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The Smart Structures Technology in the Vibration Control of Helicopter Blades in forward Flight.

Nitzsche, F. (1) and Breitbach, E. (1992) The Smart Structures Technology in the Vibration Control of Helicopter Blades in forward Flight. EOS/SPIE and IOP Publishing Ltd 1992.. 1st European Conf. on Smart Structures and Materials, Glasgow, Scotland, May, 12-14, 1992..

Full text not available from this repository.

Abstract

The performance of a single input, single output, individual blade control system, designed to attenuate the helicopter rotor vibration using piezoelectric crystals (PZT) embedded in the blade structure, is studied. The results indicate that an efficient control of the blade lower damped modes, which significantly contribute to the unpleasant vibration of helicopters, may be achieved with a "smart" adptive controller.

Item URL in elib:https://elib.dlr.de/39518/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1992,
Title:The Smart Structures Technology in the Vibration Control of Helicopter Blades in forward Flight.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Nitzsche, F. (1)UNSPECIFIEDUNSPECIFIED
Breitbach, E.UNSPECIFIEDUNSPECIFIED
Date:1992
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 321-324
Publisher:EOS/SPIE and IOP Publishing Ltd 1992.
Series Name:Session (10), 11.00
Status:Published
Keywords:Helicopter vibration, forward-Flight equations, smart structures, individual-blade-control.
Event Title:1st European Conf. on Smart Structures and Materials, Glasgow, Scotland, May, 12-14, 1992.
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:46

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