According to one aspect, a method of initial rotor state compensation for a rotorcraft includes determining a vehicle attitude of the rotorcraft prior to takeoff of the rotorcraft. A rotor state compensation is computed based on the vehicle attitude. A plurality of rotor servos is commanded to an initial rotor state based on a nominal rotor neutral position value in combination with the rotor state compensation to establish a predetermined takeoff trajectory of the rotorcraft.

    Selon un aspect de l'invention, un procédé de compensation d'état initial de rotor pour un giravion comprend la détermination de l'assiette du giravion avant son décollage. Une compensation d'état de rotor est calculée sur la base de l'assiette. Une pluralité de servocommandes de rotor est commandée pour parvenir à un état initial de rotor selon une valeur de position neutre nominale de rotor en association avec la compensation d'état de rotor, afin d'établir une trajectoire de décollage du giravion prédéfinie.


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    Title :

    INITIAL ROTOR STATE COMPENSATION FOR A ROTORCRAFT


    Additional title:

    COMPENSATION D'ÉTAT INITIAL DE ROTOR POUR UN GIRAVION


    Contributors:

    Publication date :

    2016-03-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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