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Modal Sensors and Actuators for Individual Blade Control.

Nitzsche, F. (1993) Modal Sensors and Actuators for Individual Blade Control. The 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf., AIAA/ASME Adaptive Structures Forum, Part 6, LaJolla, CA, April 19 - 22, 1993..

Full text not available from this repository.

Abstract

A general method to incorporate independent modal control to the individual blade control of rotary wings is described. Piezoelectric material may be embedded inthe blade structure and conveniently shaped to generate efficient modal filters that present excellent rejection to spillover at the design condition. Closed-loop subsystems may be optimized to improve the damping characteristics of particular blade modes in the rotating frame, aiming at helicopter vibration suppression.

Item URL in elib:https://elib.dlr.de/39573/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1993, pages=10,
Title:Modal Sensors and Actuators for Individual Blade Control.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Nitzsche, F.UNSPECIFIEDUNSPECIFIED
Date:1993
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Part 6
Page Range:pp. 3507-3516
Series Name:AIAA-93-1703-CP
Status:Published
Keywords:Modal sensors, modal actuators, Independent Modal Control, Individual Blade Control (IBC), helicopter vibration.
Event Title:The 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf., AIAA/ASME Adaptive Structures Forum, Part 6, LaJolla, CA, April 19 - 22, 1993.
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:UNSPECIFIED
DLR - Program:W RP - Raumtransport
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 10:47

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