期刊文献+

高轨大功率电源控制器的工程研制与在轨应用 被引量:3

Engineering development of GEO high-power PCU and its in-orbit application
下载PDF
导出
摘要 针对我国大功率、长寿命卫星的应用需求,开展了高轨大功率电源控制器(PCU)的研究工作。PCU设计上采用全调节统一母线,接口上适应高效三结砷化镓太阳电池阵的结电容特性,满足高比能量锂离子蓄电池组的恒流恒压充电需求;采用模块化设计,具有母线品质好、输出功率范围宽、载荷适应能力强等优点,在地球同步轨道通信卫星、遥感卫星等领域有广泛应用前景。介绍了高轨大功率PCU的工程研制和在轨应用情况,对国产大功率PCU的设计方法、技术特点及研制情况进行了描述,结合国产大功率PCU在高分四号卫星上的应用,对在轨飞行数据进行了梳理、分析和评价。 The GEO high-power PCU (Power Conditioning Unit) can meet the requirements of high-power and long-life satellite. The PCU with 3-region control and uniform bus was designed, which adapted to the junction capacitance of the high efficiency triple-junction GaAs solar cell and satisfied the demand of the high specific energy lithium battery with the constant current and constant voltage charging mode. The PCU adopted modular design with the advantages of wide range output power and excellent load adaptability, having good application prospect in high-power geosynchronous satellite. This paper described the research and application of GEO high-power PCU. The design method and technical characteristics of the PCU was introduced. The performance specification of the PCU was adequately tested and verified by qualification test. The in-orbit operation state of PCU was analyzed by telemetry data.
作者 李建平 武明 鲁伟 徐伟 王锴 LI Jian-ping;WU Ming;LU Wei;XU Wei;WANG Kai(Tianjin Institute of Power Sources, Tianjin 300384, China;Beijing Institute of Spacecraft System Engineering, Beijing 100094, China)
出处 《电源技术》 CAS 北大核心 2019年第5期864-868,共5页 Chinese Journal of Power Sources
关键词 电源控制器 大功率 全调节 在轨应用 地球同步轨道 power conditioning unit high-power fully regulated in-orbit application geosynchronous
  • 相关文献

参考文献2

二级参考文献13

  • 1石峰,赵京伟,舒乐,衡月昆,赵小健.直流高压电源纹波的实验研究[J].核电子学与探测技术,2006,26(1):54-59. 被引量:12
  • 2卫星电测技术.中国宇航出版社,2009.
  • 3赵吉明,李雨庆.空间电源系统的综合测试技术.2002中国宇航学会空间能源学术年会.
  • 4Q/w80A-97卫星电源术语.
  • 5Shiguo Luo. A review of distributed power systems part I : DC distributed power system, IEEE A&E System Maga- zine, 2005,20 (8).
  • 6James R Wertz,Wiley J Larson.航天任务的分析与设计.航空工业出版社,1992.
  • 7James A Momoh, Kaili Xu. Multiple objective optimiza- tion in a spacecraft power system to maximize service- ability, - 2005 ISAP :268 - 236.
  • 8Edward J Simburgey, Daniel Rumsey, David Hinkley, Simontiu and Peter Carian. Distributed power system for microsatellites. - 2005 IEEE. 822 - 826.
  • 9万成安,于磊,刘建强.航天器直流电源系统稳定性分析方法研究[J].航天器工程,2009,18(2):14-19. 被引量:14
  • 10刘民,孙毅,赵晓光.直流电源输出阻抗测量技术[J].宇航计测技术,2010,30(5):18-22. 被引量:4

共引文献4

同被引文献15

引证文献3

二级引证文献36

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部