An apparatus for controlling a tilt rotor is provided. The apparatus includes a thrust command generator (100) configured to generate a first collective pitch angle based on a throttle command, a rotation speed compensator (200) configured to generate a compensation value based on a target rotation speed and a current rotation speed of the motor, a compensation weight generator (300) configured to generate weight values according to a flight speed, a collective pitch angle command generator (400) configured to generate a collective pitch angle adjustment command of the rotor blade of the motor, based on a first compensation value and the first collective pitch angle, the first compensation value being obtained by multiplying the compensation value by a preset conversion ratio and a first weight value, and a motor controller (500) configured to generate a motor control command based on a second compensation value being obtained by multiplying the compensation value by a second weight value and the first collective pitch angle.


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    Title :

    METHOD AND APPARATUS FOR CONTROLLING TILT ROTOR, AND AIRCRAFT INCLUDING THE APPARATUS


    Additional title:

    VERFAHREN UND VORRICHTUNG ZUR STEUERUNG EINES KIPPROTORS UND FLUGZEUG MIT DER VORRICHTUNG
    PROCÉDÉ ET APPAREIL DE COMMANDE DE ROTOR BASCULANT, ET AÉRONEF COMPRENANT L'APPAREIL


    Contributors:
    KANG YOUNGSHIN (author) / CHO AM (author) / CHOI SEONGWOOK (author) / KIM YUSHIN (author) / BAE JONGMIN (author) / CHO JUNHO (author) / YUN HANEUL (author) / LEE MYEONG KYU (author)

    Publication date :

    2024-05-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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