MEO卫星太阳电池阵在轨功率分析  

Analysis of power output on orbit of MEO-satellite solar array

作　　者：尹兴月[1] 林君毅[1] 王晟[2] 

机构地区：[1]中国电子科技集团公司第十八研究所,天津300384 [2]海军装备部,北京100841

出　　处：《电源技术》2013年第6期1007-1009,共3页Chinese Journal of Power Sources

摘　　要：MEO卫星轨道为中轨道,轨道高度约为24 000 km。通过对卫星太阳电池阵在轨功率与地面预计结果的对比,验证了数学模型及其参数选择的准确性,为后续型号的设计工作提供了数据支持。MEO is a medium earth orbit at an altitude of 24 000 km. By comparing the results of power output on orbit of solar array with its prediction results, the accuracy of the mathematical model and its parameter selection were verified, which is important for the development of the aerospace industry in China.

关 键 词：MEO 太阳电池阵 在轨功率 

分 类 号：TM914[电气工程—电力电子与电力传动]