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Independent Modal Control for Non-Self-Adjoint Problems.

Nitzsche, F. (1993) Independent Modal Control for Non-Self-Adjoint Problems. Holt Ashley Symposium, Stanford, CA, USA, September 23-24, 1993..

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Abstract

This study describes a general method of using the independent-modal-control concept in aeroservoelastic systems. Geometric modal filters, developed to individually control free-vibration modes using adptive materials, proved to be very efficient in preventing spillover-related effects. Very robust controllers may be synthesized due to the possibility of realizing a continuous and co-locasted distribution of the sensors and actuators over the structure. In the present investigation, the procedure is extended to non-self-adjoint problems, where the presence of non-conservative forces impairs the decoupling of the equations of motion by classical means, using the orthogonality of natural modes. An example developed for a composite wing demonstrates the validity of the proposed scheme.

Item URL in elib:https://elib.dlr.de/39597/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1993, pages=11,
Title:Independent Modal Control for Non-Self-Adjoint Problems.
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
Status:Published
Keywords:Non-Self-Adjoint Systems, Independent Modal Control, Fixed Wing, Gust Alleviation, Adaptive Structures.
Event Title:Holt Ashley Symposium, Stanford, CA, USA, September 23-24, 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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