公开(公告)号：US20240166333A1

公开(公告)日：2024-05-23

申请号：US18511423

申请日：2023-11-16

Applicant: KOREA AEROSPACE RESEARCH INSTITUTE

Inventor： Youngshin KANG ,  Am CHO ,  Seongwook CHOI ,  Yushin KIM ,  Jongmin BAE ,  Junho CHO ,  Haneul YUN ,  Myeong Kyu LEE

IPC: B64C11/30 ,  B64C13/50 ,  B64D35/04

CPC classification number: B64C11/305 ,  B64C13/503 ,  B64D35/04 ,  B64C27/52

Abstract: 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.