摘要
微小卫星多采用体装式太阳电池阵,运行在100~1 000 km的轨道。卫星的飞行姿态对太阳电池阵的输出功率有重要影响。对于无姿态控制的微小卫星,分析了不同条件下太阳电池阵的功率输出。针对卫星在轨飞行,预计了太阳电池阵的输出功率及变化规律,为卫星功率计算提供了计算依据。
The minisatellites operate in orbits of around 100 km to 1 000 km above the Earth＇s surface,powered by body mounted solar array.The output of the solar array was related to the minisatellite＇s attitude.For the minisatellite without attitude control,the output of the solar array was analyzed,and the law of change of output in-orbit was also predicted,which was important to the power analysis for minisatellite.
出处
《电源技术》
CAS
CSCD
北大核心
2012年第10期1478-1480,共3页
Chinese Journal of Power Sources
