摘要
介绍了我国第一颗微小卫星“创新一号”电源分系统的技术指标、设计方案和飞行试验结果。“创新一号”卫星电源分系统采用三域控制的全调节母线拓扑结构、用软件取代硬件进行控制等新技术,取得了成功。
The technical requirement, design sketch and flight test result of the electrical power subsystem （EPS） for the CX-1 microsatellite, which is the first microsatellite in China,were introduced in this paper.The EPS with 3-domain regulated bus and hardware replaced by software is successful.
出处
《电源技术》
CAS
CSCD
北大核心
2005年第9期612-615,共4页
Chinese Journal of Power Sources
