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Structural Aspects of Active Control Technology.

Hönlinger, H. (1995) Structural Aspects of Active Control Technology. CAE-DLR Workshop on Aeroelasticity 1995, Suzhon, China, 4-5 April, 1995..

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Abstract

A survey on the structurally relevant applications of Active Control Technology is presented. The benefits and disadvantages of various active control systems for transport aircraft are discussed. The problem of adverse structural coupling is addressed and possible solutions are outlined. Smart Structure Technology offers new applications for active control technology, but, in order to exploit its full potential, multidisciplinary design methods have to be improved.

Item URL in elib:https://elib.dlr.de/39703/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1995, pages=32,
Title:Structural Aspects of Active Control Technology.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hönlinger, H.UNSPECIFIEDUNSPECIFIED
Date:1995
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:servoaeroelasticity, structural coupling, active control, ride comfort.
Event Title:CAE-DLR Workshop on Aeroelasticity 1995, Suzhon, China, 4-5 April, 1995.
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 10:51

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