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System and method for dynamically estimating output variances for carrier-smoothing filters

机译:动态估计载波平滑滤波器的输出方差的系统和方法

摘要

An improved system and method is disclosed for dynamically estimating the output variances of carrier-smoothing filters used, for example, in GPS receivers. By accurately estimating the output variances of the carrier-smoothing filters as they transition from initialization to steady-state operation, it is possible to calculate any required protection levels without having to wait for the filters to fully stabilize. As one example, a system for estimating output variances of a carrier-smoothing filter for use in a satellite navigation system receiver is disclosed, which includes a plurality of smoothing filters associated with a navigation processing unit in a satellite navigation receiver. One or more processors associated with the navigation processing unit executes an algorithm for each smoothing filter, which provides a method for dynamically calculating an output variance for a respective smoothing filter as it transitions in response to new input variance values. The method also predicts the settling point of the output variance for that smoothing filter given a set of pseudorange and carrier-phase values to be applied. Therefore, using this novel output variance prediction method, precision navigation applications such as, for example, airbome GPS-based precision landing system applications can begin operations with suitable calculated protection level values without having to wait for the smoothing filters to stabilize. Thus, such precision landing systems are available for use as soon as the required protection level values are reached.
机译:公开了一种用于动态估计例如在GPS接收机中使用的载波平滑滤波器的输出方差的改进的系统和方法。通过在载波平滑滤波器从初始化过渡到稳态操作时准确估计其平滑度,可以计算出任何所需的保护级别,而不必等待滤波器完全稳定。作为一个示例,公开了一种用于估计在卫星导航系统接收机中使用的载波平滑滤波器的输出方差的系统,该系统包括与卫星导航接收机中的导航处理单元相关联的多个平滑滤波器。与导航处理单元相关联的一个或多个处理器针对每个平滑滤波器执行算法,该算法提供了一种用于动态计算相应平滑滤波器响应于新的输入方差值而转变时的输出方差的方法。该方法还针对给定的一组伪距和载波相位值,预测了该平滑滤波器的输出方差的稳定点。因此,使用这种新颖的输出方差预测方法,精确导航应用程序(例如基于机载GPS的精确着陆系统应用程序)可以以适当的计算出的保护等级值开始操作,而不必等待平滑滤波器稳定下来。因此,一旦达到要求的防护等级值,就可以使用这种精确着陆系统。

著录项

  • 公开/公告号EP1760484A3

    专利类型

  • 公开/公告日2008-06-25

    原文格式PDF

  • 申请/专利权人 HONEYWELL INTERNATIONAL INC.;

    申请/专利号EP20060119782

  • 发明设计人 MORGAN KENNETH S.;MAY REED R.;

    申请日2006-08-30

  • 分类号G01S1/00;

  • 国家 EP

  • 入库时间 2022-08-21 19:57:48

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