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Online Monitor Against Clock and Orbit Ephemeris Faults in ARAIM

机译:在线监视器针对时钟和轨道轨道故障

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This paper describes the design and preliminary evaluation of a new 'Online' ground monitor for advanced receiver autonomous integrity monitoring (ARAIM). ARAIM is intended for vertical guidance of aircraft down to 200 feet altitude. In ARAIM, fault detection is autonomously performed at the airborne receiver using dual-frequency, multi-constellation GNSS. The ARAIM ground monitor aims at validating the assertions made at the airborne receiver on 'integrity parameters', which include, for example, the ranging error variances and prior fault probabilities associated with satellite orbit and clock ephemeris errors. To determine these integrity parameters, two candidate architectures, Offline and Online, are under consideration. Both architectures assume the constellation service providers (CSP) satisfy their service performance commitments. But, in addition, Online ARAIM provides a set of precise 'overlay' orbit and clock ephemeris parameter predictions to replace the CSP navigation message. And, the Online monitor can broadcast hourly updates on the integrity parameters. It follows that probability bounds on integrity parameters can be tightened, which ultimately reduces availability risk as compared to the Offline architecture. On the other hand, Online ARAIM increases 'connectivity risk', as it requires monitor updates to be transmitted from the ground segment to the aircraft. This paper presents an Online monitor concept, which establishes a clear relationship between the monitor's detection test statistic, and the integrity parameters broadcast to the aircraft. The test statistic is derived independently from the Online overlay ephemeris, using code and carrier phase measurements collected at a few worldwide reference stations. Preliminary evaluation of the test statistic distribution is carried out using truth data from the International GNSS Service (IGS), and using covariance analysis. Results suggest that SV position and clock estimation, which is needed to establish the monitor test statistic, is achievable at the decimeter level using a sparse network of ground reference stations.
机译:本文介绍了对高级接收者自主完整性监测(Asaim)的新“在线”地面监视器的设计和初步评价。 Asaim适用于飞机的纵向指导下降到200英尺高度。在Abriaim中,使用双频,多星座GNSS在空中接收器上自主地执行故障检测。 Araim地面监视器旨在验证在“完整性参数”上的空中接收器上的断言,包括例如与卫星轨道和时钟星历错误相关的测距差异和现有故障概率。为了确定这些完整性参数,正在考虑两个候选架构,脱机和在线。这两个架构都假设星座服务提供商(CSP)满足其服务性能的承诺。但另外,在线Asaim提供了一组精确的“叠加”轨道和时钟星历参数预测,以替换CSP导航消息。并且,在线监视器可以在完整性参数上广播每小时更新。因此,可以拧紧完整性参数上的概率范围,这最终与离线架构相比减少了可用性风险。另一方面,在线asim增加了“连接风险”,因为它需要从地面段传输到飞机的监控更新。本文展示了在线监测概念,该概念在监视器的检测测试统计数据之间建立了明确的关系,以及向飞机广播的完整性参数。测试统计量是独立于在线覆盖星历,使用在几个全球参考站收集的代码和载波相位测量来源的。使用来自国际GNSS服务(IGS)的真理数据进行测试统计分布的初步评估,并使用协方差分析。结果表明,使用稀疏地面参考站的稀疏网络在排比水平中可以实现所需的SV位置和时钟估计。

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