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Vibration Control of Flexible Aircraft with Respect to Passengers Comfort

Zuziak, P. and Šika, Z. and Valášek, M. and Vampola, T. and Klimmek, T. (2010) Vibration Control of Flexible Aircraft with Respect to Passengers Comfort. ISMA 2010 - International Conference on Noise & Vibration Engineering, 20 -22 Oct. 2010, Leuven, Belgium.

Full text not available from this repository.

Abstract

The paper deals with the development of the active vibration suppression of fuselage of flexible aircraft of BWB (blended wing body) type with respect to comfort criterions. The independent system of the proof mass actuators within the fuselage is considered as actuators, accelerometers throughout the fuselage are considered as the sensors. The placement of actuators and sensors is optimized through the special norms minimization. The feedback control design is done by H∞ method. The robustness of the controller is tested with respect to the fuel and passengers mass variations.

Item URL in elib:https://elib.dlr.de/84298/
Document Type:Conference or Workshop Item (Speech)
Title:Vibration Control of Flexible Aircraft with Respect to Passengers Comfort
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Zuziak, P.CTU in Prague, FME, Department of Mechanics, Biomechanics and MechatronicsUNSPECIFIED
Šika, Z.CTU in Prague, FME, Department of Mechanics, Biomechanics and MechatronicsUNSPECIFIED
Valášek, M.CTU in Prague, FME, Department of Mechanics, Biomechanics and MechatronicsUNSPECIFIED
Vampola, T.CTU in Prague, FME, Department of Mechanics, Biomechanics and MechatronicsUNSPECIFIED
Klimmek, T.UNSPECIFIEDUNSPECIFIED
Date:2010
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:vibration control, blended wing body, passenger comfort, NACRE-fw,
Event Title:ISMA 2010 - International Conference on Noise & Vibration Engineering
Event Location:Leuven, Belgium
Event Type:international Conference
Event Dates:20 -22 Oct. 2010
Organizer:Katholieke Universiteit Leuven
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Klimmek, Thomas
Deposited On:25 Sep 2013 14:29
Last Modified:08 May 2014 23:24

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