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Data-driven approximation of a high fidelity gust-oriented flexible aircraft dynamical model

Poussot-Vassal, Charles and Quero, David and Vuillemin, Pierre (2018) Data-driven approximation of a high fidelity gust-oriented flexible aircraft dynamical model. MATHMOD (International Conference on Mathematical Modelling), 21.-23. Feb. 2018, Wien, Österreich.

Full text not available from this repository.

Abstract

Computing responses to discrete gusts are sizing steps when designing and optimizing a new aircraft structure and geometry. Indeed, this is part of the imposed clearance certifications requested by the flight authorities. During the aircraft preliminary design phase, this clearance is done by intensive simulations, however, due to the involved models complexity, these latter are time consuming and imply an important computational burden. Especially as these simulations are involved at different steps of the aircraft optimisation process e.g. by aeroelastic, flight and control engineers. In this paper we propose a systematic way to fasten the gust simulation step and simplify the analysis by mean of data-driven model approximation in the Loewner framework. The proposed approach gathers recent advances in aeroelastic modelling and model approximation techniques. As illustrated on a high fidelity long range aircraft model, the drastic reduction of the simulation time does not induce any significant loss of accuracy.

Item URL in elib:https://elib.dlr.de/119148/
Document Type:Conference or Workshop Item (Speech)
Title:Data-driven approximation of a high fidelity gust-oriented flexible aircraft dynamical model
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Poussot-Vassal, CharlesONERAUNSPECIFIED
Quero, Daviddavid.queromartin (at) dlr.deUNSPECIFIED
Vuillemin, PierreONERAUNSPECIFIED
Date:February 2018
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:model reduction, data-driven, flexible aircraft
Event Title:MATHMOD (International Conference on Mathematical Modelling)
Event Location:Wien, Österreich
Event Type:international Conference
Event Dates:21.-23. Feb. 2018
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 - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Quero-Martin, David
Deposited On:20 Jun 2018 15:48
Last Modified:19 Jul 2018 15:00

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