无气味卡尔曼滤波算法在航空发动机性能退化评估中的应用

Ma Jingwei, Wei Fang, Cao Ming
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引用次数: 0

摘要

卡尔曼滤波和扩展卡尔曼滤波(EKF)在航空发动机性能评估中得到了广泛的应用。针对基于卡尔曼滤波的方法进行改进,探索将无气味卡尔曼滤波(Unscented Kalman Filter, UKF)算法应用于航空发动机性能退化评估。通过增加因子或调整预测方差矩阵,以及寻找Sigma点的最优分布,对UKF算法进行了改进,以获得最佳性能。仿真结果表明,与EKF算法和多维退化算法相比,本文提出的UKF算法在性能退化评估误差上有较大提升(33%),但存在数值计算时间长、对初始误差敏感等缺点。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Application of Unscented Kalman Filter Algorithm for Assessing the Aero Engine Performance Degradation
Kalman Filter and Extended Kalman Filter (EKF) have been widely applied for aero engine performance assessment. Aiming at improving upon the Kalman Filter based methods, this investigation explores applying Unscented Kalman Filter (UKF) algorithm for aero engine performance degradation evaluation. Improvements on the UKF algorithm are made for optimal performance, by adding a factor or adjusting the prediction variance matrix, as well as finding the optimal distribution of Sigma points. The simulation result shows that compared with EKF algorithm and with multi-dimensional degradation, the UKF algorithm proposed in this study improves the performance degradation assessment error by a large margin(33%), while suffering from prolonged numerical time and sensitivity to the initial error.
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