最后给出构形长期引力摄动的相关结论，并对编队构形设计提出建议，这将为研究编队构形的规划技术带来方便。
At last, some conclusions of formation secular evolvements and some advises about formation design are provided, which can be of some help to the study of formation planning.
编队卫星轨道设计与构形保持的主要目的就是以较小的代价满足这两个约束。
The purpose of the formation design and station keeping is satisfying two constraints with the least propellant cost.
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。
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.
本文研究了编队飞行卫星群的轨道动力学特性，提出了编队飞行的轨道构形设计的原则和方法。
This paper reveals the dynamical characteristics of relative orbital motion of formation flight and presents the principles and method for the orbit configuration design of formation flight.
本文研究了编队飞行卫星群的轨道动力学特性，提出了编队飞行的轨道构形设计的原则和方法。
This paper reveals the dynamical characteristics of relative orbital motion of formation flight and presents the principles and method for the orbit configuration design of formation flight.
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