Korea Aerospace Research Institute

Haneul Yun

Seongwook Choi

Youngshin Kang

Myeong Kyu Lee

Am Cho

Yushin Kim

Junho Cho

Jongmin Bae

An apparatus for controlling a tilt rotor is provided. The apparatus includes a thrust command generator configured to generate a first collective pitch angle based on a throttle command, a rotation speed compensator configured to generate a compensation value based on a rotation speed of the motor, a compensation weight generator configured to generate weight values according to a flight speed, a collective pitch angle command generator configured to generate a collective pitch angle adjustment command of the rotor blade of the motor, based on the first collective pitch angle and a first compensation value being obtained by multiplying the compensation value by a preset conversion ratio and a first weight value, and a motor controller 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 of controlling tilt rotor, apparatus for controlling tilt rotor, and aircraft including the apparatus

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Daejeon, South Korea

Haneul Yun