Please wait a minute...
 首页  期刊介绍 期刊订阅 联系我们 横山亮次奖 百年刊庆
 
最新录用  |  预出版  |  当期目录  |  过刊浏览  |  阅读排行  |  下载排行  |  引用排行  |  横山亮次奖  |  百年刊庆
清华大学学报(自然科学版)  2014, Vol. 54 Issue (4): 425-431    
  本期目录 | 过刊浏览 | 高级检索 |
基于伪距误差重建的多星故障检测方法
张鑫,崔晓伟(),冯振明
Multiple failure detection based on reconstruction of the pseudorange error
Xin ZHANG,Xiaowei CUI(),Zhenming FENG
Department of Electronic Engineering, Tsinghua University, Beijing 100084, China
全文: PDF(1100 KB)   HTML
输出: BibTeX | EndNote (RIS)      
摘要 

传统的接收机自主完好性监测(RAIM)方法使用定位解算方程的残差来进行故障识别,在单卫星故障下具有较好的性能。随着全球卫星导航系统的建设,用户观测到的卫星数目显著增加,使用多颗卫星定位可以提高定位精度。但多颗卫星同时发生故障的概率将会增大, RAIM方法需要进行改进以应对多星故障。该文首先对RAIM方法的原理进行了深入分析,推导出了误差向量和残差向量之间的投影关系。然后,通过实例论证了误差向量和残差向量在投影变换时会带来信息损失,从而使故障难以检测。最终,给出了一种新的RAIM方法。通过引入约束条件,利用残差向量重构出误差向量。根据误差向量大小,实现多星故障检测。仿真表明该方法在多星故障模式下,具有较好的检测性能。

服务
把本文推荐给朋友
加入引用管理器
E-mail Alert
RSS
作者相关文章
关键词 卫星导航系统接收机自主完好性监测投影矩阵残差误差重构    
Abstract

The traditional RAIM algorithm uses the residuals of the positioning equation for failure detection and gives better detection when only one fault exists. The global navigation satellite system gives users many more ranging sources with better positioning thanks to the increased number of visible satellites. However, the probability of simultaneous failures also increase which requires improves to the traditional RAIM algorithm to address multiple failures. The RAIM design was analyzed to deduce a relationship between the residuals and the error vector. Examples then show that some information is lost when projecting from the error vector to the residuals, which limits failure detection. A modified RAIM algorithm with additional constraints that enable the error vector to be recovered from the residuals so that multiple failures can be detected monitoring the error vector. Simulations show the ability of this method for multiple failures.

