基于模拟信号源的机载BDS接收机性能测试
|
摘要
针对机载北斗卫星导航系统(BDS)接收机无法进行实际测试的问题,基于对机载BDS接收机的首次定位时间(TTFF)、重捕时间和定位精度的分析与仿真,研究某一指标与相关参数的关系,提出利用全球导航卫星系统(GNSS)模拟信号源测试机载BDS接收机性能指标的测试方法。该方法结合真实飞行数据,利用GNSS模拟信号源模拟飞机运动过程,从而对飞行过程中机载BDS接收机的关键指标进行测试。测试结果表明:机载BDS接收机的首次定位时间满足RTCA DO-208对TTFF不大于5 min的要求;重捕时间基本满足TSO-C146d对重捕时间不大于20 s的要求;静态误差满足北斗公开服务性能规范对其不大于10 m的要求,动态误差基本满足RTCA DO-208对其小于230 m的要求,且测试结果均符合理论分析。
For the problem that the airborne Beidou Satellite Navigation System(BDS) receiver cannot be tested actually, based on the analysis and simulation of the Time to First Fix(TTFF), reacquisition time, and positioning accuracy of the airborne BDS receiver, the relationship between a certain index and related parameters is studied. A test method for testing the performance index of airborne BDS receiver using Global Navigation Satellite System(GNSS) analog signal generator is proposed. This method combines real flight data and uses GNSS analog signal generator to simulate the motion process of the aircraft, thereby testing the key indicators of the airborne BDS receiver during the flight. The test results show that the Time to First Fix of the airborne BDS receiver meets the requirements of RTCA DO-208 to TTFF not greater than 5 minutes; the reacquisition time basically meets the requirement that TSO-C146 d has a reacquisition time of less than 20 seconds; the static error meets the requirements of Beidou Service performance specifications for its requirements of not more than 10 m, the dynamic error basically meets RTCA DO-208 requirements of less than 230 m, and the above test results are in line with theoretical analysis.
For the problem that the airborne Beidou Satellite Navigation System(BDS) receiver cannot be tested actually, based on the analysis and simulation of the Time to First Fix(TTFF), reacquisition time, and positioning accuracy of the airborne BDS receiver, the relationship between a certain index and related parameters is studied. A test method for testing the performance index of airborne BDS receiver using Global Navigation Satellite System(GNSS) analog signal generator is proposed. This method combines real flight data and uses GNSS analog signal generator to simulate the motion process of the aircraft, thereby testing the key indicators of the airborne BDS receiver during the flight. The test results show that the Time to First Fix of the airborne BDS receiver meets the requirements of RTCA DO-208 to TTFF not greater than 5 minutes; the reacquisition time basically meets the requirement that TSO-C146 d has a reacquisition time of less than 20 seconds; the static error meets the requirements of Beidou Service performance specifications for its requirements of not more than 10 m, the dynamic error basically meets RTCA DO-208 requirements of less than 230 m, and the above test results are in line with theoretical analysis.
引文
[1]贾超广,王俊亚,董小环.基于卫星信号模拟器的北斗接收机测试方法[C]//中国卫星导航学术年会.2013.
[2]施荣华,叶睿,董健,等.一种导航接收机启动策略的优化方案[J].计算技术与自动化,2013,32(2):86-90.
[3]MS BRAASCH,AJV DIERENDONCK.GPS receiver architectures and measurements[C]//Proceedings of the IEEE,2002,87(1):48-64.
[4]RTCA.DO-208,Minimum operational performance standards for airborne supplemental navigation equipment using global positioning system(GPS)[S].1991.
[5]FRUEHAUF H.Issues involved with GPS signal acquisition and unlocks[DB/OL].FEI-Zyfer Inc,2005.
[6]FlightAware实时航班跟踪[DB/OL].[2017-04-14].https://zh.flightaware.com/live/.
[7]张明,顾晓雪.北斗接收机定位误差分析[J].电子与封装,2015(9):40-43.
[8]FAA.TSO-C146d,Stand-alone airborne navigation equipment using The global positioning system augmented by the satellite based augmentation system(SBAS)[S].2013.
[9]伍蔡伦,陆明泉,冯振明.高动态GNSS接收机载波环性能评估与仿真[J].现代雷达,2011,33(7):64-67.
[10]吴琼,寇艳红,郑兴平.高动态GPS接收机环路跟踪技术研究[J].测控遥感与导航定位,2008,38(12):32-36.
[11]RTCA.DO-229C,Minimum operational performance standards for global positioning system/wide area augmentation system airborne equipment[S].2001.
[12]中国卫星导航系统管理办公室.北斗公开服务性能规范[S].2013.
[2]施荣华,叶睿,董健,等.一种导航接收机启动策略的优化方案[J].计算技术与自动化,2013,32(2):86-90.
[3]MS BRAASCH,AJV DIERENDONCK.GPS receiver architectures and measurements[C]//Proceedings of the IEEE,2002,87(1):48-64.
[4]RTCA.DO-208,Minimum operational performance standards for airborne supplemental navigation equipment using global positioning system(GPS)[S].1991.
[5]FRUEHAUF H.Issues involved with GPS signal acquisition and unlocks[DB/OL].FEI-Zyfer Inc,2005.
[6]FlightAware实时航班跟踪[DB/OL].[2017-04-14].https://zh.flightaware.com/live/.
[7]张明,顾晓雪.北斗接收机定位误差分析[J].电子与封装,2015(9):40-43.
[8]FAA.TSO-C146d,Stand-alone airborne navigation equipment using The global positioning system augmented by the satellite based augmentation system(SBAS)[S].2013.
[9]伍蔡伦,陆明泉,冯振明.高动态GNSS接收机载波环性能评估与仿真[J].现代雷达,2011,33(7):64-67.
[10]吴琼,寇艳红,郑兴平.高动态GPS接收机环路跟踪技术研究[J].测控遥感与导航定位,2008,38(12):32-36.
[11]RTCA.DO-229C,Minimum operational performance standards for global positioning system/wide area augmentation system airborne equipment[S].2001.
[12]中国卫星导航系统管理办公室.北斗公开服务性能规范[S].2013.