基于多模型方法的航空发动机传感器故障诊断与估计

Wanli Zhao, Yingqing Guo, Chenyang Lai
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引用次数: 0

摘要

本文基于多模型方法,提出了一种航空发动机传感器故障诊断策略。设计了航空发动机相应的卡尔曼滤波器组。采用假设检验算法找出各模式出现的概率,然后根据最大概率准则对传感器故障进行检测和隔离。此外,对于多传感器故障诊断和估计,采用层次结构方法来实现,从而减少了模型数量,提高了计算速度。在仿真环境下,利用所提出的多模型方法对某涡扇发动机传感器的故障诊断与估计进行了研究。仿真结果表明,所提出的多模型方法能够有效地实现传感器故障诊断,并具有良好的鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Sensor Fault Diagnosis and Estimation Based on Multiple-Model Approach for Aeroengine
In this paper, based on the multiple-model (MM) approach, a sensor fault diagnosis strategy is proposed for aero engines. The aeroengine corresponding Kalman filter bank was designed. The hypothesis test algorithm is used to find the probability of each mode, and then the sensor fault is detected and isolated based on the criterion of maximum probability. In addition, for multi-sensor fault diagnosis and estimation, a hierarchical architecture approach is used to achieve, thereby reducing the number of models and increasing the speed of calculation. In the simulation environment, the proposed multi-model method was used to study the fault diagnosis and estimation of a certain turbofan engine sensor. Simulation results show that the proposed multi-model method can effectively achieve sensor fault diagnosis and has good robustness.
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