Skip to main content
Top

2018 | OriginalPaper | Chapter

Coupling of Recurrent and Static Neural Network Approaches for Improved Multi-step Ahead Time Series Prediction

Authors : Maximilian Winter, Christian Breitsamter

Published in: New Results in Numerical and Experimental Fluid Mechanics XI

Publisher: Springer International Publishing

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

A novel nonlinear system identification approach is presented based on the coupling of a neuro-fuzzy model (NFM) with a multilayer perceptron (MLP) neural network. Therefore, the recurrent NFM is employed for multi-step ahead predictions, whereas the MLP is subsequently used to perform a nonlinear quasi-static correction of the obtained time-series output. In the present work, the proposed method is applied as a reduced-order modeling (ROM) technique to lower the effort of unsteady motion-induced computational fluid dynamics (CFD) simulations, although it could be utilized generally for any nonlinear system identification task. For demonstration purposes, the NLR 7301 airfoil is investigated at transonic flow conditions, while the pitch and plunge degrees of freedom are simultaneously excited. In addition, the sequential model training process as well as the model application is presented. It is shown that the essential aerodynamic characteristics are accurately reproduced by the novel ROM in comparison to the full-order CFD reference solution. Moreover, by examining the results of the NFM without MLP correction it is indicated that the new approach leads to an increased fidelity regarding nonlinear ROM-based simulations.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Literature
1.
go back to reference Dowell, E.H., Hall, K.C.: Modeling of fluid-structure interaction. Annu. Rev. Fluid Mech. 33, 445–490 (2001)CrossRefMATH Dowell, E.H., Hall, K.C.: Modeling of fluid-structure interaction. Annu. Rev. Fluid Mech. 33, 445–490 (2001)CrossRefMATH
2.
go back to reference Faller, W.E., Schreck, S.J., Luttges, M.W.: Neural network prediction and control of three-dimensional unsteady separated flowfields. J. Aircr. 32(6), 1213–1220 (1995)CrossRef Faller, W.E., Schreck, S.J., Luttges, M.W.: Neural network prediction and control of three-dimensional unsteady separated flowfields. J. Aircr. 32(6), 1213–1220 (1995)CrossRef
3.
go back to reference Fleischer, D., Breitsamter, C.: Efficient computation of unsteady aerodynamic loads using computational-fluid-dynamics linearized methods. J. Aircr. 50(2), 425–440 (2013)CrossRef Fleischer, D., Breitsamter, C.: Efficient computation of unsteady aerodynamic loads using computational-fluid-dynamics linearized methods. J. Aircr. 50(2), 425–440 (2013)CrossRef
4.
go back to reference Glaz, B., Liu, L., Friedmann, P.P.: Reduced-order nonlinear unsteady aerodynamic modeling using a surrogate-based recurrence framework. AIAA J. 48(10), 2418–2429 (2010)CrossRef Glaz, B., Liu, L., Friedmann, P.P.: Reduced-order nonlinear unsteady aerodynamic modeling using a surrogate-based recurrence framework. AIAA J. 48(10), 2418–2429 (2010)CrossRef
5.
go back to reference Haykin, S.: Neural Networks—A Comprehensive Foundation, 2nd edn. Prentice Hall, Upper Saddle River (1998)MATH Haykin, S.: Neural Networks—A Comprehensive Foundation, 2nd edn. Prentice Hall, Upper Saddle River (1998)MATH
6.
go back to reference Kou, J., Zhang, W., Yin, M.: Novel Wiener models with a time-delayed nonlinear block and their identification. Nonlinear Dyn. 85(4), 2389–2404 (2016)CrossRef Kou, J., Zhang, W., Yin, M.: Novel Wiener models with a time-delayed nonlinear block and their identification. Nonlinear Dyn. 85(4), 2389–2404 (2016)CrossRef
7.
go back to reference Kreiselmaier, E., Laschka, B.: Small disturbance Euler equations: efficient and accurate tool for unsteady load predictions. J. Aircr. 37(5), 770–778 (2000)CrossRef Kreiselmaier, E., Laschka, B.: Small disturbance Euler equations: efficient and accurate tool for unsteady load predictions. J. Aircr. 37(5), 770–778 (2000)CrossRef
