orbit calculation

基本解释

In lower scaled action region, the experimental result is in agreement with the semiclassical closed orbit calculation using uniform approximation.
均匀化近似闭合轨道理论计算谱与实验回归谱进行了比较，发现在低作用量处两者较好符合。
The main function of orbit calculation is to simulate the flight procedure of spacecraft, before that, the dynamics model of orbit must be established.
轨道计算主要用来模拟飞行器的飞行过程，前提是建立动力学模型。
Chapter 3 analyzes numerically the effects for orbit calculation caused by orbital perturbation, parameter error and so on. A precise mathematical model of orbit calculation is given.
第三章通过数值法分析了各项轨道摄动和参数误差等因素的对轨道计算的影响，给出了精确的月球探测器轨道计算数学模型。

轨道计算
Orbit calculation becomes the basic task of research of operating programming of the payloads. In this paper, 4t1?
飞行器的轨道数据是飞行器的最基本的状态参数，轨道计算成为运控模式研究的最基本任务。
地球科学
轨道计算