The method involves transforming an acceleration setpoint by predetermined relationships into a required longitudinal attitude setpoint that is transmitted to an automatic system (26). The acceleration setpoint is transmitted into a required load factor setpoint in a longitudinal direction of an aircraft (1) parallel to a roll axis of the aircraft, where the load factor setpoint is transmitted to another automatic system (25) for maintaining the load point by controlling a collective pitch of a set of blades (2') of a propulsion unit to comply with the former setpoint. An independent claim is also included for a device for assisting piloting of a rotary wing aircraft i.e. hybrid aircraft.
Procédé de pilotage assisté d'un aéronef à voilure tournante comprenant au moins une hélice propulsive, dispositif de pilotage assisté et aéronef
Method for assisted piloting of a rotary wing aircraft comprising at least one screw propeller, assisted piloting device and aircraft
Hilfssteuerungsverfahren eines Drehflügelflugzeugs, das mindestens eine Druckschraube umfasst, Hilfssteuerungsvorrichtung und Luftfahrzeug
2017-10-18
Patent
Electronic Resource
French
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