A control device for controlling an aircraft, the control device including at least one motor-driven trim actuator with active type anchoring, the trim actuator including at least one electric motor, at least one electronic power circuit for electrically powering the electric motor(s), and speed reduction means for driving rotation of an outlet shaft of the trim actuator. The control device implements three distinct servo-control loops that are nested in one another, these three servo-control loops being formed by an electric current servo-control loop, a speed servo-control loop, and a force servo-control loop.
DISPOSITIF DE COMMANDE D'UN AERONEF, AERONEF CORRESPONDANT ET METHODE DE PILOTAGE D'UN AERONEF
AN AIRCRAFT CONTROL DEVICE, A CORRESPONDING AIRCRAFT, AND A METHOD OF CONTROLLING AN AIRCRAFT
VORRICHTUNG ZUR STEUERUNG EINES LUFTFAHRZEUGS, ENTSPRECHENDES LUFTFAHRZEUG UND STEUERMETHODE EINES LUFTFAHRZEUGS
2019-04-10
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern |
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