赵昂, 杨元喜, 许扬胤, 景一帆, 杨宇飞, 马越原, 徐君毅. GNSS单系统及多系统组合完好性分析[J]. 武汉大学学报 ( 信息科学版), 2020, 45(1): 72-80. DOI: 10.13203/j.whugis20180425
引用本文: 赵昂, 杨元喜, 许扬胤, 景一帆, 杨宇飞, 马越原, 徐君毅. GNSS单系统及多系统组合完好性分析[J]. 武汉大学学报 ( 信息科学版), 2020, 45(1): 72-80. DOI: 10.13203/j.whugis20180425
ZHAO Ang, YANG Yuanxi, XU Yangyin, JING Yifan, YANG Yufei, MA Yueyuan, XU Junyi. Integrity Analysis of GNSS Single System and Multi-system Combination[J]. Geomatics and Information Science of Wuhan University, 2020, 45(1): 72-80. DOI: 10.13203/j.whugis20180425
Citation: ZHAO Ang, YANG Yuanxi, XU Yangyin, JING Yifan, YANG Yufei, MA Yueyuan, XU Junyi. Integrity Analysis of GNSS Single System and Multi-system Combination[J]. Geomatics and Information Science of Wuhan University, 2020, 45(1): 72-80. DOI: 10.13203/j.whugis20180425

GNSS单系统及多系统组合完好性分析

Integrity Analysis of GNSS Single System and Multi-system Combination

  • 摘要: 全球导航卫星系统(global navigation satellite system,GNSS)的发展和完善为多星座融合定位、导航和授时提供了重要基础,也为接收机自主完好性监测提供了更有利的外部条件。首先通过星座仿真,分别计算了单频和双频条件下GNSS单系统及组合系统的保护水平;然后分析了全球范围内GNSS不同频率及不同组合方式条件下的保护水平的基本分布情况;最后探讨了在不同频率和组合方式条件下接收机自主完好性监测(receiver autonomous integrity monitoring,RAIM)在不同进近阶段的可用性。计算结果表明,单系统单频或双频组合均不能满足垂直制导航性能(localizer performance with vertical guidance 200ft,LPV-200)进近阶段的要求;双系统双频组合可满足LPV-200进近阶段的要求;三系统双频组合可满足具有垂直引导(approach with vertical guidance II,APV-II)的进近阶段的要求,但无法满足精密进近要求;四系统组合相比于三系统组合改善效果不明显。

     

    Abstract: The development and improvement of the global navigation satellite system (GNSS) provides an important basis for multi-constellation's fusion positioning, navigation, and timing, and it also provides more favorable external conditions for the receiver's autonomous integrity monitoring. Firstly, the protection level of GNSS single system and multi-system combination under single-frequency and dual-frequency conditions were calculated respectively through the constellation simulation. Then, This paper analyzed the basic distribution of protection levels under different frequencies and different combinations of GNSS worldwide. Finally, the availability of receiver autonomous integrity monitoring (RAIM) in different aviation approaching phases under different frequencies and combinations was discussed. The calculation results show that the single system under single-frequency or dual-frequency combination cannot meet the requirements of the approach phase of localizer performance with vertical guidance 200ft (LPV-200).Nevertheless, double-system under dual-frequency can meet the requirement.The triple-system under dual-frequency combination can meet the requirements of approach with vertical guidance II (APV-II), but cannot meet the requirements of precision approaching. But the improvement of four-system combination is not obvious compared with that of triple-system combination.

     

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