该插件实现了卫星构形的参数化设计和分析，其分析结果为其它学科的设计提供参考和依据。
Parameter design and analysis for satellite configuration can be implemented with this module, and its result can be referenced by other subject design.
通过对绕飞编队特性的研究，提出了一种适于摄影测量的卫星绕飞编队构形。
According to the study of the performance of the satellite flying-around formation, a formation suit for photogrammetry is proposed.
研究近地轨道卫星编队构形在引力摄动作用下的长期演化机理。
The mechanism of Low earth orbit(LEO) satellite formation secular evolvement under the influence of gravitational perturbations is studied.
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