A high step up flying capacitor inverter with the voltage balancing control method

Amin Ashraf Gandomi, S. Saeidabadi, S. Hosseini
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引用次数: 9

Abstract

A novel flying capacitor inverter has been proposed that utilizes the transformer in the basic unit. In order to generate all the voltage levels (even and odd) at the output, the magnitude of the capacitor's voltage is controlled. Also a new control strategy to generate maximum output voltage levels is proposed. The proposed control strategy is capable of regulating the voltage of the flying capacitor in different levels enabling tunable RMS values of the output voltage levels. In addition, a loss analysis has been performed to assess the sources of losses stemming from different components of the inverter (i.e. power switches, transformer and flying capacitor). Finally, numerical simulation has been performed to model the performance of the proposed topology and corresponding control strategy under different conditions and the results of numerical simulation confirms the stable performance of the proposed inverter.
一种采用电压平衡控制方法的高升压飞电容逆变器
提出了一种利用变压器作为基本单元的新型飞电容逆变器。为了在输出端产生所有的电压电平(偶数和奇数),电容器电压的大小是受控制的。并提出了一种新的控制策略,以产生最大输出电压水平。所提出的控制策略能够对飞行电容器的电压进行不同水平的调节,使输出电压水平的均方根值可调。此外,还进行了损耗分析,以评估逆变器不同组件(即电源开关、变压器和飞行电容器)产生的损耗来源。最后,通过数值仿真对所提出的拓扑结构和相应的控制策略在不同条件下的性能进行了建模,数值仿真结果证实了所提出的逆变器性能稳定。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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