摘要
根据带有太阳帆板的地球同步卫星在轨测试需求，分析了星上电源系统的组成及技术状态；并以光照区可调节母线为例。给出了卫星电源系统在轨测试方法及相应的计算公式；最后，通过工程验证了该方法的正确性。
This paper analyzes the composition and status of the electrical power systems of China＇s geostationary satellites in accordance with the requirements for in-orbit test of geosynchronous satellites equipped with solar arrays. Taking adjustable bus in illuminated region as an example, the method of in-orbit test for EPS systems and the calculation equations are given. Application results show that the method is effective.
出处
《飞行器测控学报》
2007年第1期38-41,共4页
Journal of Spacecraft TT&C Technology
关键词
地球同步轨道
电源系统
在轨测试
太阳帆板
卫星操作中心
Geosynchronous Orbit
Electrical Power System
In-Orbit Test
Solar Array
Satellite Operation Center
