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Parameter varying flutter suppression control for the BAH jet transport wing

Patartics, B. and Luspay, T. and Péni, T. and Takarics, B. and Vanek, B. and Kier, Thiemo (2017) Parameter varying flutter suppression control for the BAH jet transport wing. In: IFAC Proceedings Volumes (IFAC-PapersOnline), 50 (1), pp. 8163-8168. Elsevier. 20th World Congress of the International Federation of Automatic Control, July 9-14, Toulouse, France. DOI: 10.1016/j.ifacol.2017.08.1263

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Official URL: https://www.sciencedirect.com/science/article/pii/S2405896317317780

Abstract

The aeroelastic flutter is an undamped oscillation that occurs on flexible structures placed into an airflow. It is caused by the interaction of the structural dynamics and the aerodynamics. Since it generally leads to structural failure, it has to be avoided. The paper proposes a complete framework for handling the aeroservoelastic behavior of aerospace applications, addressing the high dimensional problem in a tractable manner. The applicability of the proposed methodology is demonstrated by designing a flutter suppression controller for the BAH jet transport wing.

Item URL in elib:https://elib.dlr.de/118410/
Document Type:Conference or Workshop Item (Speech)
Title:Parameter varying flutter suppression control for the BAH jet transport wing
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Patartics, B.Institute for Computer Science and Control (SZTAKI)UNSPECIFIED
Luspay, T.Institute for Computer Science and Control (SZTAKI),UNSPECIFIED
Péni, T.Institute for Computer Science and Control (SZTAKI),UNSPECIFIED
Takarics, B.Institute for Computer Science and Control (SZTAKI),UNSPECIFIED
Vanek, B.Institute for Computer Science and Control (SZTAKI),UNSPECIFIED
Kier, ThiemoThiemo.Kier (at) DLR.deUNSPECIFIED
Date:July 2017
Journal or Publication Title:IFAC Proceedings Volumes (IFAC-PapersOnline)
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:50
DOI :10.1016/j.ifacol.2017.08.1263
Page Range:pp. 8163-8168
Publisher:Elsevier
Series Name:IFAC-PapersOnLine
Status:Published
Keywords:aerospace linear parameter-varying systems model reduction robust control
Event Title:20th World Congress of the International Federation of Automatic Control
Event Location:Toulouse, France
Event Type:international Conference
Event Dates:July 9-14
Organizer:International Federation of Automatic Control (IFAC)
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: Kier, Thiemo
Deposited On:23 Jan 2018 09:42
Last Modified:31 Jul 2019 20:15

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