首页|Z源逆变器高阶微分反馈控制研究

Z源逆变器高阶微分反馈控制研究

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以航空静止变流器控制为研究对象,针对传统两级逆变结构效率低、系统复杂以及死区效应带来的死区波形畸变问题,引入Z源逆变器设计航空静止变流器;针对Z源逆变器系统高阶且非最小相位造成的控制器设计复杂的问题,引入了一种基于高阶微分器的反馈控制策略,该控制策略利用高阶微分器对系统各阶状态变量进行估计,具有不依赖于精确系统模型的特点;仿真实验表明,将此反馈控制器用于Z源逆变器输出电压控制时能够有效跟踪给定输出电压,系统受到外部扰动时依然能保持良好的静态和动态性能,满足静变流器控制需求。
Research on Higher-order Differential Feedback Control of Z-source Inverters
Taking aeronautic static inverters as the research object,the Z-source inverter is introduced to design aeronautic static inverter for its traditional two-stage structure with low efficiency and complex system and the waveform distortion caused by the dead zone effect.Aiming at the complex controller design due to the high order and non-minimum phase of Z-source inverter system,a feedback control strategy based on a high-order differentiator is introduced.The control strategy uses the higher-order differentiators to estimate the system state variables at each order,and it does not depend on an exact system model.The simulation experiments show that when used for Z-source inverter output voltage control,this feedback controller can effectively track the given output volt-age,and maintain a good steady-state and dynamic performance under external disturbances,meeting the aeronautic static inverter control requirements.

aeronautic static inverterZ-source inverterhigher order differentiatorstatus estimationfeedback control

刘松涛、王丙元

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中国民航大学电子信息与自动化学院,天津 300300

航空静止变流器 Z源逆变器 高阶微分器 状态估计 反馈控制

国家自然基金科学项目

U1333102

2024

计算机测量与控制
中国计算机自动测量与控制技术协会

计算机测量与控制

CSTPCD
影响因子:0.546
ISSN:1671-4598
年,卷(期):2024.32(2)
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