A Fault Detection Algorithm Using an Adaptive Fading Kalman Filter for Various Types of GNSS Fault

Sun Young Kim, C. Kang, Chan Gook Park
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引用次数: 3

Abstract

In this paper, a fault detection algorithm using an adaptive fading Kalman filter is introduced to detect various types of GNSS fault signal. In order to detect GNSS fault signal, the fading factor of the filter is used as a detection parameter. In simulations, the types of fault signal are represented by the ramp bias error and random bias error of the pseudo range, respectively. The change of the fading factor value according to bias error is used to compare with the detection threshold. In addition, the value of the fading factor is applied to adjust the Kalman gain and the effect of fault signal is mitigated by controlling the Kalman gain of the filter. To verify the performance of the proposed algorithm, two simple simulations are implemented. Through the results of simulation, we confirmed that the proposed algorithm works well when various types of GNSS fault signal exist.
基于自适应衰落卡尔曼滤波的GNSS故障检测算法
本文提出了一种基于自适应衰落卡尔曼滤波的故障检测算法,用于检测各种类型的GNSS故障信号。为了检测GNSS故障信号,采用滤波器的衰落因子作为检测参数。在仿真中,故障信号的类型分别由伪范围的斜坡偏置误差和随机偏置误差表示。利用渐近因子值随偏置误差的变化与检测阈值进行比较。此外,利用衰落因子的值来调整卡尔曼增益,并通过控制滤波器的卡尔曼增益来减轻故障信号的影响。为了验证所提算法的性能,进行了两个简单的仿真。仿真结果表明,该算法在多种GNSS故障信号存在的情况下都能很好地实现故障定位。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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