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Structured Control Design for a Highly Flexible Flutter Demonstrator

Pusch, Manuel and Ossmann, Daniel and Luspay, Tamás (2019) Structured Control Design for a Highly Flexible Flutter Demonstrator. Aerospace. Multidisciplinary Digital Publishing Institute (MDPI). ISSN 2226-4310

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Item URL in elib:https://elib.dlr.de/126737/
Document Type:Article
Title:Structured Control Design for a Highly Flexible Flutter Demonstrator
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Pusch, ManuelManuel.Pusch (at) DLR.deUNSPECIFIED
Ossmann, Danieldaniel.ossmann (at) dlr.deUNSPECIFIED
Luspay, TamásSztakiUNSPECIFIED
Date:5 March 2019
Journal or Publication Title:Aerospace
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:Yes
In ISI Web of Science:No
Publisher:Multidisciplinary Digital Publishing Institute (MDPI)
ISSN:2226-4310
Status:Published
Keywords:flutter control; flight control; structured control design; model based control design; optimal blending; non-linear simulation
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:11 Mar 2019 14:50
Last Modified:11 Mar 2019 14:50

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