elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Kontakt | English
Schriftgröße: [-] Text [+]

Surrogate-enhanced simulation of aircraft in trimmed state

Michler, Andreas K. und Heinrich, Ralf (2012) Surrogate-enhanced simulation of aircraft in trimmed state. Computer Methods in Applied Mechanics and Engineering, 217 (04), Seiten 96-110. Elsevier. DOI: 10.1016/j.cma.2012.01.010. ISSN 0045-7825.

Dieses Archiv kann nicht den gesamten Text zur Verfügung stellen.

Offizielle URL: http://dx.doi.org/10.1016/j.cma.2012.01.010

Kurzfassung

This paper presents a surrogate-enhanced methodology for high-fidelity simulation of aircraft in trimmed state. Surrogates of the aerodynamic loads are used to increase robustness and reduce the number of costly high-fidelity simulations necessary during trim simulations. This is accomplished in two steps: (1) by finding a suitable estimate for the solution by global and fast local searches performed on surrogates, and (2) by applying a hybrid local search to check the potential solution and to further increase its quality if necessary. For the local searches in both steps, a Newton method is employed, whereas a genetic algorithm is used only in the first step. For the Newton method, the entries of the Jacobian are provided by means of finite difference approximations and the complex-step derivative method (CSD) based on the surrogates, and it is shown how to make CSD applicable to surrogates based on radial basis functions (RBFs). In the hybrid search, the derivatives are calculated by means of surrogates, while high-fidelity simulations are used for the main calculations of the Newton method. Updating the surrogates with the results of the latter is found to significantly accelerate the convergence of the hybrid local search. The methodology is applied to challenging trim test cases, in which several of the control surfaces of a generic fighter aircraft are deflected during trim simulation. Control surface deflection is performed via RBF-based mesh deformation, and RBFs are also used for surrogate modelling, thereby fostering code modularity and re-use.

Dokumentart:Zeitschriftenbeitrag
Zusätzliche Informationen:The article is available at the following website: http://dx.doi.org/10.1016/j.cma.2012.01.010, 1 April 2012, Vol. 210-220
Titel:Surrogate-enhanced simulation of aircraft in trimmed state
Autoren:
AutorenInstitution oder E-Mail-Adresse der Autoren
Michler, Andreas K.NICHT SPEZIFIZIERT
Heinrich, RalfNICHT SPEZIFIZIERT
Datum:2012
Erschienen in:Computer Methods in Applied Mechanics and Engineering
Referierte Publikation:Ja
In SCOPUS:Ja
In ISI Web of Science:Ja
Band:217
DOI :10.1016/j.cma.2012.01.010
Seitenbereich:Seiten 96-110
Verlag:Elsevier
ISSN:0045-7825
Status:veröffentlicht
Stichwörter:surrogate modelling; aircraft trim simulation; mesh deformation; control surface deflection; radial basis functions; complex-step derivative method
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Starrflügler (alt)
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AR - Starrflüglerforschung
DLR - Teilgebiet (Projekt, Vorhaben):L - Flugphysik (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Hinterlegt von: Andreas Michler
Hinterlegt am:31 Jan 2012 14:09
Letzte Änderung:26 Mär 2015 17:20

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Copyright © 2008-2013 Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.