空间电源功率调节技术综述  

Review on Power Conditioning Unit for Spacecraft

作　　者：郭显鑫 郭祖佑[1] 王卫国[1] 

机构地区：[1]兰州物理研究所,甘肃兰州730000

出　　处：《上海航天》2010年第3期30-39,共10页Aerospace Shanghai

摘　　要：介绍了空间电源功率调节装置(PCU)的分流调节器(SR),蓄电池的充电控制器(BCR)、放电控制器(BDR)和主误差放大器(MEA)的原理和技术现状。阐述了顺序开关分流调节(S3R)、混合型调节和顺序开关分流串联调节(S4R)三种基本拓扑的工作原理,并对三者进行了性能比较,认为S4R是目前最先进的调节技术。讨论了功率调节装置模块化、智能化和小型化的发展趋势并分析了大功率的功率调节装置研制难点。The principles and current technology of shunt regulator,battery charge regulator,battery discharge regulator and main error amplifier of the power conditioning unit（PCU） in space power were introduced in this paper.The principles of the three basic regulated bus topology,which were sequential switching shunt regulator（S^3R）,hybrid regulator and sequential switching serial shunt regulator（S^4R）,were analyzed.The comparison among them was done.It was believed that S^4R topology was the most advanced.The developing trend,modularity,intelligence and thick-film were also discussed,and so were the difficulties in researching a high power PCU.

关 键 词：功率调节装置 分流调节器 充电控制器 放电控制器 顺序开关分流调节 顺序开关分流串联调节 

分 类 号：V442[航空宇航科学与技术—飞行器设计]