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Real-time model- and harmonics based actuator health monitoring

van der Linden, Franciscus L. J. and Dorkel, Andre (2017) Real-time model- and harmonics based actuator health monitoring. Shaker Verlag. 6th International Workshop on Aircraft System Technologies, 21.-22.Feb. 2017, Hamburg, Germany. ISBN 978-3-8440-5086-8.

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A Health Monitoring (HM) method, optimized for low computational power realtime computers, is presented for the detection of faults in an Electro Mechanical Actuator (EMA). The method is based on 5 steps: 1. Pre-processing of the sensor data using Kalman filtering, 2. Generating residuals, 3. Selection of the usable data for detection, 4. Harmonic analysis to identify the faults and increase the sensitivity and 5. Decision making to classify the faults. The method is tested on simulation data.

Item URL in elib:https://elib.dlr.de/115061/
Document Type:Conference or Workshop Item (Speech)
Title:Real-time model- and harmonics based actuator health monitoring
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
van der Linden, Franciscus L. J.franciscus.vanderlinden (at) dlr.dehttps://orcid.org/0000-0002-1820-7531
Dorkel, Andreandre.dorkel (at) liebherr.comUNSPECIFIED
Date:February 2017
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
Page Range:pp. 43-50
Publisher:Shaker Verlag
Keywords:Health Monitoring, EMA
Event Title:6th International Workshop on Aircraft System Technologies
Event Location:Hamburg, Germany
Event Type:international Conference
Event Dates:21.-22.Feb. 2017
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems and Cabin (old)
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control
Deposited By: van der Linden, Franciscus
Deposited On:06 Nov 2017 16:23
Last Modified:31 Jul 2019 20:12

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