首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于模型补偿的风力机变桨距线性自抗扰控制器设计
引用本文:张吉宣,贾建芳,戴媛媛.基于模型补偿的风力机变桨距线性自抗扰控制器设计[J].航空动力学报,2018,45(6):88-94.
作者姓名:张吉宣  贾建芳  戴媛媛
作者单位:中北大学 电气与控制工程学院,山西 太原030051,中北大学 电气与控制工程学院,山西 太原030051,中北大学 电气与控制工程学院,山西 太原030051
基金项目:国家自然科学基金项目(61573250)
摘    要:设计了一种变桨距线性自抗扰控制器,估计和补偿了系统未建模部分和外界干扰,实现额定风速以上时系统输出功率稳定于额定值;并采用模型补偿方法对自抗扰控制器进行优化,减少了参数整定的数目,提高了系统控制精度。对额定功率为300 kW的风电机组分别在阶跃风、阵风以及湍流风作用下进行系统仿真。结果表明,该方法可以快速调节风速变化引起的输出波动,使得系统输出稳定且超调量小,具有很好的稳定性和鲁棒性。

关 键 词:风力发电机    变桨距控制    线性自抗扰控制器    模型补偿

Design of Linear Active Disturbance Rejection Controller for WindTurbine Variable Pitch System Based on Model Compensation
ZHANG Jixuan,JIA Jianfang and DAI Yuanyuan.Design of Linear Active Disturbance Rejection Controller for WindTurbine Variable Pitch System Based on Model Compensation[J].Journal of Aerospace Power,2018,45(6):88-94.
Authors:ZHANG Jixuan  JIA Jianfang and DAI Yuanyuan
Institution:School of Electrical and Control Engineering, North University of China,Taiyuan 030051, China,School of Electrical and Control Engineering, North University of China,Taiyuan 030051, China and School of Electrical and Control Engineering, North University of China,Taiyuan 030051, China
Abstract:A linear active disturbance rejection controller (LADRC) was designed to estimate the system unmodeled part and compensate the interference, thereby achieve output power stable when wind speed was above rated wind speed. And the model compensation method was used to optimize the LADRC, to reduce the number of parameters that need to be set and improve system control accuracy. The controller was simulated in three different wind conditions in the 300 kW wind turbines. The simulation results showed that it can quickly adjust the output fluctuation caused by wind velocity variation, made the system output stable and had small overshoot in any wind speed stage. Moreover, the system had good stability and robustness.
Keywords:wind turbine  variable pitch control  linear active disturbance rejection controller (LADRC)  model compensation
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》下载免费的PDF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