Invention Grant
- Patent Title: Device and method for computing an error bound for a Kalman filter based global navigation satellite system (GMSS) position
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Application No.: US14885642Application Date: 2015-10-16
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Publication No.: US10254412B2Publication Date: 2019-04-09
- Inventor: Pedro Francisco Navarro Madrid
- Applicant: GMV AEROSPACE AND DEFENCE, S.A.
- Applicant Address: ES Madrid
- Assignee: GMV AEROSPACE AND DEFENCE, S.A.
- Current Assignee: GMV AEROSPACE AND DEFENCE, S.A.
- Current Assignee Address: ES Madrid
- Priority: EP14189240 20141016
- Main IPC: G01S19/39
- IPC: G01S19/39

Abstract:
The invention relates to a method for computing a bound B up to a given confidence level 1−α, 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; and computing the error bound B for a given confidence level from the resulting distribution.
Public/Granted literature
- US20160109579A1 DEVICE AND METHOD FOR COMPUTING AN ERROR BOUND OF A KALMAN FILTER BASED GNSS POSITION SOLUTION Public/Granted day:2016-04-21
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