A modification of the model reference approach, using numerical optimization is proposed for the estimation of external forces applied to control surfaces of an aircraft. This estimation provides the basis for the feedforward control of the surface position. Incorporated into the control system of a flight control actuator, this technique allows a significant enhancement of the actuator stiffness.<>


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    Title :

    Stiffness enhancement of flight control actuator


    Contributors:


    Publication date :

    1993-04-01


    Size :

    878786 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Stiffness Enhancement of Flight Control Actuator

    Blaignan, V.B. | Online Contents | 1993


    Stiffness enhancement of flight control actuator

    Blaignan, V.B. / Skormin, V.A. | Tema Archive | 1993


    FLIGHT CONTROL ACTUATOR

    POTIER KARL / DAVIS JENNIFER / MEDINA RAPHAEL et al. | European Patent Office | 2023

    Free access

    FLIGHT CONTROL ACTUATOR

    POTIER KARL / DAVIS JENNIFER / MEDINA RAPHAEL et al. | European Patent Office | 2023

    Free access