A method includes determining, by a computing device comprising a processor, a value for at least one parameter related to an operation of a coaxial rotary wing aircraft; processing, by the computing device, the at least one parameter to determine control power available from one or more flight controls comprising a differential cyclic; and establishing, by the computing device, a value for the differential cyclic to create a net yaw moment for the rotary wing aircraft based on the determination of the available control power.
COAXIAL ROTOR YAW CONTROL
GIERSTEUERUNG FÜR EINEN KOAXIALROTOR
COMMANDE DE LACET DE ROTOR COAXIAL
2018-12-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |