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一种新的接收机自主完好性监测算法研究

Research on a New Algorithm of Receiver Autonomous Integrity Monitoring
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摘要 基于奇偶空间的"快照"RAIM算法利用冗余GPS卫星,可以一步检测系统的较大偏差故障,但对中等的累积型故障不具备检测能力。利用多元累积和检测冗余方程的奇偶残差向量,得到了一种新的RAIM算法——多元累积RAIM(Multivariate Cumulative RAIM,MC-RAIM),并将平均运行长度(Average Run Length,ARL)作为该算法性能判决的指标,根据Markov链的状态转移矩阵计算不同维数、窗口参数和报警门限下的ARL,通过仿真实验证明该算法对于GPS系统的中等累积型故障具有检测能力,弥补了原有RAIM算法的缺陷。 The algorithm of “snapshot” receiver autonomous integrity monitoring ( RAIM ) based on parity space can detect the deviation fault of system within one step,but can’t detect the cumulative fault by using redundant GPS satellite.The multivariate cumu-lative RAIM ( MC-RAIM) is deduced by using multivariate cumulative sum to check the parity residual error of GPS redundant equa-tion.The average run length (ARL),used as the performance index of this algorithm,is computed by Markov state transfer matrix under the different condition of window coefficient and alarm threshold.The simulation experiment proves that this algorithm can detect medium cumulative fault and made use of redundant GPS to compute parity residual error,which could detect system fault within one step,but lost the capability for cumulative fault.the multivariate cumulative RAIM (MC-RAIM) Arithmetic was deduced,which using,and using average run length(ARL) as the performance index,which was computed by the.Finally,it was proved that this new Arithmetic could detect medium cumulative fault by the way of simulation and cover the shortage of “snapshot” RAIM.
出处 《无线电工程》 2014年第4期28-31,共4页 Radio Engineering
基金 国家科技支撑计划("863"计划)资助项目(2011BAH05B00) (2011BAH05B02)
关键词 马尔科夫链 平均运行长度 “快照” RAIM 多元累积RAIM “snapshot” RAIM MCRAIM Markov chain average run length
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参考文献10

  • 1PARKINSON B W, AXELRAD P.Autonomous GPS Integ- rity Monitoring Using Maximum Solution Separation [ J ]. Navigation : Journal of the Institute of Navigation, 1988,35 (2) :25-35.
  • 2GROVER B R, MCBURNEY P W. Self-eontained GPS Integrity Check Using Maximum Solution Separation [ J ]. Navigation : Journal of the Institute of Navigation, 1988,35 (1) :41-53.
  • 3STURZA M A. Navigation System Integrity Monitoring Using Redundant Measurement [ J ] .Navigation : Journal of the Institute of Navigation, 1988,35(4) :483-501.
  • 4LEE Y.Analysis of Range and Position Comparision Meth- ods as a Means to Provide GPS Integrity in the User Re- ceiver[ C ] //Proceedings of ION 42th Annual Meeting, 1986: 1-4.
  • 5BROWN R G.A Baseline GPS RAIM Scheme and a Note on the Equivalence of Three RAIM Methods [ J ]. Naviga- tion : Journal of the Institute of Navigation, 1992,39 ( 3 ) : 301-316.
  • 6JAMALI A S,LI J L,CHANDIO A F.Average Run Length Performance of Shewhart Control Chart with Interpretation Rules Using Markov Chain Approach [ C ] //2007 IEEE International Conference on Control and Automation, 2007:2 055-2 059.
  • 7王彩霞.GPS RAIM预测系统的设计和算法研究[J].现代导航,2012,3(3):165-170. 被引量:3
  • 8李亮.陆基增强系统定位与完好性监测技术研究[D].哈尔滨:哈尔滨工程大学,2013(1):10-40.
  • 9郭婧,陆明泉,崔晓伟,冯振明.三频GNSS接收机的RAIM算法研究[J].宇航学报,2011,32(8):1734-1739. 被引量:8
  • 10王尔申,张淑芳,胡青.GNSS接收机自主完好性监测算法研究[J].通信技术,2010,43(1):213-214. 被引量:6

二级参考文献24

  • 1朱衍波,张淼艳,张军.加权RAIM可用性预测方法研究[J].遥测遥控,2009,30(1):1-6. 被引量:10
  • 2陈南,高扬,陈建鹏.从GPS SS/US接口规定文件看导航电文设计的新发展[J].导航,2006,42(4):9-12. 被引量:2
  • 3Brown R G. GPS RAIM:Calculation of Thresholds and Protection Radius Using Chi-Square Methods-h Geometric Approach[J]. Navigation ION Red BookSeries, 1998(05):155-178.
  • 4Misra P, Pratt M, Muchnik R, et al. A General PAlM Algorithm Based on Receiver Clock[C].VA:the Institute of Navigation,1995:1941-1947.
  • 5Young C LEE. RAIM Availability for GPS Augmented with Barometric Altimeter Aiding and Clock Coasting[J].rhe Institute of Navigation, 1993,40(02):179-198.
  • 6Vieweg S. Integrity Monitoring and Failure Identification Within An Integrated Satellite/inertial Navigation System[C]. USA:[s.n.],1994:755-761.
  • 7Ronald Braff. Integrated Gnss/Altimeter Landing System[C]. USA:[s.n.],2007:2934-2949.
  • 8Junjie N I, Yongxin ZHU, Wei GUO. An Improved RAIM Scheme for Processing Multiple Outliers in GNSS[C].USA:IEEE Computer Society, 2007:840-845.
  • 9Ober P B, Harriman D. On the Use of Multiconstellation-RAIM for Aircraft Approaches[C].TX:the Institute of Navigation, 2006:2587-2596.
  • 10Hewitson S, Wang J L. GNSS Receiver Autonomous Integrity Monitoring(RAIM) Performance Analysis[J]. GPS Solut, 2006, 9 (10) : 155-170.

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