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Virtual flight testing of a controller for gust load alleviation using FMI for cosimulation

Müller, Reiko and Ritter, Markus (2017) Virtual flight testing of a controller for gust load alleviation using FMI for cosimulation. In: Proceedings of the 12 th International Modelica Conference, 132, pp. 921-928. Modelica Association and Linköping University Electronic Press. 12th International Modelica Conference, 15.-17. Mai 2017, Prag, Tschechien. DOI: 10.3384/ecp17132921 ISBN 978 91 7685 575 1 ISSN 1650-3686

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Official URL: https://www.modelica.org/events/modelica2017/proceedings/html/ProceedingsOfThe12thInternationalModelicaConference.pdf

Abstract

During aircraft design and certification, one of the most vital development tasks is the calculation of loads and stresses, subsequent structural sizing and iterative mutual adaptation with respect to the aircraft's systems. In an effort to build up a so called virtual flight testing capability in the DLR-wide project Digital-X (2012 - 2016), a simulation of a flexible aircraft model coupled with CFD based aerodynamics and a flight control system with included Gust Load Alleviation (GLA) was developed and subjected to a certification relevant gust encounter scenario. Due to the diversity of modeling and simulation tools present in the DLR, the Functional Mockup Interface (FMI) 2.0 model interfacing standard has been successfully employed to cosimulate the control system inside the enclosing simulation framework.

Item URL in elib:https://elib.dlr.de/112868/
Document Type:Conference or Workshop Item (Speech)
Title:Virtual flight testing of a controller for gust load alleviation using FMI for cosimulation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Müller, Reikoreiko.mueller (at) dlr.deUNSPECIFIED
Ritter, Markusmarkus.ritter (at) dlr.deUNSPECIFIED
Date:May 2017
Journal or Publication Title:Proceedings of the 12 th International Modelica Conference
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:132
DOI :10.3384/ecp17132921
Page Range:pp. 921-928
Publisher:Modelica Association and Linköping University Electronic Press
Series Name:Linköping Electronic Conference Proceedings
ISSN:1650-3686
ISBN:978 91 7685 575 1
Status:Published
Keywords:Kosimulation, Fluid- Struktur-Interaktion, Böenlastabminderung, virtuelle Flugtests
Event Title:12th International Modelica Conference
Event Location:Prag, Tschechien
Event Type:international Conference
Event Dates:15.-17. Mai 2017
Organizer:Czech Society for Cybernetics and Informatics (CSKI), Politecnico di Milano, Modelica Association
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - VicToria
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Müller, Reiko
Deposited On:16 Aug 2017 17:13
Last Modified:31 Jul 2019 20:10

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