TY - GEN
T1 - Enhanced Speed Control of Aviation PMSM Drives by a Proportional Resonant-Based ADRC With Adaptive Frequency Identification
AU - Li, Jincheng
AU - Chen, Peiyang
AU - Zhao, Xiaopeng
AU - Zhang, Mengbo
AU - Luo, Guangzhao
AU - Chen, Zhe
N1 - Publisher Copyright:
© 2023 IEEE.
PY - 2023
Y1 - 2023
N2 - The accurate speed control is significant for PMSM in aircraft flap-slat elctromechanical actuator, which serves as the key motion unit of aircraft high-lift system. However, the speed controller suffers from internal and external periodical disturbances due to current sampling and scaling errors and aerodynamic load. The periodical disturbance estimation in extended state observer is done by a proportional resonant scheme to enhance the disturbance rejection ability of speed control loop [1]. This paper proposes an adaptive sinusoidal frequency observer(ASFO)to expand the applicability of proportional resonant-based active disturbance rejection control(PRADRC) technique to applications where periodic and aperiodic disturbances exist. The resonant frequency is adaptively estimated through the ASFO whose input is the speed tracking error. The performance analysis of proposed method is proved theoretically and then validated by experiments.
AB - The accurate speed control is significant for PMSM in aircraft flap-slat elctromechanical actuator, which serves as the key motion unit of aircraft high-lift system. However, the speed controller suffers from internal and external periodical disturbances due to current sampling and scaling errors and aerodynamic load. The periodical disturbance estimation in extended state observer is done by a proportional resonant scheme to enhance the disturbance rejection ability of speed control loop [1]. This paper proposes an adaptive sinusoidal frequency observer(ASFO)to expand the applicability of proportional resonant-based active disturbance rejection control(PRADRC) technique to applications where periodic and aperiodic disturbances exist. The resonant frequency is adaptively estimated through the ASFO whose input is the speed tracking error. The performance analysis of proposed method is proved theoretically and then validated by experiments.
KW - Active Disturbance Rejection Control(ADRC)
KW - Adaptive Sinusoidal Frequency Observer
KW - Electro-Mechanical Actuator
KW - Proportional Resonant
UR - https://www.scopus.com/pages/publications/85179513300
U2 - 10.1109/IECON51785.2023.10312486
DO - 10.1109/IECON51785.2023.10312486
M3 - 会议稿件
AN - SCOPUS:85179513300
T3 - IECON Proceedings (Industrial Electronics Conference)
BT - IECON 2023 - 49th Annual Conference of the IEEE Industrial Electronics Society
PB - IEEE Computer Society
T2 - 49th Annual Conference of the IEEE Industrial Electronics Society, IECON 2023
Y2 - 16 October 2023 through 19 October 2023
ER -