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

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New Results in Numerical and Experimental Fluid Mechanics XI

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.

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References

  1. Dowell, E.H., Hall, K.C.: Modeling of fluid-structure interaction. Annu. Rev. Fluid Mech. 33, 445–490 (2001)

    Article  MATH  Google Scholar 

  2. 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)

    Article  Google Scholar 

  3. Fleischer, D., Breitsamter, C.: Efficient computation of unsteady aerodynamic loads using computational-fluid-dynamics linearized methods. J. Aircr. 50(2), 425–440 (2013)

    Article  Google Scholar 

  4. 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)

    Article  Google Scholar 

  5. Haykin, S.: Neural Networks—A Comprehensive Foundation, 2nd edn. Prentice Hall, Upper Saddle River (1998)

    MATH  Google Scholar 

  6. 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)

    Article  Google Scholar 

  7. Kreiselmaier, E., Laschka, B.: Small disturbance Euler equations: efficient and accurate tool for unsteady load predictions. J. Aircr. 37(5), 770–778 (2000)

    Article  Google Scholar 

  8. Ljung, L.: System Identification: Theory for the User. Prentice Hall, Upper Saddle River (1999)

    Book  MATH  Google Scholar 

  9. Lucia, D.J., Beran, P.S., Silva, W.A.: Reduced-order modeling: new approaches for computational physics. Prog. Aerosp. Sci. 40, 51–117 (2004)

    Article  Google Scholar 

  10. MATLAB, Software Package, Ver. 8.5, The MathWorks, Natick, MA (2015)

    Google Scholar 

  11. Nelles, O.: Nonlinear System Identification—From Classical Approaches to Neural Networks and Fuzzy Models. Springer, Berlin (2001)

    MATH  Google Scholar 

  12. 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)

    Article  Google Scholar 

  13. 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)

    Article  Google Scholar 

  14. Winter, M., Breitsamter, C.: Neurofuzzy-model-based unsteady aerodynamic computations across varying freestream conditions. AIAA J. 54(9), 2705–2720 (2016)

    Article  Google Scholar 

  15. 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)

    Article  Google Scholar 

  16. Wright, J.R., Cooper, J.E.: Introduction to Aircraft Aeroelasticity and Loads. Wiley, West Sussex (2007)

    Book  Google Scholar 

  17. 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)

    Article  Google Scholar 

  18. Zwaan, R.J.: Summary of Data Required for the AGARD SMP Activity ‘Standard Aeroelastic Configurations’—Two-Dimensional Configurations, MP 79015 U, NLR (1979)

    Google Scholar 

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Acknowledgements

The authors would like to thank the Bavarian Research Foundation (Bayerische Forschungsstiftung) for the funding of the project ROM-Aer (AZ 1050-12).

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Correspondence to Maximilian Winter .

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Winter, M., Breitsamter, C. (2018). Coupling of Recurrent and Static Neural Network Approaches for Improved Multi-step Ahead Time Series Prediction. In: Dillmann, A., et al. New Results in Numerical and Experimental Fluid Mechanics XI. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 136. Springer, Cham. https://doi.org/10.1007/978-3-319-64519-3_39

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  • DOI: https://doi.org/10.1007/978-3-319-64519-3_39

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