7. Thirdly, take a lunar probe for example, the trajectory under precise gravitymodels is designed based on STK by solving N-body problem through the differentialcorrecting method.
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- 再次,以月球探测器的极轨轨道设计为例,采用微分修正法求解N体问题,基于STK进行精确引力模型下的轨道优化设计。收藏指正