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Fault Tolerant Control of an Experimental Flexible Wing

Ossmann, Daniel and Pusch, Manuel (2019) Fault Tolerant Control of an Experimental Flexible Wing. Aerospace. Multidisciplinary Digital Publishing Institute (MDPI). DOI: 10.3390/aerospace6070076 ISSN 2226-4310

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Official URL: https://www.mdpi.com/2226-4310/6/7/76


Item URL in elib:https://elib.dlr.de/132451/
Document Type:Article
Title:Fault Tolerant Control of an Experimental Flexible Wing
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Ossmann, DanielDaniel.Ossmann (at) dlr.deUNSPECIFIED
Pusch, ManuelManuel.Pusch (at) dlr.deUNSPECIFIED
Date:2019
Journal or Publication Title:Aerospace
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI :10.3390/aerospace6070076
Publisher:Multidisciplinary Digital Publishing Institute (MDPI)
ISSN:2226-4310
Status:Published
Keywords:fault tolerant control; fault detection; control allocation; actuator faults; structural mode damping; wind tunnel experiments
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
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Deposited By: Pusch, Manuel
Deposited On:06 Dec 2019 17:04
Last Modified:14 Dec 2019 04:24

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