卫星电力系统用新型双输入多输出交错直流升压变换器

J. Gorji, K. Abbaszadeh, Farhad Bagheroskouei
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引用次数: 9

摘要

提出了一种新的双输入多输出交错直流升压变换器。该变换器是一种可用于卫星电源系统的高增益非隔离升压变换器。该变换器具有几个输出增益不同的直流链路,以馈送其他卫星子系统。该变换器是一种交错升压变换器,因此它比传统的变换器性能更好。该变换器在卫星供电子系统中的主要任务是最大功率点跟踪(MPPT)、电池充电和线路直流稳压。通常,需要三个独立的转换器来提供这些任务。通过增加电力电子装置,卫星的体积和重量将会增加。这是不可取的,因此,必须使用综合电路来同时执行上述三项任务。所提出的变换器具有集成结构,只有四个由不同占空比控制的开关。此外,该转换器具有用于连接太阳能阵列的单向输入和用于连接电池的双向输入。根据电池的充电或放电状态,该变换器定义了三种工作模式。该变换器的一个突出特点是电池底座接地,因此噪音不会损坏电池,从而提高电池的使用寿命。在不同工况下的仿真结果验证了理论分析的正确性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A New Two-input And Multi-output Interleaved DC_DC Boost Converter For Satellites Power system
a new two-input and multi-output interleaved DC_DC boost converter is proposed. This converter is a high gain and non-isolated boost converter, which can be used in satellites power system. This converter has several dc links with different gains in the output to feed other satellite subsystems. This converter is an interleaved boost converter, so it performs better than the conventional converters. The main tasks of this converter in the subsystem of satellite energy supply are maximum power points tracking (MPPT), battery charging and line dc voltage regulation. Normally, three separate converters are required to provide these tasks. By increasing the power electronic devices, the volume and weight of the satellite will go up. This is not desirable, therefore, must use a comprehensive circuit to perform the three above tasks at the same time. The proposed converter has an integrated structure with only four switches that controlled by different duty cycles. Also this converter has a uni-directional input for connecting the solar array and a bi-directional input for connecting the battery. Based on charging or discharging state of the battery, three operation modes are defined for this converter. One of the prominent features of the proposed converter is the battery bases grounded, so the noise cannot damage the battery and so on increase the useful life of battery. Theoretical analysis of the proposed converter is verified by simulation results for different operation conditions.
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