The optimal design of the trajectory for the standard twice reentry of mooncraft under the conditions of the trajectory endpoint set and multiply objective constraints in this paper.
对登月飞船在指定轨道终点及多约束条件下两次再入轨道的优化设计进行了研究。
The optimal design of the trajectory for the standard twice reentry of mooncraft under the conditions of the trajectory endpoint set and multiply objective constraints in this paper.
对登月飞船在指定轨道终点及多约束条件下两次再入轨道的优化设计进行了研究。
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