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嫦娥系列月球探测卫星轨道设计是基于受摄二体问题模型和限制性三体问题模型,根据相应的约束条件,利用摄动理论,求解卫星地月转移轨道入口点和卫星月球捕获点的状态参数,从而利用轨道拼接法设计运行轨道,并根据探测卫星不同任务设计特定的轨道。
Chang’e series lunar orbital satellite orbit design is based on the two-body model and the restricted three-body problem model, according to the corresponding constraints, the use of perturbation theory to solve the moon satellite orbit satellite acquisition point and the moon landing point state parameters , So as to design the orbit using the orbital splicing method and design a specific orbit according to different tasks of the sounding satellite.