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DEVICE AND METHOD FOR COMPUTING AN ERROR BOUND OF A KALMAN FILTER BASED GNSS POSITION SOLUTION

机译:基于卡尔曼滤波器的GNSS位置解的误差界的计算装置和方法

摘要

The invention relates to a method for computing a bound B up to a given confidence level 1-4, of an error in a state vector estimation KSV of a state vector TSV of a physical system as provided by a Kalman filter. The method decomposes the errors of the Kalman solution as a sum of the errors due to each of the measurement types used in the filter, In addition, the contribution of each type of measurement is bounded by a multivariate t-distribution that considers the error terms from all the epochs processed. Then, the method implements three main operations:computing a probability distribution of the measurement errors for each epoch and measurement type;summing the previous distributions to obtain a global distribution that models the Kalman solution error; andcomputing the error bound B for a given confidence level from the resulting distribution.
机译:本发明涉及一种方法,该方法用于计算由卡尔曼滤波器提供的物理系统的状态向量TSV的状态向量估计KSV中的误差,直到给定的置信度1-4的边界B。该方法将Kalman解的误差分解为由于滤波器中使用的每种测量类型而导致的误差之和。此外,每种测量类型的贡献都由考虑误差项的多元t分布来界定。从所有时代开始。然后,该方法实现了三个主要操作: 计算每个时期和测量类型的测量误差的概率分布; 对先前的分布求和以获得一个全局分布模拟卡尔曼解法误差;和 从结果分布中计算给定置信度的错误绑定B。

著录项

  • 公开/公告号US2016109579A1

    专利类型

  • 公开/公告日2016-04-21

    原文格式PDF

  • 申请/专利权人 GMV AEROSPACE AND DEFENCE S.A.;

    申请/专利号US201514885642

  • 发明设计人 PEDRO FRANCISCO NAVARRO MADRID;

    申请日2015-10-16

  • 分类号G01S19/23;

  • 国家 US

  • 入库时间 2022-08-21 14:37:31

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