A device for control and closed-loop control of an actuating system of an aircraft is disclosed. The device has a first input interface, which is configured to receive first input data indicating a reference variable, a second input interface, which is configured to receive second input data indicating a controlled variable, and a control output, which is configured to output a control signal. The control signal indicates a manipulated variable for an actuating system of an aircraft, which is to be controlled by means of the actuating system. The reference variable indicates a target acceleration at a point of the aircraft that is to be controlled by means of the actuating system, and the controlled variable indicates an actual acceleration of the aircraft at the point. Taking into account the reference variable and the controlled variable, the device is configured to determine the manipulated variable, in particular from the difference between the reference variable and the controlled variable, and to output the control signal corresponding to the manipulated variable via the control output. Further, an arrangement for control and closed-loop control of an actuating system of an aircraft as well as a method are provided.


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    Title :

    VORRICHTUNG, ANORDNUNG UND VERFAHREN FÜR DIE STEUERUNG UND REGELUNG EINES STELLSYSTEMS EINES FLUGZEUGS


    Additional title:

    APPARATUS, ASSEMBLY AND METHOD FOR CONTROLLING AN ACTUATING SYSTEM OF AN AIRCRAFT IN AN OPEN-LOOP AND CLOSED-LOOP MANNER
    DISPOSITIF, AGENCEMENT ET PROCÉDÉ POUR ASSURER LA COMMANDE ET LA RÉGULATION D'UN SYSTÈME DE RÉGLAGE D'UN AÉRONEF


    Contributors:

    Publication date :

    2022-09-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen




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