In this paper, flight guidance dynamics are shown to be implicit differentially flat with respect to the inertial position of an aircraft. This proves the existence of a set of relations between these flat outputs and the state variables representative of flight guidance dynamics and between these flat outputs and the basic inputs to flight guidance dynamics. A neural network is introduced to obtain, from the actual trajectory, nominal flight parameters which can be compared with actual values to detect abnormal behaviour.


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    Titel :

    Fault Detection in Flight Guidance Dynamics Based on Differential Flatness


    Beteiligte:
    Fellouah, Rabbah (Autor:in) / Lu, Wen (Autor:in) / Doncescu, Andrei (Autor:in) / Mora-Camino, F. (Autor:in)


    Erscheinungsdatum :

    01.10.2006


    Format / Umfang :

    345734 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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