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适用于多模接收机的RAIM算法 被引量:2

RAIM algorithm used in multimode receiver
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摘要 为保证接收机工作在多系统环境时仍具有完好性检测性能,针对传统算法在不同测距标准差时,较小测距标准差对应卫星的虚警率上升,且出现故障时对其正确检测能力下降的问题,在传统最优奇偶矢量法的基础上提出一种改进算法—加权最优奇偶矢量法。经蒙特卡罗仿真证明:该算法在有效抑制低测距标准差对应卫星虚警率的同时,也有效地提高了对此类卫星发生故障时的正确检测能力。 Based on the traditional optimal parity vector algorithm, an improved algorithm, weighted optimal parity vector algorithm, is proposed to ensure receivers' performance of autonomous integrity monitoring function under multisystem environment. This new algorithm effectively solves the problem of a rising false alarm probability and declining detection ability for satellites with small ranging standard deviation values compared to those with larger ones. Monte Carlo simulations show that the new algorithm effectively reduces the false alarm probability and significantly improves the ability of successful detection for satellites with small ranging standard deviation values.
出处 《信息与电子工程》 2012年第3期252-256,共5页 information and electronic engineering
基金 国家"863计划"资助项目(2007AA12Z336 2009AA12Z313)
关键词 多模接收机 接收机自主完好性检测(RAIM) 最优奇偶矢量法 蒙特卡罗仿真 muitimode receiver Receiver Autonomous Integrity Monitoring(RAIM) optimal parity vector Monte Carlo simulation
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  • 1陈一虹.导航系统的仿真及实时性研究[M].北京:北京航空航天大学,1996..
  • 2LIU J.GPS RAIM:statistics based improvement on the calculation of threshold and horizontal protection radius[C] //Proc of International Symposium on GPS/GNSS.2005:8-10.
  • 3OBER P B.Integrity prediction and monitoring of navigation systems[D].Netherlands:Delft University of Technology,2003.
  • 4SHANK C,LAVRAKAS J.GPS integrity:an MCS perspective[C] //Proc of ION GPS-93,the 6th International Technical Meeting of the Satellite Division of the Institute of Navigation.1993:465-474.
  • 5PENNY G P,WEESE J,LITTLE J A,et al.A comparison of similarity measures for use in 2D or 3D medical image registration[J].IEEE Trans on Image Processing,1998,17(4):586-595.
  • 6OBER P B.New generally applicable metrics for RAIM/AAIM integrity monitoring[C] //Proc of ION CPS-96,the 9th International Technical Meeting of the Satellite Division of the Institute of Navigation.1996:1677-1686.
  • 7LEE Y C.Performance of receiver autonomous integrity monitoring (PALM) in the presence of simultaneous multiple satellite faults[C] //Proc of ION,the 60th Annual Meeting/U.S.Air Force Institute of Technology and The U.S.Air Force Research Laboratory,Sensors Directorate.2004:7-9.
  • 8BROWN R G.Solution of the two-failure GPS PAIM problem under worst-case bias conditions:parity space approach[J].NAVIGATION,1997,44.(4):425-431.
  • 9BROWN A K,STURZA M A.The effect of geometry on integrity monitoring performance[C] //Proc of the ION Annual Meeting.1990:121-129.
  • 10BROWN A K,STURZA M A.Comparison of fixed and variable threshold RAIM algorithms[C] //Proc of ION.1990:437-443.

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同被引文献16

  • 1於宗俦,李明峰.多维粗差的同时定位与定值[J].武汉测绘科技大学学报,1996,21(4):323-329. 被引量:88
  • 2BAARDA W. A testing procedure for use in geodetic net- works [ M ]. Delft : Netherlands Geodetic Commissio, 1968.
  • 3Brown R G. A Baseline GPS RAIM scheme and a note on the equivalence of three RAIM methods [ J ]. Navigation, 1992,39(3) :301 -316.
  • 4Hewitson S, Wang J L. GNSS Receiver Autonomous In- tegrity Monitoring (RAIM) performance analysis [ J ]. GPS Solutions ,2006,9 ( 10 ) : 155 - 170.
  • 5Liu R H, Zhan X L.Study of RAIM Algorithm and Availabil- ity Analysis Under COMPASS[ C ]//IEEE 2011 : 4346-4349.
  • 6Lee Y. Analysis of Range and Position Comparison Methods as a Means to Provide GPS Integrity in the User Receiver [ C ]// ION AM 1986,Seattle,WA,USA, 1986.
  • 7Parkinson B, Axelrad P. Autonomous GPS Integrity Monitor- ing Using the Pseudorange Residual [J].Navigation: Journal of the Institute of Navigation, 1988,35 (2) : 255-274.
  • 8Sturza M. Navigation System Integrity Monitoring Using Re- dundant Measurements [ J ]. Navigation: Journal of the Insti- tute of Navigation, 1988,35 (4) :483-501.
  • 9Brown R G.A Baseline GPS RAIM Scheme and a Note on the Equivalence of Three RAIM Methods [ J ]. Navigation: Jour- nal of the Institute of Navigation, 1992,39(3): 301-316.
  • 10Safety Regulation Group. GPS Integrity and Potential Impact on Aviation Safety[ R ]. CAA THESIS, 2003,9.

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