Title of article
A Fault-tolerance Estimating Method for Ionosphere Corrections in Satellite Navigation System
Author/Authors
GAO، نويسنده , , Shuliang and Li، نويسنده , , Rui and HUANG، نويسنده , , Zhigang، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2011
Pages
7
From page
749
To page
755
Abstract
Aiming to the reliable estimates of the ionosphere differential corrections for the satellite navigation system in the presence of the ionosphere anomaly, a fault-tolerance estimating method, which is based on the distributed Kalman filtering, is proposed. The method utilizes the parallel sub-filters for estimating the ionosphere differential corrections. Meanwhile, an infinite norm (IN) method is proposed for the detection of the ionosphere irregularity in the filter processing. Once the anomaly is detected, the sub-filter contaminated by the anomaly measurements will be excluded to ensure the reliability of the estimates. The simulation is conducted to validate the method and the results indicate that the anomaly can be found timely due to the novel fault detection method based on the infinite norm. Because of the parallel sub-filter architecture, the measurements are classified by the spatial distribution so that the ionosphere anomaly can be positioned and excluded more easily. Thus, the method can provide the robust and accurate ionosphere differential corrections.
Keywords
Differential corrections , ionosphere anomaly , fault-tolerance , Fault detection , Kalman filter
Journal title
Chinese Journal of Aeronautics
Serial Year
2011
Journal title
Chinese Journal of Aeronautics
Record number
2265078
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