In the dynamic method, starting from the analytical solutions of the CW equations, the flying-around orbit is proved to be an ellipse centered at the referencesatellite.
动力学方法从CW方程的解析解出发，证明了绕飞轨道是以参考卫星为中心的椭圆。
2
This result have definite worth of reference for the structure design and analysis of the satellite antenna.
该结果对卫星天线结构设计与分析有一定的参考价值。
3
This paper gives the one-side approximate lower limit of complex system availability by using fitting method, it can be used in reference to evaluate the shortest life of satellite system.