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Flexible polarization demultiplexing method based on an adaptive process noise covariance Kalman filter
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作者 葛军 闫连山 +5 位作者 易安林 盘艳 蒋林 代亮亮 潘炜 罗斌 《Chinese Optics Letters》 SCIE EI CAS CSCD 2018年第6期19-23,共5页
A flexible polarization demultiplexing method based on an adaptive Kalman filter(AKF) is proposed in which the process noise covariance has been estimated adaptively. The proposed method may significantly improve th... A flexible polarization demultiplexing method based on an adaptive Kalman filter(AKF) is proposed in which the process noise covariance has been estimated adaptively. The proposed method may significantly improve the adaptive capability of an extended Kalman filter(EKF) by adaptively estimating the unknown process noise covariance. Compared to the conventional EKF, the proposed method can avoid the tedious and time consuming parameter-by-parameter tuning operations. The effectiveness of this method is confirmed experimentally in 128 Gb/s 16 QAM polarization-division-multiplexing(PDM) coherent optical transmission systems. The results illustrate that our proposed AKF has a better tracking accuracy and a faster convergence(about 4 times quicker)compared to a conventional algorithm with optimal process noise covariance. 展开更多
关键词 EKF PDM Flexible polarization demultiplexing method based on an adaptive process noise covariance Kalman filter QAM
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A new adaptive Kalman filter for navigation systems of carrier-based aircraft 被引量:3
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作者 Lifei ZHANG Shaoping WANG +1 位作者 Maria Sergeevna SELEZNEVA Konstantin Avenirovich NEUSYPIN 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2022年第1期416-425,共10页
The features of carrier-based aircraft’s navigation systems during the approach and landing phases are investigated.A new adaptive Kalman filter with unknown state noise statistics is proposed to improve the accuracy... The features of carrier-based aircraft’s navigation systems during the approach and landing phases are investigated.A new adaptive Kalman filter with unknown state noise statistics is proposed to improve the accuracy of the INS/GNSS integrated navigation system.The adaptive filtering algorithm aims to estimate and adapt the unknown state noise covariance Q in high dynamic conditions,when the measurement noise covariance R is assumed to be known empirically in advance.The new adaptive Kalman filter based on the innovation sequence and pseudo-measurement vector approach makes it more effective to estimate and adapt Q.The simulation results and semi-physical experiments show that the application of the proposed adaptive Kalman filter can guarantee a higher estimation accuracy of the state variables. 展开更多
关键词 Adaptive filters Apriori statistics Deck landing aircraft Innovation sequence State noise covariance
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