A Robust Unscented Kalman Filter for Intermittent and Featureless Aircraft Sensor Faults

被引:6
|
作者
Nie, Tongpan [1 ]
Deng, Ziyu [2 ]
Wang, Yu [1 ]
Qin, Xiansheng [2 ]
机构
[1] Aviation Ind Corp China, Aircraft Inst 1, Xian 710089, Peoples R China
[2] Northwestern Polytech Univ, Sch Mech Engn, Xian 710072, Peoples R China
来源
IEEE ACCESS | 2021年 / 9卷
关键词
Covariance matrices; Noise measurement; Kalman filters; Aircraft; Technological innovation; Observers; Measurement uncertainty; State estimation; intermittent measurements; fault detection; unscented Kalman filter;
D O I
10.1109/ACCESS.2021.3057889
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Fault tolerance is crucial to reliable state estimations in aircrafts. When time-varying sensor faults are coupled with nonlinear system models, it is non-trivial to robustly recover system states. In this paper, based on an intermittent-measurement unscented Kalman filter (IMUKF), we propose a new state-estimation method by combining the IMUKF with maximum-likelihood estimation and Gaussian mixture reduction. For nonlinear systems under time-varying and featureless sensor faults, the proposed method performs robust estimation without past error history or explicit fault detection, achieving significantly enhanced accuracy under severe conditions. With a nonlinear twin-spool jet engine as the example in simulations, the effectiveness of the proposed method is verified.
引用
收藏
页码:28832 / 28841
页数:10
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