Methods and apparatus for monitoring and detecting failures in the actuation of a control system, such as a flight control system for an aircraft, include defining a nominal model of the control system in terms of the state variables of the control system, defining a model of an asymmetric "actuation monitoring envelope" that dynamically bounds a range that measured state variables of the system are allowed to take during operation of the system as a function of the nominal system state model, monitoring a signal corresponding to a state variable of the system during operation thereof, and detecting a failure in the actuation of the control system when the monitored signal exceeds the bounds of the monitoring envelope.


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    Titel :

    CONTROL SYSTEM ACTUATION FAULT MONITORING


    Weitere Titelangaben:

    CONTROLE DES DEFAILLANCES DE DECLENCHEMENT D'UN SYSTEME DE COMMANDE


    Beteiligte:
    MOSSMAN DAVID C (Autor:in) / ENNS RUSSELL J (Autor:in) / DAHMAN JONATHAN B (Autor:in)

    Erscheinungsdatum :

    01.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64C AEROPLANES , Flugzeuge



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