TY - GEN
T1 - Coupling of recurrent and static neural network approaches for improved multi-step ahead time series prediction
AU - Winter, Maximilian
AU - Breitsamter, Christian
N1 - Publisher Copyright:
© Springer International Publishing AG 2018.
PY - 2018
Y1 - 2018
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=85033444308&partnerID=8YFLogxK
U2 - 10.1007/978-3-319-64519-3_39
DO - 10.1007/978-3-319-64519-3_39
M3 - Conference contribution
AN - SCOPUS:85033444308
SN - 9783319645186
T3 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
SP - 433
EP - 442
BT - New Results in Numerical and Experimental Fluid Mechanics XI - Contributions to the 20th STAB/DGLR Symposium
A2 - Dillmann, Andreas
A2 - Wagner, Claus
A2 - Heller, Gerd
A2 - Kramer, Ewald
A2 - Bansmer, Stephan
A2 - Radespiel, Rolf
A2 - Semaan, Richard
PB - Springer Verlag
T2 - 20th STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics, 2016
Y2 - 8 November 2016 through 9 November 2016
ER -