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一种地基增强系统(GBAS)B值的分析与处理技术 被引量:5

Analysis and Processing of B-Values for GNSS GBAS
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摘要 地基增强系统中采用B值是多个接收机输出观测量偏差,是地面站系统进行完好性监测的重要参数之一,为系统进行基于接收机故障的完好性风险评估提供基础判断依据。在单系统的卫星导航着陆系统中,B值的处理采用了伪距修正残差的基本思想,但对于多系统卫星导航系统情况下,接收机的故障需要进行独立分析和综合判断,判断的门限也存在区别,因此,本文基于地基增强系统中B值的计算方法,针对GPS系统进行B值的计算分析,提出了一种适用于多系统的B值计算方法,为多系统地基增强系统的完好性监测处理方法进行了研究和分析。 B-values are the difference ofpseudorange corrections for multiple reference receivers on GBAS (Ground Based Augmentation System). It is one of important parameters for the ground system integrity monitoring, which is used as a basic reference for the integrity risk estimation based on reference receivers' failure. For single satellite navigation system, the residual of pseudorange corrections is adopted in the B-value processing. However, an independent analysis and integrated processing are necessary for detecting the failure of multiple reference receivers. Therefore, a new B-value algorithm available for multiple systems is put forward based on the traditional B-value processing method and the analysis of GPS data. The algorithm can be used for integrity monitoring for future GNSS GBAS system.
出处 《现代导航》 2013年第1期19-23,共5页 Modern Navigation
基金 国家科技支撑计划课题-GNSS地基增强系统 课题编号:2011BAH24B03
关键词 B值 完好性 伪距修正残差 B-values Integrity Pseudorange Correction Residual
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参考文献6

  • 1Elliott D. Kaplan;Christopher J. Hegarty;寇艳红.GPS原理与应用(第二版)[M]{H}北京:电子工业出版社,20077.
  • 2Jiyun Lee. GPS-Based Aircraft Landing Systems with Enhanced Performance:Beyond Accuracy[D].Standford University,2005,(3):25-80.
  • 3Gang Xie. Optimal on-airport monitoring of the integrity of GPS-Based landing systems[D].Standford University,2004,(3):20-80.
  • 4杨文辉,周保军.LAAS地面系统中多基准一致性检测算法的分析[J].电子学报,2006,34(3):469-471. 被引量:15
  • 5朱衍波,张晓林,薛瑞,张淼艳.民航GPS地基区域完好性监视系统设计与实现[J].北京航空航天大学学报,2006,32(7):797-801. 被引量:8
  • 6Per-Ludvig Normark,Gang Xie,Dennis Akos,San Pullen. The Next Generation Integrity Monitor Testbed (IMT) for Ground System Development and Validation Testing[A].Salt Lake City,UT,.

二级参考文献11

  • 1RTCA DO-208,Minimum Operational Performance Standards for Airborne Supplemental Navigation Equipment Using Global Positioning System (GPS)[S]
  • 2FAA TSO-C129a,Airborne Supplemental Navigation Equipment Using the Global Positioning System (GPS)[S]
  • 3FAA E-2892b,Specification for the Wide Area Augmentation System (WAAS)[S]
  • 4RTCA DO-246B,GNSS-Based Precision Approach Local Area Augmentation System (LAAS) Signal-in-space Interface Control Document (ICD)[S]
  • 5Young C Lee.Receiver autonomous integrity monitoring (RAIM) capability for sole-means GPS navigation in the oceanic phase of flight[J].IEEE Aerospace and Electronic Systems Magazine,1992,7(5):29-36
  • 6Pieter Bastiaan Ober.Integrity prediction and monitoring of navigation systems[M].Leiden:Integricom Publishers,2003
  • 7RONALD BRAFF,et al.Description of the FAA's Local Area Augmentation System (LAAS)[J].NAVIGATION:Journal of The Institute of Navigation,1997,44 (4):411 -423.
  • 8U.S.Federal Aviation Administration.Specification:Performance Type One Local Area Augmentation System Ground Facility[DB/OL].http://gps.faa.gov/Library/Documents/laas_ faa2937.pdf,1999-09-21.
  • 9Dr Robert et al.Comparison of LAAS B-Values to the Linear Model Optimum B-values[A].ION 55th Annual Meeting[C].Cambridge,MA:The Institute of Navigation,1999-06-28.191-198.
  • 10Gang Xie,et al.Integrity design and updated test results for the stanford LAAS integrity monitor testbed[A].ION 57th Annual Meeting/CIGTF 20th Biennial Guidance Test Symposium[C].Albuquerque,NM:The Institute of Navigation,2001-06-11.681 -693.

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