Methods and devices for detecting oscillatory faults in a positional servocontrol arrangement for an aircraft control surface are provided. The detection device estimates a reference position of the control surface and, with the aid of a model in which at each iteration a residual value of the previous iteration, multiplied by a dynamic gain, is injected, detects an oscillatory fault with the aid of this reference position.


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    Titel :

    Method and device for detecting oscillatory failures in a position servocontrol subsystem of an aircraft control surface


    Beteiligte:
    GOUPIL PHILIPPE (Autor:in) / BABANDO OLIVIER (Autor:in) / SIFI MOHCINE (Autor:in) / LAVIGNE LOÏC (Autor:in) / CAZAURANG FRANCK (Autor:in)

    Erscheinungsdatum :

    2015-12-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL



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