首页> 外文期刊>Aerospace and Electronic Systems, IEEE Transactions on >DC/DC Converter for the International Space Station
【24h】

DC/DC Converter for the International Space Station

机译:国际空间站的DC / DC转换器

获取原文
获取原文并翻译 | 示例
           

摘要

A dc/dc converter for power distribution aboard the International Space Station (ISS) and space vehicles employing the 120 V dc bus is proposed. It is well suited to supply power to multiple loads including peripheral low voltage point-of-load (POL) regulators. The dc/dc converter is phase-shift controlled at the constant frequency of 500 kHz. The topology is characterized by distribution in a sequence of 4 metal-oxide semiconductor field-effect transistors (MOSFETs), switched ON at zero voltage. The linear model has first-order dynamics. Responses to small and large load variations benefit from its advantageous control features. A peculiar characteristic is its high dynamic independence of load typology and output power. To focus on this quality, dynamic performances are investigated through analyses, simulations, and measurements considering three types of loads: constant current, resistive, and constant power. Experimental data from a 100 W prototype fit the model forecasts well.
机译:提出了一种用于在国际空间站(ISS)和采用120 V直流总线的航天器上进行配电的DC / DC转换器。它非常适合为包括外围低压负载点(POL)调节器的多个负载供电。 dc / dc转换器以500 kHz恒定频率进行相移控制。该拓扑的特点是按四个金属氧化物半导体场效应晶体管(MOSFET)的顺序分布,并在零电压下导通。线性模型具有一阶动力学。有利的控制功能使对大小负载变化的响应都受益。独特的特性是负载类型和输出功率的高度动态独立性。为了关注这一质量,通过分析,模拟和测量来研究动态性能,其中考虑了三种类型的负载:恒定电流,电阻性和恒定功率。 100 W原型的实验数据很好地拟合了模型预测。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号