Configurable High Voltage Power Supply for Full Electric Propulsion Spacecraft

M. Bekemans, François Bronchart, T. Scalais, A. Franke
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引用次数: 6

Abstract

The present paper describes several technological topics featured in a new prototype of anode/beam supply for 5 kW Power Processing Unit (PPU), dedicated to be compatible with many thruster types and operating modes thanks to a configurable output stage and wide output voltage range. The achievements in terms of power density and cost reduction are attributed to a new electrical topology (Dual Active Bridge) allowing better current form factor and hence lower losses, but also to wide-bandgap semiconductors and to a new, high-power, high-voltage transformer. A versatile digital control has been implemented to be compatible with all output configurations and to use additional degree of freedom in the control loop to minimize certain losses.
全电力推进航天器的可配置高压电源
本文介绍了用于5kw功率处理单元(PPU)的阳极/光束电源的新原型中的几个技术主题,由于可配置的输出级和宽输出电压范围,该原型致力于与许多推进器类型和工作模式兼容。功率密度和成本降低方面的成就归功于新的电拓扑(双有源桥),它允许更好的电流形状因子,从而降低损耗,但也归功于宽带隙半导体和新的高功率高压变压器。一个通用的数字控制已经实现与所有输出配置兼容,并在控制回路中使用额外的自由度,以尽量减少某些损失。
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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