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Vibration Control of Rotary Wings Using Smart Structures

Nitzsche, F. and Breitbach, E. (1994) Vibration Control of Rotary Wings Using Smart Structures. Smart Materials and Structures, 3 (2), pp. 181-189.

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/39690/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=1994,
Title:Vibration Control of Rotary Wings Using Smart Structures
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Nitzsche, F.UNSPECIFIEDUNSPECIFIED
Breitbach, E.UNSPECIFIEDUNSPECIFIED
Date:1994
Journal or Publication Title:Smart Materials and Structures
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:3
Page Range:pp. 181-189
Status:Published
Keywords:Helicopter vibration, smart structures, real-time controller, modal filters, individual blade-control.
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
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 10:51

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