A method for executing yaw control of an aircraft including two rotors is provided. The method includes inducing helicopter yaw by creating a differential torque between the two rotors, wherein the creating of the differential torque comprises inducing a differential collective pitch to generate a differential thrust, and maintaining helicopter roll equilibrium during the inducing of the helicopter yaw by inducing a differential cyclic pitch to generate a differential lift offset.
HIGH-AUTHORITY YAW CONTROL FOR A TANDEM VEHICLE WITH RIGID ROTORS
HOCHAUTORITÄRE GIERSTEUERUNG FÜR EIN TANDEMFAHRZEUG MIT STARRER ROTOREN
COMMANDE DE LACET À AUTORITÉ ÉLEVÉE POUR VÉHICULE TANDEM DOTÉ DE ROTORS RIGIDES
2018-07-18
Patent
Elektronische Ressource
Englisch
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