Power Management of a Modular Three-Port Converter-Based Spacecraft Power System

被引：14
作者：
Zhang, Junjun [1 ]
Wu, Hongfei [1 ]
Xing, Yan [1 ]
Hu, Haibing [1 ]
Cao, Feng [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Jiangsu Key Lab Renewable Energy Generat & Power, Nanjing 211100, Jiangsu, Peoples R China
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2016年 / 52卷 / 01期
基金：
中国国家自然科学基金;
关键词：
DROOP CONTROL; REGULATOR; INTERFACE;
D O I：
10.1109/TAES.2015.140808
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A modular three-port converter-based spacecraft power system is analyzed. To achieve power management of the distributed power system, a novel hybrid power control strategy is proposed, that is, current sharing control on the battery port when the battery discharges and power distribution based on the ability of sources when the battery charges. With the proposed power control, reliable and stable operations of the system within all of the conditions can be achieved. The experimental results demonstrate the feasibility of the proposed power control strategy.
引用
收藏
页码：486 / U533
页数：7
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