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.
STEUERUNG UND REGELUNG VON AKTOREN, DIE AERODYNAMISCHE STEUERFLÄCHEN EINES LUFTFAHRZEUGS ANTREIBEN
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
2022-01-05
Patent
Elektronische Ressource
Deutsch
Steuerung und Regelung von Aktoren, die aerodynamische Steuerflächen eines Luftfahrzeugs antreiben
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