北京航空航天大学学报 ›› 2018, Vol. 44 ›› Issue (4): 684-690.doi: 10.13700/j.bh.1001-5965.2017.0277

• 论文 • 上一篇    下一篇

BDS/GPS组合导航接收机自主完好性监测算法

王尔申1, 杨福霞1, 庞涛1, 曲萍萍1, 蓝晓宇1, 姜毅2   

  1. 1. 沈阳航空航天大学电子信息工程学院, 沈阳 110136;
    2. 大连海事大学信息科学技术学院, 大连 116026
  • 收稿日期:2017-05-03 出版日期:2018-04-20 发布日期:2018-04-27
  • 通讯作者: 王尔申 E-mail:wes2016@126.com
  • 作者简介:王尔申,男,博士,教授。主要研究方向:卫星导航、卫星导航信号性能评估。
  • 基金资助:
    国家自然科学基金(61571309,61101161);中央高校基本科研业务费专项资金(3132016317);辽宁省“百千万人才工程”;辽宁省高等学校优秀人才支持计划(LR2016069);辽宁省教育厅科学技术研究项目(L201716);航空科学基金(2015ZC54010)

BDS/GPS combined navigation receiver autonomous integrity monitoring algorithm

WANG Ershen1, YANG Fuxia1, PANG Tao1, QU Pingping1, LAN Xiaoyu1, JIANG Yi2   

  1. 1. School of Electronic and Information Engineering, Shenyang Aerospace University, Shenyang 110136, China;
    2. Information Science and Technology College, Dalian Maritime University, Dalian 116026, China
  • Received:2017-05-03 Online:2018-04-20 Published:2018-04-27
  • Supported by:
    National Natural Science Foundation of China (61571309,61101161); the Fundamental Research Funds for the Central Universities (3132016317); Liaoning BaiQianWan Talents Program; Program for Liaoning Excellent Talents in University (LR2016069); Scientific Study Project for Liaoning Province Ministry of Education (L201716); Aeronautical Science Foundation of China (2015 ZC54010)

摘要: 为使接收机自主完好性监测(RAIM)技术应用于民航垂直引导进近(APV)飞行阶段成为可能,研究了BDS/GPS组合导航RAIM算法。提出了一种基于BDS/GPS定位解最优加权平均解的算法,结合最优加权平均解与BDS/GPS定位解的关系建立检验统计量,根据最大允许的虚警率计算检验门限,实现对故障所在卫星导航系统的检测,并采用加权最小二乘残差法对故障进行检测与识别。研究结果对多星座组合卫星导航系统应用于民航APV飞行阶段的导航具有一定的参考意义。

关键词: 接收机自主完好性监测(RAIM), 北斗卫星导航系统(BDS), 组合导航, 垂直引导进近(APV), 加权平均

Abstract: In order to make receiver autonomous integrity monitoring (RAIM) technique be applied to approach with vertical guidance (APV) flight phase in civil aviation navigation, the BDS/GPS combined navigation RAIM algorithm is studied. An algorithm based on the optimal weighted average solution of BDS/GPS position solution is proposed. Combined with the relationship between the optimal weighted average solution and BDS/GPS position solution, a test statistic is established. The test threshold is obtained according to the maximum allowable false alarm probability, and then the satellite navigation system fault is detected. Through the weighted least squares residual method, the satellite fault is detected and identified. The results are instructive for the study of multi-constellation combined satellite navigation system applied to the navigation in civil aviation APV flight phase.

Key words: receiver autonomous integrity monitoring(RAIM), BeiDou navigation satellite system(BDS), combined navigation, approach with vertical guidance (APV), weighted average

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