The invention relates to a device and to a method for the open and closed control of n actuators An, n=1, 2, . . . , N, where N≥1, which drive aerodynamic control surfaces of an aircraft. The proposed device includes a first interface at which, by manually inputting of a pilot into an input means, predefinitions SVPilot for controlling the actuators An are generated and made available and/or a second interface at which, by means of an automatic flight controller of the aircraft, predefinitions SVAutoPilot for controlling the actuators An are generated and made available, a unit, which on the basis of predefinitions SVPilot and/or SVAutoPilot per actuator An, determines a reference variable FAn,setpoint, for controlling the actuator An, wherein the reference variable FAn,setpoint specifies a setpoint force or a setpoint torque, and per actuator An a force/torque controller REGn for performing closed control of the actuator An on the basis of the assigned reference variable FAn,setpoint and a force/torque FAn generated by the actuator An as a closed-control variable which is determined by a sensor device S1n, which is respectively present at or in the actuator An or in the drivetrain of the respective actuator An.


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    Title :

    STEUERUNG UND REGELUNG VON AKTOREN, DIE AERODYNAMISCHE STEUERFLÄCHEN EINES LUFTFAHRZEUGS ANTREIBEN


    Additional title:

    OPEN AND CLOSED CONTROL OF ACTUATORS WHICH DRIVE AERODYNAMIC CONTROL SURFACES OF AN AIRCRAFT
    COMMANDE ET RÉGULATION D'ACTIONNEURS QUI ENTRAÎNENT DES GOUVERNES AÉRODYNAMIQUES D'UN AÉRONEF


    Contributors:

    Publication date :

    2022-01-05


    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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