A High-Frequency GaN-Based Motor Drive for Aircraft Electromechanical Actuators

被引:0
作者
Luo, Bin [1 ]
Luo, Guangzhao [1 ]
Li, Sihai [1 ]
An, Zezou [1 ]
Shen, Hongming [1 ]
Sun, Jian [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Sch Automat, Xian 710072, Peoples R China
[2] GanSu Key Lab Aeronaut Electromech Actuator, Lanzhou, Peoples R China
关键词
Damping; Logic gates; Oscillators; Motor drives; Motors; Aircraft; Crosstalk; Driver circuits; motor drives; RC snubber; ELECTRIC AIRCRAFT;
D O I
10.1109/TIE.2024.3413809
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
To achieve superior dynamic response performance for aircraft electromechanical actuators (EMAs), high speed, low inductance, or multipole permanent magnet synchronous motors (PMSMs) prove to be ideal candidates. This necessitates a high-switching frequency for the motor drives. Cascode gallium nitride (GaN) devices present themselves as highly appealing for this specific application due to their high-switching frequency, low losses, and ability to operate at high temperatures. However, due to the intricate device structure and the high rates of change of voltage (dv/dt) and current (di/dt), GaN-based motor drives are more susceptible to oscillations, leading to electromagnetic interference (EMI) issues. This article presents a cascode GaN-based motor drive operating at a 100-kHz switching frequency for aircraft EMAs. A mathematical model is established to elucidate the mechanisms behind the turn-on dv/dt effect and turn-off di/dt effect of the cascode GaN-based inverter, shedding light on the occurrence of oscillations. The impact of gate driver parameters on the dv/dt and di/dt effects is thoroughly examined. Furthermore, a design method for RC snubber parameters is proposed to further alleviate the turn-off di/dt effect. Finally, experimental validations are conducted to confirm the efficacy of the proposed design methods and the performance of the high-frequency GaN-based motor drive.
引用
收藏
页码:1217 / 1229
页数:13
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