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 OF ASSISTED PILOTING OF A ROTARY WING AIRCRAFT HAVING AT LEAST ONE PROPULSION PROPELLER, AN ASSISTED PILOTING DEVICE, AND AN AIRCRAFT
HILFSSTEUERUNGSVERFAHREN EINES DREHFLÜGELFLUGZEUGS, DAS MINDESTENS EINE DRUCKSCHRAUBE UMFASST, HILFSSTEUERUNGSVORRICHTUNG UND LUFTFAHRZEUG
12.12.2018
Patent
Elektronische Ressource
Französisch
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