相邻两个升轨点之间的时间区间被称为节点周期(nodal period)或 者轨道周期(orbit period)。在一个节点周期内,卫星环绕地球完 成一圈公转(revolution)。
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Then, the relationship among nodal period, fundamental interval and orbital altitude was educed by deriving the definitions of fictitious node.
通过引入假想交点的概念,推导出了交点周期、基本交点距与轨道高度的关系。
On the basis of analyzing the effect of common configuration design method for the general method, the equal nodal period design method is introduced to improve the general method in this paper.
在分析编队构形一般设计方法设计效果的基础上,提出一种等交点周期法,对一般方法进行了改进。
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