FALSE ALARM DISTRIBUTION IN ADVANCED RECEIVER AUTONOMOUS INTEGRITY MONITORING

    公开(公告)号:EP3373041A1

    公开(公告)日:2018-09-12

    申请号:EP18160320.0

    申请日:2018-03-06

    IPC分类号: G01S19/20

    CPC分类号: G01S19/20

    摘要: A Global Navigation Satellite System receiver (102) comprising at least one processor (104) is provided. The processor is configured to: determine a weighted false alarm probability allocation for at least one sub-solution in a solution separation based integrity monitoring module (130), wherein the weighted false alarm probability allocation is based on pre-determined values for missed detection probability and fault probability for the sub-solution, wherein the at least one sub-solution is created by excluding a set of potentially faulty satellites from a full solution, wherein a fault mode occurs when there is a faulty satellite in the excluded set of potentially faulty satellite, wherein the at least one sub-solution's missed detection probability is probability that detection of associated fault mode occurrence in a sub-solution was missed, and wherein the at least one sub-solution's fault probability is probability that the fault mode occurs; compute a weighted protection level based on the weighted false alarm probability.

    A method for reducing an impact of signal anomalies on a device for position detection in a global navigation system
    7.
    发明公开
    A method for reducing an impact of signal anomalies on a device for position detection in a global navigation system 审中-公开
    一种用于减少信号异常的影响,一种用于确定在全球导航系统位置的方法

    公开(公告)号:EP2930534A1

    公开(公告)日:2015-10-14

    申请号:EP14001485.3

    申请日:2014-04-11

    申请人: Astrium GmbH

    发明人: Oehler, Veit

    IPC分类号: G01S19/20

    CPC分类号: G01S19/20

    摘要: The present disclosure provides a method for reducing an impact of signal anomalies on a device for position detection in a global navigation system, which includes a plurality of space vehicles transmitting navigation signals to the device for position detection. The method includes the steps of:
    1) receiving, by the device, a first group of navigation signals from the space vehicles, each navigation signal having an integrity risk contribution associated thereto;
    2) calculating, by the device, at least one first overall integrity of the first group of navigation signals based on their associated integrity risk contributions, the method further including,
    3) if the at least one first overall integrity is below a first predetermined threshold, determining a position of the device; or
    4) if at least one first overall integrity exceeds the first predetermined threshold,
    4a) removing n navigation signals having the highest integrity risk contributions from the first group to obtain a second group of navigation signals, n being a natural number;
    4b) determining the position of the device based on the group of navigation signals obtained in step 4a).

    摘要翻译: 本公开提供了一种用于在全球导航系统,其包括空间飞行器发射的导航信号,以用于位置检测的装置的多个A装置上的信号异常的影响的减少用于位置检测的方法。 该方法包括如下步骤:具有向与其相关联的贡献完整性风险每个导航信号1)接收由所述装置中,从空间飞行器的导航信号的第一组; 2)计算,由装置的基础上,他们的相关联的完整性风险捐款的第一组导航信号中的至少一个第一整体完整性,该方法还包括,3)如果所述至少一个第一整体完整性是低于第一预定阈值 的,确定性的采矿设备的位置; 或4)如果至少一个第一整体完整性超过第一预定阈值,图4a)去除具有与所述第一组的最高完整性风险的贡献,以获得导航信号的第二组,其中n是一个自然数n的导航信号; 4b)的确定性采矿设备的基于组在步骤4a中获得导航信号)的位置。

    Multi-level/multi-threshold/multi-persistency GPS/GNSS atomic clock monitoring
    8.
    发明公开
    Multi-level/multi-threshold/multi-persistency GPS/GNSS atomic clock monitoring 有权
    多级/ mehrschwellige /多个持久化GPS / GNSS原子钟监控

    公开(公告)号:EP2897001A2

    公开(公告)日:2015-07-22

    申请号:EP14198176.1

    申请日:2014-12-16

    IPC分类号: G04F5/14 G01R23/00

    摘要: Methods and apparatus to monitor GPS/GNSS atomic clocks are disclosed. An example method includes establishing a measured difference between an atomic frequency standard (AFS) and a monitoring device. The method also includes modeling an estimated difference model between the AFS and the monitoring device, and computing a residual signal based on the measured difference and the estimated difference model. In addition, the method includes analyzing, by a first detector, the residual signal at multiple thresholds, each of the thresholds having a corresponding persistency defining the number of times a threshold is exceeded before one or more of a phase jump, a rate jump, or an acceleration error is indicated. Furthermore, the method includes analyzing, by a second detector, a parameter of the estimated difference model at multiple thresholds, each of the thresholds having a corresponding persistency defining the number of times a drift threshold is exceeded before a drift is indicated.

    Architectures for high integrity multi-constellation solution separation
    9.
    发明公开
    Architectures for high integrity multi-constellation solution separation 审中-公开
    用于高度完整性多星座解决方案分离的架构

    公开(公告)号:EP2887097A2

    公开(公告)日:2015-06-24

    申请号:EP14190750.1

    申请日:2014-10-28

    IPC分类号: G01S19/20 G01S19/42

    CPC分类号: G01S19/20 G01S19/421

    摘要: A method comprises receiving a plurality of signals from a plurality of space-based satellites, wherein the plurality of space-based satellites comprises at least one space-based satellite from each of a plurality of Navigation Satellite System (NSS) constellations. The method also comprises determining, in a first domain, a first plurality of sub-solutions based on a respective sub-set of the plurality of signals, each respective sub-set in the first domain chosen according to a characteristic defining the first domain; and determining, in a second domain, a second plurality of sub-solutions based on a respective sub-set of the plurality of signals, each respective sub-set in the second domain chosen according to a characteristic defining the second domain. The method further comprises determining if an error is present in the navigation system based on the first plurality of sub-solutions and on the second plurality of sub-solutions.

    摘要翻译: 一种方法包括:从多个基于空间的卫星接收多个信号,其中所述多个基于空间的卫星包括来自多个导航卫星系统(NSS)星座中的每一个的至少一个基于空间的卫星。 该方法还包括基于多个信号的相应子集在第一域中确定第一多个子解,根据定义第一域的特性选择第一域中的每个相应子集; 以及基于所述多个信号的相应子集在第二域中确定第二多个子解,根据定义所述第二域的特性选择所述第二域中的每个相应子集。 该方法还包括基于第一多个子方案和第二多个子方案来确定导航系统中是否存在错误。