首页 | 本学科首页   官方微博 | 高级检索  
     

三相电压型脉宽调制整流器定频模型预测控制
引用本文:王涛,吴黎明,张晓. 三相电压型脉宽调制整流器定频模型预测控制[J]. 航空动力学报, 2017, 44(5): 17-21, 45
作者姓名:王涛  吴黎明  张晓
作者单位:中国矿业大学 信息与电气工程学院,江苏 徐州221008,中国矿业大学 信息与电气工程学院,江苏 徐州221008,中国矿业大学 信息与电气工程学院,江苏 徐州221008
基金项目:国家自然科学基金项目(51407183)
摘    要:针对三相电压型脉宽调制(PWM)整流器有限控制集模型预测控制采样频率高、开关频率不固定的缺点,提出了一种定频模型预测控制方法。通过求解价值函数得到PWM整流器交流侧下一采样时刻所要输出的电压值,利用空间矢量脉宽调制技术输出计算得到的电压值,实现定频模型预测控制。仿真与试验结果表明:所提出的控制算法开关频率恒定,稳态电流谐波含量低,实现了整流器高功率因数运行。

关 键 词:脉宽调制整流器   定频   预测控制   空间矢量

Constant Switching Frequency Model Predictive Control of ThreePhaseVoltage Type Pulse Width Modulation Rectifier
WANG Tao,WU Liming and ZHANG Xiao. Constant Switching Frequency Model Predictive Control of ThreePhaseVoltage Type Pulse Width Modulation Rectifier[J]. Journal of Aerospace Power, 2017, 44(5): 17-21, 45
Authors:WANG Tao  WU Liming  ZHANG Xiao
Affiliation:School of Information and Electrical Engineering, China University of Mining and Technology,Xuzhou 221008, China,School of Information and Electrical Engineering, China University of Mining and Technology,Xuzhou 221008, China and School of Information and Electrical Engineering, China University of Mining and Technology,Xuzhou 221008, China
Abstract:To solve the problem of high sampling rate and uncertain switching frequency in finitecontrolset, odel predictive control (FCSMPC) of threephase voltage type pulse width modulation (PWM) rectifier, a kind of constant switching frequency method was proposed. The voltage of AC side of rectifier which would be effected in the next sampling period was obtained by solving cost function, then the voltage would be produced by using space vector pulse width modulation method to achieve constant switching frequency. Simulation and experimental results showed that the proposed control algorithm had constant switching frequency, low harmonic content and the rectifier operates with high power factor.
Keywords:pulse width modulation rectifier   constant switching frequency   model predictive control (MPC)   space vector
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号