机译:基于两段月球自由返回轨迹的月球轨道插入
School of Aerospace Engineering, Tsinghua University, Beijing 100084, China ,Department of Aerospace, Texas A&M University;
School of Aerospace Engineering, Tsinghua University, Beijing 100084, China;
School of Aerospace Engineering, Tsinghua University, Beijing 100084, China;
School of Aerospace Engineering, Tsinghua University, Beijing 100084, China;
Two-segment free-return; Lunar global coverage; Restricted three-body model;
机译:可变对称自由返回轨迹的最佳月球轨道插入
机译:基于伪状态理论的二段月球自由返回轨迹设计
机译:两段月球自由返回轨迹的分析
机译:基于假稳义理论的双分割月球自由返回轨迹
机译:利用月球侦察轨道数据发现和表征月球熔岩管的新方法
机译:月球轨道激光测高仪探测月潮
机译:月球出击任务的月球插入目标和相关出站任务设计
机译:月球大气尘环境探测器(LaDEE)航天器对月球轨道插入机动失效的应变轨迹设计。