A method for optimizing the operation of at least one first propeller and of at least one second propeller of a hybrid helicopter. The method comprises the following step during a control phase: deflection, with an autopilot system, of at least one aerodynamic stabilizer member into a setpoint position having, with respect to a reference position, a target deflection angle that is a function of a setpoint deflection angle, the setpoint deflection angle being calculated by the autopilot system in order to compensate for a torque exerted by the lift rotor at zero sideslip.
PROCÉDÉ DE COMMANDE D'AU MOINS UN ORGANE AÉRODYNAMIQUE DE DÉRIVE D'UN HÉLICOPTÈRE HYBRIDE ET UN HÉLICOPTÈRE HYBRIDE
METHOD FOR CONTROLLING AT LEAST ONE AERODYNAMIC RUDDER OF A HYBRID HELICOPTER AND HYBRID HELICOPTER
VERFAHREN ZUR STEUERUNG MINDESTENS EINES AERODYNAMISCHEN SEITENRUDERS EINES HYBRIDHUBSCHRAUBERS UND ENTSPRECHENDER HYBRIDHUBSCHRAUBER
2025-05-07
Patent
Electronic Resource
French
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