研究了通过遗传算法模型优化设计侦察卫星轨道高度、轨道倾角、右升交点角及平近点角等轨道参数的方法。
Through the GA model, the orbital elements of each satellite such as altitude, inclination, RAAN and mean anomaly are optimized.
自动化的检测软件检测到存储每个卫星,碎片和流星视频剪辑,并提供估计的,高度和轨道倾角。
The automated detection software stores video clips of each detected satellite, debris, and meteor and provides estimates of the, altitude and inclination of the orbits.
提出了一个由八颗同地迹有一定倾角的地球同步圆形轨道(IGSO)卫星组成的区域导航星座方案。
A regional navigation constellation scheme composing eight IGSO satellites of ground track is presented in this paper.
并且根据卫星群偏心率与倾角综合的分离思想,讨论了两种策略,使得卫星群的构形可通过每个成员的轨道要素简单表出。
The satellites follow a combined eccentricity and inclination vector separation strategy, so that the group geometry can be expressed simply by the orbital elements of each member.
利用STK软件的输出数据,分析并仿真了不同轨道倾角和高度卫星的太阳帆板和本体外表面的温度特性。
By using the output data of the STK software, the temperature characteristics of the solar panels of the satellites at different inclinations and altitudes are analyzed and simulated.
利用一条假设的卫星轨道说明了月球引力场对其轨道倾角的影响。
A supposed orbit to show the effect of the moon gravitation on the orbit inclination is also introduced.
利用一条假设的卫星轨道说明了月球引力场对其轨道倾角的影响。
A supposed orbit to show the effect of the moon gravitation on the orbit inclination is also introduced.
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