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基于多通道SQM指标联合的矢量接收机多径干扰检测方法

贾琼琼 朱传胜

贾琼琼, 朱传胜. 基于多通道SQM指标联合的矢量接收机多径干扰检测方法[J]. 全球定位系统, 2023, 48(3): 110-119. doi: 10.12265/j.gnss.2023037
引用本文: 贾琼琼, 朱传胜. 基于多通道SQM指标联合的矢量接收机多径干扰检测方法[J]. 全球定位系统, 2023, 48(3): 110-119. doi: 10.12265/j.gnss.2023037
JIA Qiongqiong, ZHU Chuansheng. Multipath interference detection method for vector receivers based on joint multi-channel SQM metrics[J]. GNSS World of China, 2023, 48(3): 110-119. doi: 10.12265/j.gnss.2023037
Citation: JIA Qiongqiong, ZHU Chuansheng. Multipath interference detection method for vector receivers based on joint multi-channel SQM metrics[J]. GNSS World of China, 2023, 48(3): 110-119. doi: 10.12265/j.gnss.2023037

基于多通道SQM指标联合的矢量接收机多径干扰检测方法

doi: 10.12265/j.gnss.2023037
基金项目: 中国民航大学民航航班广域监视与安全管控技术重点实验室开放基金(202202)
详细信息
    作者简介:

    贾琼琼:(1986—),女,硕士,副教授,研究方向为信号处理在卫星导航中的应用研究

    朱传胜:(1997—),男,硕士,研究方向为卫星导航与多径干扰监测

    通讯作者:

    贾琼琼 E-mail: qqjia@cauc.edu.cn

  • 中图分类号: P228.4

Multipath interference detection method for vector receivers based on joint multi-channel SQM metrics

  • 摘要: 矢量接收机利用各跟踪通道间信息共享达到通道间相互辅助的作用,因此相对于传统的标量接收机能在复杂环境下提供更好的性能. 然而在城市峡谷等复杂环境下,多径传输会严重限制矢量接收机的性能,若能及时发现多径并加以处理则能消除多径干扰的影响. 本文从多径对矢量接收机的影响机理出发,研究基于信号质量监测(SQM)的多径检测问题. 在分析现有的针对标量接收机信号SQM指标的基础上,结合矢量接收机通道耦合的特点,提出一种联合多通道SQM指标的矢量接收机多径检测方法. 最后,通过仿真实验验证了所提方法能够有效地检测与直达信号幅度比小于0.5、相对码延时在0.3~0.6码片的多径干扰.

     

  • 图  1  多径干扰下的自相关函数

    图  2  标量接收机跟踪结构

    图  3  矢量接收机跟踪结构

    图  4  多径干扰下矢量跟踪中不同跟踪通道信号相关函数

    图  5  多径干扰下Ratio和Delta指标变化

    图  6  多径干扰下Double Delta、ELP、Slope和文献[16]提出的指标变化

    图  7  Ratio指标和Delta指标取绝对值后的直方图以及理论概率密度函数曲线

    图  8  本文方法流程图

    图  9  SQM指标检测率随时间变化趋势

    图  10  SQM指标检测率随虚警率变化趋势

    图  11  SQM指标检测率随多径码延时变化趋势

    图  12  SQM指标检测率随多径相对幅度变化趋势

    图  13  多通道联合指标检测率随时间变化趋势

    图  14  多通道联合指标检测率随虚警率变化趋势

    图  15  多通道联合指标检测率随码延时变化趋势

    图  16  多通道联合指标检测率随多径相对幅度变化趋势

    图  17  二次检测后多通道联合指标检测率随虚警率变化趋势

    表  1  常用的SQM指标

    接收机类型指标名称指标计算表达式均值
    标量跟踪Delta[3]$\displaystyle\frac{ { {I_{\rm{E}}} - {I_{\rm{L}}} } }{ { {I_{\rm{P}}} } }$0
    Ratio[3]$\displaystyle\frac{ { {I_{\rm{E}}} + {I_{\rm{L}}} } }{ { {I_{\rm{P}}} } }$1.9
    Double Delta[6]$\displaystyle\frac{ {({I_{ {{\rm{E}}_1} } } - {I_{ {{\rm{L}}_1} } }) - ({I_{ {{\rm{E}}_2} } } - {I_{ {{\rm{L}}_2} } })} }{ { {I_{\rm{P}}} } }$0
    ELP[8]${\arctan }\left( {\displaystyle\frac{ { {Q_{\rm{E} } } } }{ { {I_{\rm{E} } } } } } \right) - {\arctan }\left( {\displaystyle\frac{ { {Q_{\rm{L} } } } }{ { {I_{\rm{L} } } } } } \right)$0
    Slope[15]$\displaystyle\frac{ {2 \cdot ({I_{ {{\rm{L}}_1} } } - {I_{ {{\rm{L}}_2} } })} }{ { {I_{\rm{P}}}({d_1} - {d_2})} }$−1
    矢量跟踪文献[16]$\left\{ \begin{gathered} \frac{ { {I_{\rm{P}}} - {I_{\rm{L}}} } }{ { {I_{\rm{E}}} + {I_{\rm{L}}} } }{\text{ } }\left| { {I_{\rm{E}}} } \right| \geqslant \left| { {I_{\rm{L}}} } \right| \\ \frac{ { {I_{\rm{P}}} - {I_{\rm{E}}} } }{ { {I_{\rm{E}}} + {I_{\rm{L}}} } }{\text{ } }\left| { {I_{\rm{E}}} } \right| < \left| { {I_{\rm{L}}} } \right| \\ \end{gathered} \right.$0.5
    下载: 导出CSV

    表  2  仿真实验参数设置

    相关参数取值
    接收机中频/MHz1.405
    接收机采样率/MHz5.714
    数据长度/s30
    多径干扰时间/s10~20
    受干扰卫星号2
    下载: 导出CSV
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  • 收稿日期:  2023-03-08

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