International Journal of Control, Automation and Systems 2010; 8(4): 727-734
Published online August 3, 2010
https://doi.org/10.1007/s12555-010-0403-5
© The International Journal of Control, Automation, and Systems
Neural Network (NN) models based on autoregressive structures have long been used for nonlinear system identification problems. Their application for on-line implementations, however require them to be trained within a prescribed time span, which is often related to the sampling time of the system. In this paper, we introduce a NN model that is embedded with a dimensionality reduction mechanism in order to reduce the size of the network. The dimensionality reduction is based on Principal Component Analysis (PCA) and the resulting smaller NN trains faster. The longitudinal and lateral dynamics of a rotary wing Unmanned Aerial Vehicle (UAV) is modelled using flight test data. The re-sults of system identification, error statistics and training times are provided to highlight the benefits of the proposed approach for NN based system identification models.
Keywords Dynamic modelling, neural network, principal component analysis, rotary wing UAV, system identification.
International Journal of Control, Automation and Systems 2010; 8(4): 727-734
Published online August 1, 2010 https://doi.org/10.1007/s12555-010-0403-5
Copyright © The International Journal of Control, Automation, and Systems.
Mahendra Kumar Samal, Sreenatha Anavatti, Tapabrata Ray, and Matthew Garratt
University of New South Wales, Australia
Neural Network (NN) models based on autoregressive structures have long been used for nonlinear system identification problems. Their application for on-line implementations, however require them to be trained within a prescribed time span, which is often related to the sampling time of the system. In this paper, we introduce a NN model that is embedded with a dimensionality reduction mechanism in order to reduce the size of the network. The dimensionality reduction is based on Principal Component Analysis (PCA) and the resulting smaller NN trains faster. The longitudinal and lateral dynamics of a rotary wing Unmanned Aerial Vehicle (UAV) is modelled using flight test data. The re-sults of system identification, error statistics and training times are provided to highlight the benefits of the proposed approach for NN based system identification models.
Keywords: Dynamic modelling, neural network, principal component analysis, rotary wing UAV, system identification.
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