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.
METHOD AND APPARATUS FOR CONTROLLING TILT ROTOR, AND AIRCRAFT INCLUDING THE APPARATUS
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
2024-05-22
Patent
Electronic Resource
English
European Patent Office | 2024
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