8.
go back to reference Ljung, L.: System Identification: Theory for the User. Prentice Hall, Upper Saddle River (1999)CrossRefMATH Ljung, L.: System Identification: Theory for the User. Prentice Hall, Upper Saddle River (1999)CrossRefMATH
9.
go back to reference Lucia, D.J., Beran, P.S., Silva, W.A.: Reduced-order modeling: new approaches for computational physics. Prog. Aerosp. Sci. 40, 51–117 (2004)CrossRef Lucia, D.J., Beran, P.S., Silva, W.A.: Reduced-order modeling: new approaches for computational physics. Prog. Aerosp. Sci. 40, 51–117 (2004)CrossRef
10.
go back to reference MATLAB, Software Package, Ver. 8.5, The MathWorks, Natick, MA (2015) MATLAB, Software Package, Ver. 8.5, The MathWorks, Natick, MA (2015)
11.
go back to reference Nelles, O.: Nonlinear System Identification—From Classical Approaches to Neural Networks and Fuzzy Models. Springer, Berlin (2001)MATH Nelles, O.: Nonlinear System Identification—From Classical Approaches to Neural Networks and Fuzzy Models. Springer, Berlin (2001)MATH
12.
go back to reference Silva, W.A., Bartels, R.E.: Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 code. J. Fluids Struct. 19, 729–745 (2004)CrossRef Silva, W.A., Bartels, R.E.: Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 code. J. Fluids Struct. 19, 729–745 (2004)CrossRef
13.
go back to reference Tang, L., Bartels, R.E., Chen, P.-C., Liu, D.D.: Numerical investigation of transonic limit cycle oscillations of a two-dimensional supercritical wing. J. Fluids Struct. 17, 29–41 (2003)CrossRef Tang, L., Bartels, R.E., Chen, P.-C., Liu, D.D.: Numerical investigation of transonic limit cycle oscillations of a two-dimensional supercritical wing. J. Fluids Struct. 17, 29–41 (2003)CrossRef
14.
go back to reference Winter, M., Breitsamter, C.: Neurofuzzy-model-based unsteady aerodynamic computations across varying freestream conditions. AIAA J. 54(9), 2705–2720 (2016)CrossRef Winter, M., Breitsamter, C.: Neurofuzzy-model-based unsteady aerodynamic computations across varying freestream conditions. AIAA J. 54(9), 2705–2720 (2016)CrossRef
15.
go back to reference Winter, M., Breitsamter, C.: Efficient unsteady aerodynamic loads prediction based on nonlinear system identification and proper orthogonal decomposition. J. Fluids Struct. 67, 1–21 (2016)CrossRef Winter, M., Breitsamter, C.: Efficient unsteady aerodynamic loads prediction based on nonlinear system identification and proper orthogonal decomposition. J. Fluids Struct. 67, 1–21 (2016)CrossRef
16.
go back to reference Wright, J.R., Cooper, J.E.: Introduction to Aircraft Aeroelasticity and Loads. Wiley, West Sussex (2007)CrossRef Wright, J.R., Cooper, J.E.: Introduction to Aircraft Aeroelasticity and Loads. Wiley, West Sussex (2007)CrossRef
17.
go back to reference Zhang, W., Wang, B., Ye, Z., Quan, J.: Efficient method for limit cycle flutter analysis by nonlinear aerodynamic reduced-order models. AIAA J. 50(5), 1019–1028 (2012)CrossRef Zhang, W., Wang, B., Ye, Z., Quan, J.: Efficient method for limit cycle flutter analysis by nonlinear aerodynamic reduced-order models. AIAA J. 50(5), 1019–1028 (2012)CrossRef
18.
go back to reference Zwaan, R.J.: Summary of Data Required for the AGARD SMP Activity ‘Standard Aeroelastic Configurations’—Two-Dimensional Configurations, MP 79015 U, NLR (1979) Zwaan, R.J.: Summary of Data Required for the AGARD SMP Activity ‘Standard Aeroelastic Configurations’—Two-Dimensional Configurations, MP 79015 U, NLR (1979)
Metadata
Title
Coupling of Recurrent and Static Neural Network Approaches for Improved Multi-step Ahead Time Series Prediction
Authors
Maximilian Winter
Christian Breitsamter
Copyright Year
2018
DOI
https://doi.org/10.1007/978-3-319-64519-3_39

Premium Partners