Key wordssatellite navigation system    receiver autonomous integrity monitoring (RAIM)    projection matrix    residual    error reconstruction
收稿日期: 2013-09-09      出版日期: 2014-04-15
基金资助:中科院青年基金项目(2012PNTT12)
引用本文:   
张鑫,崔晓伟,冯振明. 基于伪距误差重建的多星故障检测方法[J]. 清华大学学报(自然科学版), 2014, 54(4): 425-431.
Xin ZHANG,Xiaowei CUI,Zhenming FENG. Multiple failure detection based on reconstruction of the pseudorange error. Journal of Tsinghua University(Science and Technology), 2014, 54(4): 425-431.
链接本文:  
http://jst.tsinghuajournals.com/CN/  或          http://jst.tsinghuajournals.com/CN/Y2014/V54/I4/425
特征值 特征向量
0 [-0.633, -0.056, -0.014, -0.360, -0.568, 0.370, -0.083]T
[0.384, -0.115, -0.476, -0.412, 0.220, 0.600, 0.188]T
[0, 0.021, 0.444, 0.495, 0.160, 0.701, -0.202]T
[0, 0.601,0.287, -0.080, -0.069, 0.083, 0.734]T
1 [0.251, 0.736, -0.198, -0.060, -0.207, 0.032, -0.555]T
[-0.624, 0.283, -0.358, 0.088, 0.628, 0.007, -0.023]T
[0, 0.016, 0.571, -0.662, 0.401, -0.063, -0.264]T
  投影矩阵的特征值与特征向量
误差模式 定位结果误差 残差向量 检验统计量
E1 [-7.9, -8.6, 0.2] [0.25, 18.67, -7.12, -0.90, 0.94, 0.74, -12.59] 560.1
E2 [-2.2, 32.3, 8.3] [0.12, 0.74, -1.33, 1.20, -0.83, 0.15, -0.05] 4.5
E3 [-13.0, -2.1, 21.7] [-3.75, -12.59, -0.98, 6.18, -0.17, -0.05, 11.36] 340.7
  不同误差模式下的解算结果
分组号 进行约束
的卫星编号
可进行故障识
别的卫星编号
1 3、 4、 5、 6 1、 2
2 1、 2、 5、 6 3、 4
3 1、 2、 3、 4 5、 6
  6颗可见星时的约束分组
分组号 进行约束
的卫星编号
可进行故障识
别的卫星编号
1 4、 5、 6、 7 1、 2、 3
2 2、 3、 6、 7 1、 4、 5
3 2、 3、 4、 5 1、 6、 7
4 1、 3、 5、 7 2、 4、 6
5 1、 3、 4、 6 2、 5、 7
6 1、 2、 5、 6 3、 4、 7
7 1、 2、 4、 7 3、 5、 6
  7颗可见星时的约束分组
可见卫星数 单星故障
分组数
双星故障
分组数
三星故障
分组数
6 3 - -
7 3 7 -
8 2 6 14
9 2 5 12
10 2 5 10
11 2 4 9
12 2 3 8
  几种典型情况的约束分组数目统计
伪距误差向量 Q值
E1 1 [0, 30.0, 0, 0, 0, 0, 0] 0.00
2 [894.0, 0, 0, 503.0, 831.4, 0, 0] 944 322 ×
3 [-10.7, 0, 0, 0, 0, 145.0, -36.1] 1 420 ×
E2 1 [1.5, -0.1, -3.3, 0, 0, 0, 0] 2.3 ×
2 [40.1, 0, 0, 25.0, 36.6, 0, 0] 1 968 ×
3 [0, 0, 0, 0, 0, 30.0, 0] 0.00
E3 1 [-2.8, 25.2, -13.1, 0, 0, 0, 0] 180.5 ×
2 [-590.2, 0, 0, -317.1, -543.1, 0, 0] 395 546 ×
3 [0, 0, 0, 0, 0, 0, 30.0] 0.00
  重构伪距误差法计算示意
  伪距误差重构结果
[1] Lee Y C, Dyke K, DeCleene B, et al. Summary of RTCA SC-159 GPS integrity working group activities [J].Journal of the Institute of Navigation, 1996, 43(3): 307-362.
[2] Parkinson B W. Global positioning system: theory and applications[M]. Washington DC, USA: American Institute of Aeronautics and Astronautics, 1996.
[3] Walter T, Enge P, Blanch J, et al.Worldwide vertical guidance of aircraft based on modernized GPS and new integrity augmentations[J]. Proceedings of the IEEE, 2008, 96(12): 1918-1935.
[4] Hwang P, Brown R G. From RAIM to NIORAIM: A new integrity approach to integrated multi-GNSS systems[J]. Inside GNSS, 2008, 3(4): 24-33.
[5] Blanch J, Walter T, Enge P. RAIM with optimal integrity and continuity allocations under multiple failures[J]. Aerospace and Electronic Systems, IEEE Transactions, 2010, 46(3): 1235-1247.
[6] Milner C D, Ochieng W Y. A Fast and efficient integrity computation for non-precision approach performance assessment[J]. GPS Solutions, 2010, 14(2): 193-205.
[7] Lee Y C. A position domain relative RAIM method[J]. Aerospace and Electronic Systems, IEEE Transactions, 2011, 47(1): 85-97.
[8] Martini I, Hein G W. An integrity monitoring technique for multiple failures detection[J]. Position, Location, And Navigation Symposium, IEEE/ION, 2006: 450-467.
[9] Schroth, Georg, Rippl, et al. Enhancements of the range consensus algorithm (RANCO) [C]// Proceedings of the 21st International Technical Meeting of the Satellite Division of the Institute of Navigation. Georgia, USA: Institute of Navigation, 2008: 93-103.
[10] Macabiau, Christophe, Gerfault, et al. RAIM performance in presence of multiple range failures [C]// Proceedings of the 2005 National Technical Meeting of the Institute of Navigation. San Diego, USA: Institute of Navigation, 2005: 779-791.
[11] Ober P B. Integrity prediction and monitoring of navigation systems: architectures and algorithms[M]. Leiden, Netherlands: Integricom, 2003.
[12] 郭婧, 崔晓伟, 陆明泉, 等. 支持垂直引导进近的多星座RAIM算法[J]. 清华大学学报: 自然科学版, 2011, 51(2): 154-160. GUO Jing, CUI Xiaowei, LU Mingquan, et al.Multi-constellation RAIM for approach with vertical guidance[J]. Journal of Tsinghua University: Science and Technology, 2011, 51(2): 154-160. (in Chinese)
[13] Brown R G. Solution of thetwo-failure GPS RAIM problem under worst-case bias conditions[J]. NAVIGATION, Journal of the Institute of Navigation, 1997, 44(4): 425-432.
No related articles found!
Viewed
Full text


Abstract

Cited

  Shared   
  Discussed   
版权所有 © 《清华大学学报(自然科学版)》编辑部
本系统由北京玛格泰克科技发展有限公司设计开发 技术支持:support@magtech.com.cn