电工技术学报  2017, Vol. 32 Issue (增刊1): 107-115    DOI: 10.19595/j.cnki.1000-6753.tces.L70603
电机与电器 |
基于自抗扰控制原理的全电飞机用永磁同步电机转速闭环控制
崔淑梅1, 匡志1, 杜博超1, Ostanin Sergei Yurievich2, Milyaev Igor Matveevich3
1. 哈尔滨工业大学电气工程及自动化学院 哈尔滨 150001;
2. 莫斯科动力学院 莫斯科 111250;
3. 俄罗斯科学院冶金和材料学研究所 叶卡捷琳堡 620016
Speed Closed-Loop Control of Permanent Magnet Synchronous Motor for All-Electric Aircraft Applications Based on Active Disturbance Rejection Controller
Cui Shumei1, Kuang Zhi1, Du Bochao1, Ostanin Sergei Yurievich2, Milyaev Igor Matveevich3
1. School of Electrical Engineering and Automation Harbin Institute of Technology Harbin 150001 China;
2. Moscow Power Engineering Institute Moscow 111250 Russia;
3. A.A. Baikov Institute of Metallurgy and Material Science Yekaterinburg 620016 Russia
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摘要 采用永磁同步电机直接驱动全电飞机螺旋桨,为了抑制不稳定气流对输出转矩影响和提高螺旋桨抗扰动能力,对永磁同步电机实现基于自抗扰原理的转速闭环控制。分析不同飞行状态下螺旋桨的转速与转矩需求,建立基于自抗扰转速闭环控制模型并利用Dspace模拟飞行工况运行。仿真和实验验证了基于自抗扰转速闭环系统对负载变化具有抗扰能力,整个飞行工况下永磁同步电机转速响应平稳,转矩输出符合螺旋桨转矩需求。
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崔淑梅
匡志
杜博超
Ostanin Sergei Yurievich
Milyaev Igor Matveevich
关键词 永磁同步电机自抗扰控制器转速闭环控制全电飞机    
Abstract:This paper utilized permanent magnet synchronous motor (PMSM) to directly drive the propeller blade of an electric aircraft, in order to restrain unstable air flow effects for output torque and improve disturbance rejection ability for propeller, speed closed loop control of PMSM based on active disturbance rejection controller (ADRC) was employed. The torque requirement on propeller blade operation was analyzed in different flying status, the model of speed closed loop based on ADRC was built and the flying condition was simulated by using Dspace. The simulation and experiment results validate the ability to resist load disturbance, the response of speed is stable and the output torque accord with required torque for propeller during the whole flying statues.
Key wordsPermanent magnet synchronous motor (PMSM)    active disturbance rejection controller (ADRC)    speed closed loop control    all-electric aircraft   
收稿日期: 2016-08-20      出版日期: 2017-09-14
PACS: TM341  
基金资助:国家自然科学基金项目资助(51577035)
通讯作者: 崔淑梅 女,1964年生,教授,博士生导师,研究方向为电动汽车电驱动控制。E-mail:cuism@hit.edu.cn   
作者简介: 匡 志 男,1983年生,博士研究生,研究方向为电动车用驱动电机系统及其控制。E-mail:kuangzhi0201 @126.com
引用本文:   
崔淑梅, 匡志, 杜博超, Ostanin Sergei Yurievich, Milyaev Igor Matveevich. 基于自抗扰控制原理的全电飞机用永磁同步电机转速闭环控制[J]. 电工技术学报, 2017, 32(增刊1): 107-115. Cui Shumei, Kuang Zhi, Du Bochao, Ostanin Sergei Yurievich, Milyaev Igor Matveevich. Speed Closed-Loop Control of Permanent Magnet Synchronous Motor for All-Electric Aircraft Applications Based on Active Disturbance Rejection Controller. Transactions of China Electrotechnical Society, 2017, 32(增刊1): 107-115.
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