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Vibration Control of Rotary Wings Using Smart Structures.

Nitzsche, F. and Breitbach, E. (1993) Vibration Control of Rotary Wings Using Smart Structures. International Forum on Aeroelasticity and Structural Dynamics 1993, Palais des CongrŠs, Strasbourg, France, 24-26 May 1993..

Full text not available from this repository.

Abstract

The problem of vibration reduction of rotary wings in forward flight is studied using the concept of individual blade control. Smart structures are used as a means to construct geometric modal filters able to perform independent modal control of the critical modes in the rotating frame. A real time controller that could circumvent the inherent nonlinearities of the system and is intrinsically robust is devised.

Item URL in elib:https://elib.dlr.de/39585/
Document Type:Conference or Workshop Item (Paper)
Additional Information: institution=Association A‚ronautique et Astronautique de France., LIDO-Berichtsjahr=1993, pages=17,
Title:Vibration Control of Rotary Wings Using Smart Structures.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Nitzsche, F.UNSPECIFIEDUNSPECIFIED
Breitbach, E.UNSPECIFIEDUNSPECIFIED
Date:1993
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 1
Page Range:pp. 293-309
Status:Published
Keywords:Helicopter vibration, smart structures, real-time controller, modal filters, individual-blade-control.
Event Title:International Forum on Aeroelasticity and Structural Dynamics 1993, Palais des CongrŠs, Strasbourg, France, 24-26 May 1993.
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 10:48

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