Robust error-state Kalman-type filters for attitude estimation

被引:2
|
作者
Belles, Andrea [1 ]
Medina, Daniel [1 ]
Chauchat, Paul [2 ]
Labsir, Samy [3 ]
Vila-Valls, Jordi [4 ]
机构
[1] German Aerosp Ctr DLR, Neustrelitz, Germany
[2] Aix Marseille Univ, CNRS, LIS, Marseille, France
[3] IPSA TeSA, Toulouse, France
[4] ISAE SUPAERO, Toulouse, France
来源
关键词
Attitude estimation; Quaternion estimation; GNSS; Error-state filters; Robust filtering; Robust statistics;
D O I
10.1186/s13634-024-01172-w
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
State estimation techniques appear in a plethora of engineering fields, in particular for the attitude estimation application of interest in this contribution. A number of filters have been devised for this problem, in particular Kalman-type ones, but in their standard form they are known to be fragile against outliers. In this work, we focus on error-state filters, designed for states living on a manifold, here unit-norm quaternions. We propose extensions based on robust statistics, leading to two robust M-type filters able to tackle outliers either in the measurements, in the system dynamics or in both cases. The performance and robustness of these filters is explored in a numerical experiment. We first assess the outlier ratio that they manage to mitigate, and second the type of dynamics outliers that they can detect, showing that the filter performance depends on the measurements' properties.
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收藏
页数:19
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