Differential RAIM and relative RAIM for orbit ephemeris fault detection

M. Joerger, S. Stevanovic, S. Khanafseh, B. Pervan
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引用次数: 4

Abstract

This paper introduces new monitors for the detection of orbit ephemeris faults affecting differential carrier phase measurements in a shipboard aircraft landing application. Two shipboard monitors are first designed. While they provide high detection performance against two targeted fault types, they are ineffective against the other types of orbit ephemeris faults. In response, to protect the user against the entire threat space, a new airborne receiver autonomous integrity monitoring (RAIM) algorithm is developed. This `unified' RAIM approach (URAIM) exploits both differential RAIM (which is most efficient at airship separation distances larger than 5 nmi) and relative RAIM (which, in contrast, performs better as the aircraft approaches the ship). Performance evaluations demonstrate URAIM'm potential to detect all types of orbit ephemeris faults using a single, unified residual-based RAIM method.
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差分RAIM和相对RAIM用于轨道星历故障检测
本文介绍了一种用于检测影响舰载飞机着陆差分载波相位测量的轨道星历故障的新型监测仪。首先设计了两个船载监视器。虽然它们对两种目标故障类型提供了较高的检测性能,但对其他类型的轨道星历故障却无效。为此,为了保护用户免受整个威胁空间的侵害,提出了一种新的机载接收机自主完整性监测算法。这种“统一”雷姆方法(URAIM)利用差分雷姆(在飞艇分离距离大于5海里时最有效)和相对雷姆(相反,当飞机接近船只时表现更好)。性能评估表明,URAIM有潜力使用单一的、统一的基于残差的RAIM方法检测所有类型的轨道星历故障。
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