In recent years, aircraft accidents have especially increased on concorde aircrafts. Due to the aircrafts going out of control, many people have lost their lives. Neural network controllers can be accepted as an alternative to control this kind of plane. In this study, a neural network control system was employed to control the nose angle of supersonic concorde aircrafts. The designed model reference adaptive neural controller is a feedforward multilayered perceptron structure. Backpropagation algorithm was utilized to update weights of the neural controller. For comparison, standard proportional-integral-derivate control system was also used with empirically selected gain parameters. Consequently, between the two approaches, the neural networks have a superior performance in the control of such aircrafts.


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    Title :

    Design of neural controller system for concorde aircrafts


    Contributors:
    Yildirim, S. (author) / Erkaya, S. (author) / Uzmay, I. (author)

    Published in:

    Publication date :

    2004


    Size :

    10 Seiten, 14 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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