Detection and Identification of Loss of Efficiency Faults of Flight Actuators

We propose linear parameter-varying (LPV) model-based approaches to the synthesis of robust fault detection and diagnosis (FDD) systems for loss of efficiency (LOE) faults of flight actuators. The proposed methods are applicable to several types of parametric (or multiplicative) LOE faults such as a...

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Main Authors: Ossmann Daniel, Varga Andreas
Format: Article
Language:English
Published: Sciendo 2015-03-01
Series:International Journal of Applied Mathematics and Computer Science
Subjects:
Online Access:https://doi.org/10.1515/amcs-2015-0004
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spelling doaj-b70c83ec5074489d97e4f0d167e97dfe2021-09-06T19:39:48ZengSciendoInternational Journal of Applied Mathematics and Computer Science2083-84922015-03-01251536310.1515/amcs-2015-0004amcs-2015-0004Detection and Identification of Loss of Efficiency Faults of Flight ActuatorsOssmann Daniel0Varga Andreas1Institute of System Dynamics and Control DLR Oberpfaffenhofen, D-82234 Wessling, GermanyInstitute of System Dynamics and Control DLR Oberpfaffenhofen, D-82234 Wessling, GermanyWe propose linear parameter-varying (LPV) model-based approaches to the synthesis of robust fault detection and diagnosis (FDD) systems for loss of efficiency (LOE) faults of flight actuators. The proposed methods are applicable to several types of parametric (or multiplicative) LOE faults such as actuator disconnection, surface damage, actuator power loss or stall loads. For the detection of these parametric faults, advanced LPV-model detection techniques are proposed, which implicitly provide fault identification information. Fast detection of intermittent stall loads (seen as nuisances, rather than faults) is important in enhancing the performance of various fault detection schemes dealing with large input signals. For this case, a dedicated fast identification algorithm is devised. The developed FDD systems are tested on a nonlinear actuator model which is implemented in a full nonlinear aircraft simulation model. This enables the validation of the FDD system’s detection and identification characteristics under realistic conditions.https://doi.org/10.1515/amcs-2015-0004aerospace engineeringfault detection and diagnosisloss of efficiency type of faultsflight actuator faults
collection DOAJ
language English
format Article
sources DOAJ
author Ossmann Daniel
Varga Andreas
spellingShingle Ossmann Daniel
Varga Andreas
Detection and Identification of Loss of Efficiency Faults of Flight Actuators
International Journal of Applied Mathematics and Computer Science
aerospace engineering
fault detection and diagnosis
loss of efficiency type of faults
flight actuator faults
author_facet Ossmann Daniel
Varga Andreas
author_sort Ossmann Daniel
title Detection and Identification of Loss of Efficiency Faults of Flight Actuators
title_short Detection and Identification of Loss of Efficiency Faults of Flight Actuators
title_full Detection and Identification of Loss of Efficiency Faults of Flight Actuators
title_fullStr Detection and Identification of Loss of Efficiency Faults of Flight Actuators
title_full_unstemmed Detection and Identification of Loss of Efficiency Faults of Flight Actuators
title_sort detection and identification of loss of efficiency faults of flight actuators
publisher Sciendo
series International Journal of Applied Mathematics and Computer Science
issn 2083-8492
publishDate 2015-03-01
description We propose linear parameter-varying (LPV) model-based approaches to the synthesis of robust fault detection and diagnosis (FDD) systems for loss of efficiency (LOE) faults of flight actuators. The proposed methods are applicable to several types of parametric (or multiplicative) LOE faults such as actuator disconnection, surface damage, actuator power loss or stall loads. For the detection of these parametric faults, advanced LPV-model detection techniques are proposed, which implicitly provide fault identification information. Fast detection of intermittent stall loads (seen as nuisances, rather than faults) is important in enhancing the performance of various fault detection schemes dealing with large input signals. For this case, a dedicated fast identification algorithm is devised. The developed FDD systems are tested on a nonlinear actuator model which is implemented in a full nonlinear aircraft simulation model. This enables the validation of the FDD system’s detection and identification characteristics under realistic conditions.
topic aerospace engineering
fault detection and diagnosis
loss of efficiency type of faults
flight actuator faults
url https://doi.org/10.1515/amcs-2015-0004
work_keys_str_mv AT ossmanndaniel detectionandidentificationoflossofefficiencyfaultsofflightactuators
AT vargaandreas detectionandidentificationoflossofefficiencyfaultsofflightactuators
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