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BDS/GPS组合导航接收机自主完好性监测算法
引用本文:王尔申,杨福霞,庞涛,曲萍萍,蓝晓宇,姜毅.BDS/GPS组合导航接收机自主完好性监测算法[J].北京航空航天大学学报,2018,44(4):684-690.
作者姓名:王尔申  杨福霞  庞涛  曲萍萍  蓝晓宇  姜毅
作者单位:沈阳航空航天大学 电子信息工程学院,沈阳,110136;大连海事大学 信息科学技术学院,大连,116026
基金项目: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) 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(2015ZC54010)
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
收稿时间:2017-05-03

BDS/GPS combined navigation receiver autonomous integrity monitoring algorithm
WANG Ershen,YANG Fuxia,PANG Tao,QU Pingping,LAN Xiaoyu,JIANG Yi.BDS/GPS combined navigation receiver autonomous integrity monitoring algorithm[J].Journal of Beijing University of Aeronautics and Astronautics,2018,44(4):684-690.
Authors:WANG Ershen  YANG Fuxia  PANG Tao  QU Pingping  LAN Xiaoyu  JIANG Yi
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 navi-gation 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 in-structive for the study of multi-constellation combined satellite navigation system applied to the navigation in civil aviation APV flight phase.
Keywords:receiver autonomous integrity monitoring(RAIM)  BeiDou navigation satellite system(BDS)  combined navigation  approach with vertical guidance (APV)  weighted average
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