Citation: | Song Shunguang, Wang Chunjie. Landing stability analysis of the lunar lander based on Monte Carlo approach[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(9): 1192-1196. (in Chinese) |
[1] 褚桂柏,张熇.月球探测器技术[M].北京:中国科学技术出版社,2007:123-131 Chu Guibai,Zhang He.Lunar probe techniques[M].Beijing:China Science & Technology Press,2007:123-131(in Chinese) [2] Hilderman R A,Mueller W H,Mantus M.Landing dynamics of the lunar excursion module[J].Journal of Spacecraft and Rockets,1966,3(10):1484-1489 [3] 朱汪,杨建中.月球着陆器软着陆机构着陆稳定性仿真分析[J].宇航学报,2009,30(5):1792-1796 Zhu Wang,Yang Jianzhong.Touchdown stability simulation of landing gear system for lunar lander[J].Journal of Astronautics,2009,30(5):1792-1796(in Chinese) [4] Briere M,Weber J.Robotic lunar lander development project:three dimensional dynamic stability testing and analysis[R].NASA/CP-2011-215873,2010 [5] Ponnusamy D,Maahs G.Development and testing of leg assemblies for robotic lunar lander[C]//Ouwehand L.Proceedings of the 14th European Space Mechanisms and Tribology Symposium.Noordwijk:ESA Communications,2011:485-492 [6] Cole T J,Bassler J,Cooper S,et al.The challenges of designing a lightweight spacecraft structure for landing on the lunar surface[J].Acta Astronautica,2012,71:83-91 [7] 林轻,聂宏,徐磊,等.月球着陆器软着陆稳定性关键影响因素分析[J].南京航空航天大学学报,2012,44(2):152-158 Lin Qing,Nie Hong,Xu Lei,et al.Analysis on key influence factors of soft-landing stability in lunar lander[J].Journal of Nanjing University of Aeronautics and Astronautics,2012,44(2):152-158(in Chinese) [8] Lavender R E.Monte Carlo approach to touchdown dynamics for soft lunar landings[R].NASA-TN-D-3117,1965 [9] Merchant D H,Sawdy D T.Monte Carlo dynamic analysis for lunar module landing loads[J].Journal of Spacecraft and Rockets,1971:8(1):48-55 [10] Lu Yuntong,Wang Chunjie,Zeng Fuming,et al.A Monte Carlo analysis of lunar lander dynamics at touchdown[C]//CSAA.Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology.Xi-an:Northwestern Polytechnical University Press,2010:481-484 [11] 逯运通,宋顺广,王春洁,等.基于刚柔耦合模型的月球着陆器缓冲试验动力学仿真分析[J].北京航空航天大学学报,2010,36(11):1348-1352 Lu Yuntong,Song Shunguang,Wang Chunjie,et al.Dynamic analysis for lunar lander based on rigid-flexible coupled model[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(11):1348-1352(in Chinese) [12] Rogers W F.Apollo experience report-lunar module landing gear subsystem[R].NASA-TN-D-6850,1972 [13] Zupp G A,Doiron H H.A mathematical procedure for predicting the touchdown dynamics of a soft-landing vehicle[R].NASA-TN-D-7045,1971 [14] Law A M.Simulation modeling and analysis[M].4th ed.Beijing:Tsinghua University Press,2009:494-500 [15] GB/T 4088-2008 数据的统计处理和解释二项分布参数的估计与检验[S] GB/T 4088-2008 Statistical interpretation of data-estimation and hypothesis test of parameter in binomial distribution[S]
|