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航空发动机MIMO系统的闭环辨识与故障诊断算法

任佳 马宏军

测控技术2017,Vol.36Issue(4):153-158,6.
测控技术2017,Vol.36Issue(4):153-158,6.

航空发动机MIMO系统的闭环辨识与故障诊断算法

Estimation and Fault Diagnosis Algorithm for Closed-Loop MIMO Aero-Engine Systems

任佳 1马宏军2

作者信息

  • 1. 中国飞机强度研究所航空结构强度动力学实验室,陕西西安710065
  • 2. 东北大学信息科学与工程学院,辽宁沈阳110819
  • 折叠

摘要

Abstract

Aero-engines have characteristics with complex structure and prone to fault,in addition,conventional modeling methods based on mechanism analysis have troubles of complicated process and low operational efficiency.To solve these problems,an algorithm is proposed for parameter identification and fault diagnosis based on data,which could be used in closed-loop MIMO(multiple-input multiple-output) aero-engine systems.By choosing appropriate auxiliary parameters,auxiliary models are established.Then time delay is calculated by determining the order of the auxiliary model,parameters of forward channels and feedback channels are identified by multi-stage least square algorithm.An example of biaxial gas turbine engine system is given for certification.It shows that the algorithm could be used for diagnosing gas path fault when the forgetting factor is changing by convergence of recognition result.Finally,two kinds of important characteristics are introduced,about importance and principium of selecting forgetting factor and excluding disturbance of noises by distinguishing it from the fault result.

关键词

航空发动机/MIMO系统/闭环辨识/故障诊断/最小二乘/辅助模型

Key words

aero-engine/MIMO system/closed-loop identification/fault diagnosis/least square/auxiliary model

分类

航空航天

引用本文复制引用

任佳,马宏军..航空发动机MIMO系统的闭环辨识与故障诊断算法[J].测控技术,2017,36(4):153-158,6.

基金项目

国家自然科学基金面上项目(61473067) (61473067)

测控技术

OACSCDCSTPCD

1000-8829

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