The invention discloses a rotor wing driving method and device. The method comprises the following steps: receiving a flight control command; acquiring the current rotation status of a first motor corresponding to a first steering engine, and the current rotation status of a second motor corresponding to a second steering engine; determining the first rotation status needed by the first motor according to the flight control command and the current status of the first motor; determining the second rotation status needed by the second motor according to the flight control command and the current status of the second motor; controlling the first motor to rotate at the corresponding second rotation status, thus realizing the torsion of a first paddle clamping body relative to a lower rotor hub; and controlling the second motor to rotate at the corresponding second rotation status, thus realizing the torsion of a second paddle clamping body relative to an upper rotor hub. Therefore, the defect that driving process of the existing rotor wing driving system is complicated by adopting the corresponding rotor wing driving method can be solved.


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    Titel :

    Rotor wing driving method and device


    Beteiligte:
    TIAN GANGYIN (Autor:in)

    Erscheinungsdatum :

    29.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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