This method provides better accuracy than approaches that modify the initial conditions of the C-W equations for a circular referenceorbit.
与对圆参考轨道的C - W方程初始条件进行修正的方法相比，该方法有更高的设计精度。
2
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 reference satellite.
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。
3
Introduce the reference frame and time system used in orbit design particularly. Analyzed the orbit characteristic of two-body problem and launch window.