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Low C/N_0 Carrier Tracking Loop Based on Optimal Estimation Algorithm in GPS Software Receivers 被引量:18

Low C/N_0 Carrier Tracking Loop Based on Optimal Estimation Algorithm in GPS Software Receivers
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摘要 Suppressing jitter noises in a phase locked loop( PLL) is of great importance in order to keep precise and continuous track of global positioning system (GPS)signals characterized by low carrier-to-noise ratio( C/No ). This article proposes and analyzes an improved Kalman-filter-based PLL to process weak carrier signals in GPS software receivers. After reviewing the optimal-bandwidth-based traditional second-order PLL, a Kalman-filter-based estimation algorithm is implemented for the new PLL by decorrelating the model error noises and the measurement noises. Finally,the efficiency of this new Kalman-filter-based PLL is verified by experimental data. Compared to the traditional second-order PLL, this new PLL is in position to make correct estimation of the carrier phase differences and Doppler shifts with less overshoots and noise disturbances and keeps an effective check on the disturbances out of jitter noises in PLL. The results show that during processing normal signals,this improved PLL reduces the standard deviation from 0. 010 69 cycle to 0. 007 63 cycle, and for weak signal processing,the phase jitter range and the Doppler shifts can be controlled within ± 17° and ±5 Hz as against ±25° and + 15 Hz by the traditional PLL. Suppressing jitter noises in a phase locked loop( PLL) is of great importance in order to keep precise and continuous track of global positioning system (GPS)signals characterized by low carrier-to-noise ratio( C/No ). This article proposes and analyzes an improved Kalman-filter-based PLL to process weak carrier signals in GPS software receivers. After reviewing the optimal-bandwidth-based traditional second-order PLL, a Kalman-filter-based estimation algorithm is implemented for the new PLL by decorrelating the model error noises and the measurement noises. Finally,the efficiency of this new Kalman-filter-based PLL is verified by experimental data. Compared to the traditional second-order PLL, this new PLL is in position to make correct estimation of the carrier phase differences and Doppler shifts with less overshoots and noise disturbances and keeps an effective check on the disturbances out of jitter noises in PLL. The results show that during processing normal signals,this improved PLL reduces the standard deviation from 0. 010 69 cycle to 0. 007 63 cycle, and for weak signal processing,the phase jitter range and the Doppler shifts can be controlled within ± 17° and ±5 Hz as against ±25° and + 15 Hz by the traditional PLL.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2010年第1期109-116,共8页 中国航空学报(英文版)
基金 National Natural Science Foundation of China(40671155) National High-tech Research and Development Programof China(2006AA12A108) Research Program of Hong Kong Polytech-nic University(G-U203)
关键词 global positioning system signal processing Kalman filters software radio phase locked loop global positioning system signal processing Kalman filters software radio phase locked loop
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  • 1L Congmin1,2, GU Yidong3, LIN Baojun3 & GUO Jiong3 1. Center for Space Science and Applied Research, Chinese Academy of Sciences, Beijing 100080, China,2. Graduate School of the Chinese Academy of Sciences, Beijing 100039, China,3. General Establishment of Space Science and Application, Chinese Academy of Sciences, Beijing 100080, China,Correspondence should be addressed to L Congmin.Integrated precise orbit determination of Shenzhou IV unmanned spacecraft[J].Science China(Technological Sciences),2004,47(5):518-525. 被引量:1
  • 2Moncef Gabbouj,Edward J. Coyle,Neal C. Gallagher.An overview of median and stack filtering[J].Circuits Systems and Signal Processing.1992(1)

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