This paper presents an application of dynamic inversion control with adaptive neural networks to a tailless fighter aircraft. We propose an extension of the dynamic inversion control using proportional-integral desired dynamics. The performance of the PI adaptive dynamic inversion controller is compared to an adaptive dynamic inversion controller using PD desired dynamics. The controller was tested in a 6-DOF simulation of the ICE tailless fighter aircraft. Simulation results are given for simultaneous longitudinal and lateral manoeuvres performed under nominal conditions and also with the simulated failure of a major control surface. The PI dynamic inversion controller with neural network adaptation outperforms both the baseline PI controller without adaptation and also a PD dynamic inversion controller with neural network adaptation.


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    Titel :

    PI control of a tailless fighter aircraft with dynamic inversion and neural networks


    Beteiligte:
    Schumacher, C. (Autor:in) / Johnson, J.D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1999


    Format / Umfang :

    5 Seiten, 15 Quellen




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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