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The Development of Neural Network Based System Identification ...

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140 CHAPTER 5 NN BASED SYSTEM IDENTIFICATION: RESULTS AND DISCUSSION<br />

Table 5.7<br />

<strong>The</strong> modified Elman network parameters.<br />

Elman <strong>Network</strong> Specifications for Attitude Dynamics<br />

Number <strong>of</strong> past outputs 1<br />

Number <strong>of</strong> past inputs 1<br />

Number <strong>of</strong> neurons 4<br />

Activation function at hidden layer<br />

Tanh<br />

Activation function at output layer Linear<br />

Number <strong>of</strong> regressors 4<br />

Total number <strong>of</strong> weights 34<br />

Weight decay 0.0001<br />

Self connection strength α 0.5<br />

10 3 Hidden Neurons Size<br />

10 2<br />

RMSE (%)<br />

10 1<br />

10 0<br />

1 2 3 4 5 6 7 8 9 10<br />

Figure 5.15 <strong>The</strong> validation RMSE comparison for different hidden neuron sizes. <strong>The</strong> k-cross validation<br />

process was conducted for modified Elman network with network structure <strong>of</strong> 4 regressors (n y = 1 and<br />

n u = 1). <strong>The</strong> neural network training was carried out using the <strong>of</strong>f-line Levenberg-Marquardt (LM)<br />

algorithm.<br />

estimated from the <strong>of</strong>f-line trained modified Elman network is shown in Figure 5.16 and<br />

Figure 5.17. <strong>The</strong> <strong>of</strong>f-line LM training is carried out using training data set from 16 s<br />

to 28 s, and the prediction performance is validated on roll rate and pitch rate data<br />

(test data) from 36 s to 37 s. <strong>The</strong> network is trained using the nearly optimal structure<br />

from Table 5.7. <strong>The</strong>se predicted responses from modified Elman network are overlaid<br />

with the measured helicopter responses from the test data set. <strong>The</strong> results indicate<br />

that one-step ahead modified Elman network prediction overlap the test data almost

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