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GNSS Intentional Interference Mitigation via Average KF Innovation and Pseudo Track Updation

机译:通过平均KF创新和伪轨幅更新,GNSS故意干扰缓解

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GNSS based navigation is vulnerable to intentional interferences like jamming, meaconing, and spoofing. In the jamming attack, there is no position estimate from the navigation filter. Whereas, in the case of meaconing and spoofing attacks, the navigation track is misguided by projecting the false measurements onto the GNSS receiver. In the above two cases, the measurements are either corrupted by jamming or spoofed. Therefore, to address this problem, this paper presents a novel pseudo-state update and pseudo-covariance update equations for the Kalman filter (KF) at a given epoch to improve the performance of GNSS track. Simulation results reveals that proposed method enhanced the navigation accuracy (by including two adders, two flip flops and a control unit) compared to other traditional methods. Further, it is evident from the results that the proposed approach provided improved performance in track continuity and position root mean square error(PRMSE) compared to existing techniques.
机译:基于GNSS的导航容易受到干扰,躁动和欺骗等故意干扰的攻击。在干扰攻击中,导航滤波器没有位置估计。虽然,在拍摄和欺骗攻击的情况下,通过将假测量投影到GNSS接收器上,导航轨迹被误导。在上述两种情况下,测量由干扰或欺骗损坏。因此,为了解决这个问题,本文提出了一种在给定时期的Kalman滤波器(KF)的小说伪状态更新和伪协方差更新方程,以提高GNSS轨道的性能。仿真结果表明,与其他传统方法相比,所提出的方法增强了导航精度(通过包括两个加法器,两个触发器和控制单元)。此外,与现有技术相比,所提出的方法在轨道连续性和位置根部均方误差(PRMSE)中提供了改进的性能。

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