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Differential RAIM and relative RAIM for orbit ephemeris fault detection

机译:差分RAIM和相对RAIM用于轨道星历的故障检测。

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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.
机译:本文介绍了用于监测影响舰载机着陆应用中差分载波相位测量的轨道星历故障的新型监测器。首先设计了两个舰载监视器。它们在针对两种目标故障类型提供高检测性能的同时,对其他类型的星历表故障无效。作为响应,为了保护用户免受整个威胁空间的侵害,开发了一种新的机载接收机自主完整性监控(RAIM)算法。这种“统一”的RAIM方法(URAIM)既利用了差分RAIM(在大于5 nmi的飞艇分离距离时效率最高),又利用了相对RAIM(相反,当飞机接近船舶时,其性能更好)。性能评估表明,URAIM具有使用单一统一的基于残差的RAIM方法检测所有类型的星历故障的潜力。

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