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An Adaptive INS-Aided PLL Tracking Method for GNSS Receivers in Harsh Environments

机译:恶劣环境中GNSS接收器的自适应Ins-辅助PLL跟踪方法

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摘要

As the weak link in global navigation satellite system (GNSS) signal processing, the phase-locked loop (PLL) is easily influenced with frequent cycle slips and loss of lock as a result of higher vehicle dynamics and lower signal-to-noise ratios. With inertial navigation system (INS) aid, PLLs' tracking performance can be improved. However, for harsh environments with high dynamics and signal attenuation, the traditional INS-aided PLL with fixed loop parameters has some limitations to improve the tracking adaptability. In this paper, an adaptive INS-aided PLL capable of adjusting its noise bandwidth and coherent integration time has been proposed. Through theoretical analysis, the relation between INS-aided PLL phase tracking error and carrier to noise density ratio (C/N-0), vehicle dynamics, aiding information update time, noise bandwidth, and coherent integration time has been built. The relation formulae are used to choose the optimal integration time and bandwidth for a given application under the minimum tracking error criterion. Software and hardware simulation results verify the correctness of the theoretical analysis, and demonstrate that the adaptive tracking method can effectively improve the PLL tracking ability and integrated GNSS/INS navigation performance. For harsh environments, the tracking sensitivity is increased by 3 to 5 dB, velocity errors are decreased by 36% to 50% and position errors are decreased by 6% to 24% when compared with other INS-aided PLL methods.
机译:作为全球导航卫星系统(GNSS)信号处理的弱链路,锁相环(PLL)容易受到频繁循环滑动和锁丢失,由于更高的车辆动态和较低的信噪比。通过惯性导航系统(INS)辅助,可以提高PLL的跟踪性能。然而,对于具有高动态和信号衰减的恶劣环境,具有固定环路参数的传统Ins-辅助PLL具有提高跟踪适应性的一些限制。本文已经提出了一种能够调整其噪声带宽和相干积分时间的自适应Ins-辅助PLL。通过理论分析,建立了Ins-Affive PLL相位跟踪误差与噪声密度比(C / N-0),车辆动态,AIVEIDEM更新时间,噪声带宽和相干集成时间之间的关系。在最小跟踪误差标准下,关系公式用于为给定应用程序选择最佳集成时间和带宽。软件和硬件仿真结果验证了理论分析的正确性,并证明了自适应跟踪方法可以有效地提高PLL跟踪能力和集成的GNSS / INS导航性能。对于恶劣环境,跟踪灵敏度增加3至5dB,与其他Ins-Agl方法相比,速度误差降低36%至50%至50%至50%,并且位置误差减小6%至24%。

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