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基于抗饱和PI控制器和占空比调制的直线游标永磁电机直接推力控制
引用本文:赵文祥,吴彬玉,陈前,邱先群,姜庆旺.基于抗饱和PI控制器和占空比调制的直线游标永磁电机直接推力控制[J].控制与决策,2018,33(1):175-180.
作者姓名:赵文祥  吴彬玉  陈前  邱先群  姜庆旺
作者单位:江苏大学电气信息工程学院,江苏镇江212013,江苏大学电气信息工程学院,江苏镇江212013,江苏大学电气信息工程学院,江苏镇江212013,江苏大学电气信息工程学院,江苏镇江212013,江苏大学电气信息工程学院,江苏镇江212013
基金项目:国家自然科学基金项目(51777090, 51277194);江苏省333工程科研基金项目(BRA2017388);江苏省高校优势学科项目(苏政办发[2014]).
摘    要:针对直线游标永磁电机控制系统存在的非线性饱和及推力脉动大等问题,提出一种基于抗饱和PI控制器及占空比调制的改进式直接推力控制方法.该控制器采用变结构的积分环节,能快速退出饱和区.在分析电压矢量对电磁推力的影响基础上,采用开关频率固定的占空比调制方式.仿真与实验结果表明,所提出的改进式直接推力控制方法能有效减小系统的超调量和推力脉动,提高系统的稳定性和鲁棒性.

关 键 词:直线电机  永磁电机  抗饱和  PI控制器  直接推力控制  占空比调制

Direct thrust force control of linear vernier PM motor based on anti-windup PI controller and duty ratio modulation
ZHAO Wen-xiang,WU Bin-yu,CHEN Qian,QIU Xian-qun and JIANG Qing-wang.Direct thrust force control of linear vernier PM motor based on anti-windup PI controller and duty ratio modulation[J].Control and Decision,2018,33(1):175-180.
Authors:ZHAO Wen-xiang  WU Bin-yu  CHEN Qian  QIU Xian-qun and JIANG Qing-wang
Affiliation:School of Electrical and Information Engineering,Jiangsu University,Zhenjiang 212013,China,School of Electrical and Information Engineering,Jiangsu University,Zhenjiang 212013,China,School of Electrical and Information Engineering,Jiangsu University,Zhenjiang 212013,China,School of Electrical and Information Engineering,Jiangsu University,Zhenjiang 212013,China and School of Electrical and Information Engineering,Jiangsu University,Zhenjiang 212013,China
Abstract:Due to the nonlinear saturation and high thrust force ripples in linear vernier permanent-magnet motor drive, an improved direct thrust force control strategy based on the anti-windup PI controller and duty ratio modulation is proposed. The variable-structure is adopted in the proposed controller, which can make the system quickly exit saturation zone. Duty ratio modulation with a constant switching frequency is adopted based on the analysis of effects that voltage vector has on thrust force ripples in the control strategy. The simulation and experimental results show that the proposed improved direct thrust force control system can effectively reduce the systemic overshoot and thrust ripples, thus improving the stability and robustness of the control system.
Keywords:
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