用的精度要求,这表明非waas、单频GPS用于ADS-B地面应用的可行性。论文最后概述了研究需求,并提出了下一步的研究方向。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Global positioning system accuracy under varying ionospheric conditions for surface Automatic Dependent Surveillance-Broadcast applications
New flight deck-based applications of Automatic Dependent Surveillance-Broadcast (ADS-B) offer the potential to meet improved critical safety and economic targets for airport surface operations. Specifically, standards for ADS-B applications have been developed [1] to reduce and prevent runway collisions between aircraft on the airport surface using flight deck equipment. Such applications require surveillance information with position accuracy ranging between 10 to 30 meters 95 percent of the time. Global Positioning System (GPS) information without Wide Area Augmentation System (WAAS) provides sufficient position accuracy under most conditions; however, significant solar flare activities can change the ionization characteristics of the upper layers of the atmosphere which alters GPS signal propagation resulting in decreased position accuracy, potentially making the information unusable for ADS-B surface applications. This paper describes the results of an analysis of the impact of ionospheric disturbances on the position accuracy of a single frequency GPS receiver under a range of assumed operational conditions. The results are expected to be useful for an assessment of single frequency GPS technology for ADS-B surface applications and to help identify mitigations. The analysis assumes a nominal GPS constellation as defined in the GPS Standard Positioning Service (SPS) Performance Standards (PS) and a set of GPS receiver errors models. These include tropospheric, multi-path, and receiver noise error models, which are either adopted by the GPS WAAS aviation receiver performance standard or shown in open literature as representative of actual GPS receiver errors. Interference errors are assumed to be zero and interference risks are assumed to have been mitigated by airport operation authorities. The ionospheric errors are modeled based on the errors in actual GPS Navigation Message broadcast values under minimum, maximum, and average solar cycle activity conditions. Results show the impact of these activities on various position accuracy parameters and horizontal position, and include worst case conditions. Given the assumed models, the accuracy requirements for ADS-B surface applications were always exceeded for modern GPS receivers operating in all-in-view mode, suggesting feasibility of non-WAAS, single frequency GPS for ADS-B surface applications. The paper concludes with an outline of research needs and proposed next steps.
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