A System-Level Failure Propagation Detectability Using ANFIS for an Aircraft Electrical Power System

The Electrical Power System (EPS) in an aircraft is designed to interact extensively with other systems. With a growing trend towards more electric aircraft, the complexity of interactions between the EPS and other systems has grown. This has resulted in an increased necessity of implementing health...

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Main Authors: Cordelia Mattuvarkuzhali Ezhilarasu, Ian K. Jennions
Format: Article
Language:English
Published: MDPI AG 2020-04-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/10/8/2854
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spelling doaj-7c84ea50f3804e38a890a2bd1be14f8f2020-11-25T03:10:24ZengMDPI AGApplied Sciences2076-34172020-04-01102854285410.3390/app10082854A System-Level Failure Propagation Detectability Using ANFIS for an Aircraft Electrical Power SystemCordelia Mattuvarkuzhali Ezhilarasu0Ian K. Jennions1IVHM Centre, Cranfield University, Cranfield MK43 0AL, UKIVHM Centre, Cranfield University, Cranfield MK43 0AL, UKThe Electrical Power System (EPS) in an aircraft is designed to interact extensively with other systems. With a growing trend towards more electric aircraft, the complexity of interactions between the EPS and other systems has grown. This has resulted in an increased necessity of implementing health monitoring methods like diagnosis and prognosis of the EPS at the systems level. This paper focuses on developing a diagnostic algorithm for the EPS to detect and isolate faults and their root causes that occur at the Line Replaceable Units (LRUs) connecting with aircraft systems like the engine and the fuel system. This paper aims to achieve this in two steps: (i) developing an EPS digital twin and presenting the simulation results for both healthy and fault scenarios, (ii) developing an Adaptive Neuro-Fuzzy Inference System (ANFIS) monitor to detect faults in the EPS. The results from the ANFIS monitor are processed in two methods: (i) a crisp boundary approach, and (ii) a fuzzy boundary approach. The former approach has a poor misclassification rate; hence the latter method is chosen to combine with causal reasoning for isolating root causes of these interacting faults. The results from both these methods are presented through examples in this paper.https://www.mdpi.com/2076-3417/10/8/2854Electrical Power SystemANFIScausal reasoningdiagnosisfault propagationaircraft
collection DOAJ
language English
format Article
sources DOAJ
author Cordelia Mattuvarkuzhali Ezhilarasu
Ian K. Jennions
spellingShingle Cordelia Mattuvarkuzhali Ezhilarasu
Ian K. Jennions
A System-Level Failure Propagation Detectability Using ANFIS for an Aircraft Electrical Power System
Applied Sciences
Electrical Power System
ANFIS
causal reasoning
diagnosis
fault propagation
aircraft
author_facet Cordelia Mattuvarkuzhali Ezhilarasu
Ian K. Jennions
author_sort Cordelia Mattuvarkuzhali Ezhilarasu
title A System-Level Failure Propagation Detectability Using ANFIS for an Aircraft Electrical Power System
title_short A System-Level Failure Propagation Detectability Using ANFIS for an Aircraft Electrical Power System
title_full A System-Level Failure Propagation Detectability Using ANFIS for an Aircraft Electrical Power System
title_fullStr A System-Level Failure Propagation Detectability Using ANFIS for an Aircraft Electrical Power System
title_full_unstemmed A System-Level Failure Propagation Detectability Using ANFIS for an Aircraft Electrical Power System
title_sort system-level failure propagation detectability using anfis for an aircraft electrical power system
publisher MDPI AG
series Applied Sciences
issn 2076-3417
publishDate 2020-04-01
description The Electrical Power System (EPS) in an aircraft is designed to interact extensively with other systems. With a growing trend towards more electric aircraft, the complexity of interactions between the EPS and other systems has grown. This has resulted in an increased necessity of implementing health monitoring methods like diagnosis and prognosis of the EPS at the systems level. This paper focuses on developing a diagnostic algorithm for the EPS to detect and isolate faults and their root causes that occur at the Line Replaceable Units (LRUs) connecting with aircraft systems like the engine and the fuel system. This paper aims to achieve this in two steps: (i) developing an EPS digital twin and presenting the simulation results for both healthy and fault scenarios, (ii) developing an Adaptive Neuro-Fuzzy Inference System (ANFIS) monitor to detect faults in the EPS. The results from the ANFIS monitor are processed in two methods: (i) a crisp boundary approach, and (ii) a fuzzy boundary approach. The former approach has a poor misclassification rate; hence the latter method is chosen to combine with causal reasoning for isolating root causes of these interacting faults. The results from both these methods are presented through examples in this paper.
topic Electrical Power System
ANFIS
causal reasoning
diagnosis
fault propagation
aircraft
url https://www.mdpi.com/2076-3417/10/8/2854
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