Free return orbit design and characteristics analysis for manned lunar mission

查看全文 作　　者：PENG QiBo SHEN HongXin LI [1]HaiYang

机构地区：[1]College of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China

出　　处：《Science China(Technological Sciences)》索引2011年第54卷第12期,共8页

基　　金：supported by the National Natural Science Foundation of China (Grant No.10902121) 摘　　要：A circumlunar free return orbit design model that satisfies manned lunar mission constraints is established. By combining analytical method with numerical method,a serial orbit design strategy from initial value design to precision solution is proposed. A simulation example is given,and the conclusion indicates that the method has excellent convergence performance and precision. According to a great deal of simulation results solved by the method,the free return orbit characters such as accessible moon orbit parameters,return orbit parameters,transfer delta velocity,etc. are analyzed,which can supply references to constitute manned lunar mission orbit scheme. 关键词：返回轨道设计模型载人登月特性轨道参数环月轨道数值方法设计策略

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Free return orbit design and characteristics analysis for manned lunar mission

参考文献(14)

引证文献(25)

耦合文献(42)

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