针对目前有关GPS欺骗干扰技术的研究较少涉及GPS时间欺骗干扰,且因实验条件限制,难以构建与重放实际欺骗场景,因此不同场景GPS时间欺骗对目标接收机影响仍不明确的问题,基于TEXBAT(Texas Spoofing Test Battery)提供的3组不同场景GPS时...针对目前有关GPS欺骗干扰技术的研究较少涉及GPS时间欺骗干扰,且因实验条件限制,难以构建与重放实际欺骗场景,因此不同场景GPS时间欺骗对目标接收机影响仍不明确的问题,基于TEXBAT(Texas Spoofing Test Battery)提供的3组不同场景GPS时间欺骗数据集,建立了GPS时间欺骗模型,分析了欺骗过程中存在的两种相位对齐模式对欺骗行为的影响;利用自编软件对采集的欺骗场景的原始高保真数字实时数据进行数据处理,分别得到目标接收机受欺骗与未受欺骗时的接收机钟差及钟差变化率、多普勒频率与载噪比、载波相位与接收机天线位置随时间的变化情况;深入分析了不同场景GPS时间欺骗对目标接收机的影响。实验结果表明,不同场景GPS时间欺骗将从不同角度有效影响GPS定时结果,所得结论将为GPS时间欺骗与抗欺骗技术提供重要参考。展开更多
The value range of the failure threshold will generate an uncertain influence on the prediction results for the remaining useful life(RUL) of equipment. Most of the existing studies on the RUL prediction assume that t...The value range of the failure threshold will generate an uncertain influence on the prediction results for the remaining useful life(RUL) of equipment. Most of the existing studies on the RUL prediction assume that the failure threshold is a fixed value,as they have difficulty in reflecting the random variation of the failure threshold. In connection with the inadequacies of the existing research, an in-depth analysis is carried out to study the effect of the random failure threshold(RFT) on the prediction results for the RUL. First, a nonlinear degradation model with unit-to-unit variability and measurement error is established based on the nonlinear Wiener process. Second, the expectation-maximization(EM) algorithm is used to solve the estimated values of the parameters of the prior degradation model, and the Bayesian method is used to iteratively update the posterior distribution of the random coefficients. Then, the effects of three types of RFT constraint conditions on the prediction results for the RUL are analyzed, and the probability density function(PDF) of the RUL is derived. Finally,the degradation data of aero-turbofan engines are used to verify the correctness and advantages of the method.展开更多
Once the spoofer has controlled the navigation sys-tem of unmanned aerial vehicle(UAV),it is hard to effectively control the error convergence to meet the threshold condition only by adjusting parameters of estimation...Once the spoofer has controlled the navigation sys-tem of unmanned aerial vehicle(UAV),it is hard to effectively control the error convergence to meet the threshold condition only by adjusting parameters of estimation if estimation of the spoofer on UAV has continuous observation error.Aiming at this problem,the influence of the spoofer’s state estimation error on spoofing effect and error convergence conditions is theoretically analyzed,and an improved adaptively robust estimation algo-rithm suitable for steady-state linear quadratic estimator is pro-posed.It enables the spoofer’s estimator to reliably estimate UAV status in real time,improves the robustness of the estima-tor in responding to observation errors,and accelerates the con-vergence time of error control.Simulation experiments show that the mean value of normalized innovation squared(NIS)is reduced by 88.5%,and the convergence time of NIS value is reduced by 76.3%,the convergence time of true trajectory error of UAV is reduced by 42.3%,the convergence time of estimated trajectory error of UAV is reduced by 67.4%,the convergence time of estimated trajectory error of the spoofer is reduced by 33.7%,and the convergence time of broadcast trajectory error of the spoofer is reduced by 54.8%when the improved algorithm is used.The improved algorithm can make UAV deviate from pre-set trajectory to spoofing trajectory more effectively and more subtly.展开更多
文摘针对目前有关GPS欺骗干扰技术的研究较少涉及GPS时间欺骗干扰,且因实验条件限制,难以构建与重放实际欺骗场景,因此不同场景GPS时间欺骗对目标接收机影响仍不明确的问题,基于TEXBAT(Texas Spoofing Test Battery)提供的3组不同场景GPS时间欺骗数据集,建立了GPS时间欺骗模型,分析了欺骗过程中存在的两种相位对齐模式对欺骗行为的影响;利用自编软件对采集的欺骗场景的原始高保真数字实时数据进行数据处理,分别得到目标接收机受欺骗与未受欺骗时的接收机钟差及钟差变化率、多普勒频率与载噪比、载波相位与接收机天线位置随时间的变化情况;深入分析了不同场景GPS时间欺骗对目标接收机的影响。实验结果表明,不同场景GPS时间欺骗将从不同角度有效影响GPS定时结果,所得结论将为GPS时间欺骗与抗欺骗技术提供重要参考。
基金supported by the China Postdoctoral Science Foundation(2017M623415)。
文摘The value range of the failure threshold will generate an uncertain influence on the prediction results for the remaining useful life(RUL) of equipment. Most of the existing studies on the RUL prediction assume that the failure threshold is a fixed value,as they have difficulty in reflecting the random variation of the failure threshold. In connection with the inadequacies of the existing research, an in-depth analysis is carried out to study the effect of the random failure threshold(RFT) on the prediction results for the RUL. First, a nonlinear degradation model with unit-to-unit variability and measurement error is established based on the nonlinear Wiener process. Second, the expectation-maximization(EM) algorithm is used to solve the estimated values of the parameters of the prior degradation model, and the Bayesian method is used to iteratively update the posterior distribution of the random coefficients. Then, the effects of three types of RFT constraint conditions on the prediction results for the RUL are analyzed, and the probability density function(PDF) of the RUL is derived. Finally,the degradation data of aero-turbofan engines are used to verify the correctness and advantages of the method.
基金supported by the State Key Laboratory of Geo-Information Engineering(SKLGIE2022-Z-2-1)the National Natural Science Foundation of China(41674024,42174036).
文摘Once the spoofer has controlled the navigation sys-tem of unmanned aerial vehicle(UAV),it is hard to effectively control the error convergence to meet the threshold condition only by adjusting parameters of estimation if estimation of the spoofer on UAV has continuous observation error.Aiming at this problem,the influence of the spoofer’s state estimation error on spoofing effect and error convergence conditions is theoretically analyzed,and an improved adaptively robust estimation algo-rithm suitable for steady-state linear quadratic estimator is pro-posed.It enables the spoofer’s estimator to reliably estimate UAV status in real time,improves the robustness of the estima-tor in responding to observation errors,and accelerates the con-vergence time of error control.Simulation experiments show that the mean value of normalized innovation squared(NIS)is reduced by 88.5%,and the convergence time of NIS value is reduced by 76.3%,the convergence time of true trajectory error of UAV is reduced by 42.3%,the convergence time of estimated trajectory error of UAV is reduced by 67.4%,the convergence time of estimated trajectory error of the spoofer is reduced by 33.7%,and the convergence time of broadcast trajectory error of the spoofer is reduced by 54.8%when the improved algorithm is used.The improved algorithm can make UAV deviate from pre-set trajectory to spoofing trajectory more effectively and more subtly.
