A method for controlling an engine, a device for controlling an engine and an aircraft, the method comprising the steps of determining a first intensity Kp, representing a stiffness, according to a physical stiffness Kss of the mechanical connection and a stiffness setpoint Kpspec to be rendered on the control column, a second intensity Kv, representing a damping, according to a physical damping fss between the control column and the engine and a damping setpoint Kvspec to be rendered on the control column, and a third intensity Ka, representing an inertia, according to a physical inertia Jss of the control column and an inertia setpoint Kaspec to be rendered on the control column.
PROCÉDÉ DE COMMANDE D'UN MOTEUR D'UNE COMMANDE D'UN AÉRONEF, DISPOSITIF DE COMMANDE ET AÉRONEF
METHOD FOR CONTROLLING AN AIRCRAFT CONTROL ENGINE, CONTROL DEVICE AND AIRCRAFT
VERFAHREN ZUR STEUERUNG EINES FLUGZEUGSTEUERUNGSMOTORS, STEUERUNGSVORRICHTUNG UND FLUGZEUG
2023-10-11
Patent
Elektronische Ressource
Französisch
PROCÉDÉ DE COMMANDE D'UN MOTEUR D'UNE COMMANDE D'UN AÉRONEF, DISPOSITIF DE COMMANDE ET AÉRONEF
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