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LPV model-based robust diagnosis of flight actuator faults

Varga, Andreas and Ossmann, Daniel (2013) LPV model-based robust diagnosis of flight actuator faults. Control Engineering Practice. Elsevier. DOI: 10.1016/j.conengprac.2013.11.004 ISSN 0967-0661

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Official URL: http://authors.elsevier.com/sd/article/S0967066113002086

Abstract

A linear parameter-varying (LPV) model-based synthesis, tuning and assessment methodology is developed and applied for the design of a robust fault detection and diagnosis (FDD) system for several types of flight actuator faults such as jamming, runaway, oscillatory failure, or loss of efficiency. The robust fault detection is achieved by using a synthesis approach based on an accurate approximation of the nonlinear actuator-control surface dynamics via an LPV model and an optimal tuning of the free parameters of the FDD system using multi-objective optimization techniques. Real-time signal processing is employed for identification of different fault types. The assessment of the FDD system robustness has been performed using both standard Monte Carlo methods as well as advanced worst-case search based optimization-driven robustness analysis. A supplementary industrial validation performed on the AIRBUS actuator test bench for the monitoring of jamming, confirmed the satisfactory performance of the FDD system in a true industrial setting.

Item URL in elib:https://elib.dlr.de/86817/
Document Type:Article
Title:LPV model-based robust diagnosis of flight actuator faults
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Varga, AndreasAndreas.Varga (at) DLR.deUNSPECIFIED
Ossmann, Danieldaniel.ossmann (at) dlr.deUNSPECIFIED
Date:11 December 2013
Journal or Publication Title:Control Engineering Practice
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI :10.1016/j.conengprac.2013.11.004
Publisher:Elsevier
ISSN:0967-0661
Status:Published
Keywords:fault detection, fault identification, fault diagnosis, flight actuator faults.
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems & Cabin (old)
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Deposited By: Varga, Dr.-Ing. Andreas
Deposited On:18 Dec 2013 11:24
Last Modified:31 Jul 2019 19:44

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