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基于干扰观测器的磁悬浮姿控飞轮电机控制
引用本文:周新秀,房建成,刘刚,张然.基于干扰观测器的磁悬浮姿控飞轮电机控制[J].北京航空航天大学学报,2012,38(11):1459-1463,1468.
作者姓名:周新秀  房建成  刘刚  张然
作者单位:北京航空航天大学仪器科学与光电工程学院,北京,100191;中国空间技术研究院,北京,100094
基金项目:国家杰出青年科学基金资助项目,国家自然科学基金资助项目
摘    要:由于磁悬浮飞轮转子不平衡振动的存在,飞轮力矩/转速控制精度受到影响.为有效地对不平衡振动干扰进行估计,提出了一种针对时变谐波扰动的非线性干扰观测方法,观测器的动态与稳态性能可以根据系统要求设定,具有全局一致收敛性;在非线性干扰观测器的基础上设计变结构控制器对飞轮转速进行控制并对干扰进行补偿,通过改进变结构控制器的滑模函数与控制律系统抖振可以有效地削弱.仿真与实验结果表明:基于非线性干扰观测器的变结构控制器具有很好的扰动抑制能力和动态响应、稳态误差调节能力,可用于实现飞轮输出力矩控制.

关 键 词:磁悬浮  飞轮  非线性干扰观测  变结构控制
收稿时间:2011-05-27

Disturbance observer based magnetically suspended reaction attitude flywheel motor control
Zhou Xinxiu Fang Jiancheng Liu GangSchool of Instrument Science and Opto-electronics Engineering,Beijing University of Aeronautics and Astronautics,Beijing,China Zhang Ran.Disturbance observer based magnetically suspended reaction attitude flywheel motor control[J].Journal of Beijing University of Aeronautics and Astronautics,2012,38(11):1459-1463,1468.
Authors:Zhou Xinxiu Fang Jiancheng Liu GangSchool of Instrument Science and Opto-electronics Engineering  Beijing University of Aeronautics and Astronautics  Beijing  China Zhang Ran
Institution:1. School of Instrument Science and Opto-electronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;2. China Academy of Space Technology Research Institute, Beijing 100094, China
Abstract:As the existence of mass unbalance of magnetically suspended flywheel rotor, the precision of output torque/speed of flywheel would be influenced. In order to estimate the unbalance vibration, a nonlinear disturbance observer for time-variation harmonic disturbance was proposed. The dynamic response and steady-stage error regulating characteristics can be adjusted according to systematic requirement. A variable structure controller based on nonlinear disturbance observer was designed for speed control and vibration compensation. By improving the sliding mode function and sign function the chattering can be suppressed. The validity of the control method has been proved by simulation and experiment. The proposed controller is superior in the dynamic response performance, steady-stage error regulating characteristics and disturbance attenuation ability.
Keywords:
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