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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    Title :

    Fault Detection in Flight Guidance Dynamics Based on Differential Flatness


    Contributors:


    Publication date :

    2006-10-01


    Size :

    345734 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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