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Design and Simulation of Semi-Active Landing Gears for Transport Aircraft

Krüger, W. (2002) Design and Simulation of Semi-Active Landing Gears for Transport Aircraft. In: Mechanics of Structures and Machines Volume 30, Number 4. Dekker. ISBN ISSN 0890-5452.

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Abstract

This paper describes an integrated design process for control laws for semi-active aircraft landing gears, addresses interfaces required for the implementation of different computer aided engineering (CAE) tools used in the process, and presents a multibody aircraft simulation model. Three control laws, a skyhook-type controller, a fuzzy-logic controller, and a state feedback controller, are designed, and the control parameters of all three controllers optimized using a multiobjective parameter optimization. Finally, simulation results for passive, fully active, and semi-active systems are compared.

Item URL in elib:https://elib.dlr.de/14364/
Document Type:Contribution to a Collection
Additional Information: LIDO-Berichtsjahr=2003,
Title:Design and Simulation of Semi-Active Landing Gears for Transport Aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krüger, W.UNSPECIFIEDUNSPECIFIED
Date:2002
Journal or Publication Title:Mechanics of Structures and Machines
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Number 4
Publisher:Dekker
Series Name:Volume 30
ISBN:ISSN 0890-5452
Status:Published
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):L - Flexible Aircraft (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: Klauer, Monika
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 21:45

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