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创新一号微小卫星电源分系统
引用本文:李国欣,张利群,张忠卫,张平.创新一号微小卫星电源分系统[J].上海航天,2006,23(1):41-45,60.
作者姓名:李国欣  张利群  张忠卫  张平
作者单位:上海空间电源研究所,上海,200233
摘    要:介绍了我国第一颗微小卫星创新一号(CX-1)电源分系统的性能、组成、工作原理,以及太阳电池阵、镉镍电池组和电源控制器等的设计和相应参数。分析了设计中采用的三域控制统一母线调节、高效三结砷化镓太阳电池发电和充电V-T曲线智能化控制管理等关键技术。飞行试验结果表明,CX-1卫星电源分系统的性能优良、工作可靠,达到了设计要求。

关 键 词:微小卫星  电源分系统  三域控制  砷化镓太阳电池  智能化控制管理
文章编号:1006-1630(2006)06-0041-05
收稿时间:2005-01-12
修稿时间:2005-01-122005-02-18

Electrical Power Subsystem of CX-1 Micro-Satellite
LI Guo-xin,ZHANG Li-qun,ZHANG Zhong-wei,ZHANG Ping.Electrical Power Subsystem of CX-1 Micro-Satellite[J].Aerospace Shanghai,2006,23(1):41-45,60.
Authors:LI Guo-xin  ZHANG Li-qun  ZHANG Zhong-wei  ZHANG Ping
Institution:Shanghai Institute of Space Power-Sources, Shanghai 200233, China
Abstract:The performance,construction,principle,and design and parameters of solar array,Cd-Ni battery and power controller of the power subsystem for CX-1 satellite,which was the first micro-satellite in China,were introduced in this paper.The key technologies such as 3-region control and uniform bus alignment,high efficiency power generating of 3-node GaAs solar cell,and intelligent control management of charge V-T curve were also analyzed.The on-orbit data showed that the function of the power subsystem operated with high performance and reliability which met the requirements in design.
Keywords:Micro-satellite  Electrical power subsystem  3-region control  GaAs solar cell  Intelligent control management
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