... 自动再入制导 automatic reehtry guidance 基准轨道 datum orbit; reference orbit 弹道再入 ballistic reentry ...
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eccentric reference orbit 椭圆参考轨道
Osculating Reference Orbit 密切参考轨道
elliptical reference orbit 椭圆参考轨道
noncircular reference orbit 椭圆参考轨道
reference orbit eccentricity 椭圆参考轨道
This method provides better accuracy than approaches that modify the initial conditions of the C-W equations for a circular reference orbit.
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。
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。
Introduce the reference frame and time system used in orbit design particularly. Analyzed the orbit characteristic of two-body problem and launch window.
详细介绍了用于轨道设计的坐标系统和时间系统，分析了二体轨道特性和发射窗口的基本特性。
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