Taking the design of Venus gravity-assist trajectories as an example, the relation between orbital eccentricity and orbitalinclination was analyzed.
以金星借力轨道设计为例,分析了轨道偏心率与轨道倾角增量之间的关系。
2
The orbitalinclination, orbital altitude, elevation of GPS antenna and orbital eccentricity were researched as the influential factors to doppler range.
研究轨道倾角、轨道高度、GPS天线仰角和轨道偏心率等因素对多普勒频率搜索范围的影响。
3
The most efficient launch trajectory is due east from a launch site, which places the satellite into an orbitalinclination equal to the latitude of the launch site.