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.


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    Title :

    PROCEDE DE PILOTAGE ASSISTE D'UN AERONEF A VOILURE TOURNANTE COMPRENANT AU MOINS UNE HELICE PROPULSIVE, DISPOSITIF DE PILOTAGE ASSISTE ET AERONEF


    Additional title:

    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


    Contributors:

    Publication date :

    2018-06-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge