月球着陆器着陆安全分析方法

苏庆华; 赵剡

月球着陆器着陆安全分析方法

苏庆华,
赵剡

北京航空航天大学仪器科学与光电工程学院, 北京 100191

基金项目: 航空科学基金资助项目(20100818018)

详细信息

中图分类号: V11
计量
- 文章访问数: 1851
- HTML全文浏览量: 159
- PDF下载量: 607
- 被引次数: 0
出版历程
- 收稿日期: 2011-07-31
- 网络出版日期: 2012-11-30

Analysis method for lunar landers landing safety

School of Instrument Science and Opto-electronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 月球着陆器软着陆地点选择及安全着陆实现是探月二期的关键问题.采用不考虑着陆器着陆过程中发动机控制、着陆姿态控制和动力学性能,在计算机上依据低精度月面数据和已有月面典型地形特征分布/形状模型仿真生成高精度着陆区域;根据着陆器的结构尺寸和着陆安全要求对每个安全参数进行计算、比较、判断得到单次着陆安全性,利用蒙特卡洛方法计算多次在仿真地形上的着陆安全概率.试验结果表明:采用这种方法时,着陆器的结构尺寸相同分析结果才有意义.在计算机上仿真生成着陆区域、设置着陆器结构尺寸和安全参数,使其可以用于地面系统的仿真实验,也可在月面软着陆过程中实时分析选定区域的着陆安全概率.
- 着陆器 /
- 着陆区域 /
- 着陆安全
Abstract: In the lunar exploration program Ⅱ, the lunar lander to a safelanding site selection and realize safelanding is the key issues. Without considering engine control, attitude control and dynamic property, a high-definition landing territory was simulated on computer based on the low-definition data and known characteristic models of lunar surface. One times landing security can be obtained by computing and analyzing lander profiles and landing safety requirement. The landing safety possibility of this terrain can be obtained by computing many times landing only under the condition of same lander profiles. The landing territory, lander profile and safety parameters were simulated on computer by this method can be applied to both ground simulation experiments and real-timely analyzing possibility of landing safety during soft landing on the lunar surface.
- lander /
- landing area /
- landing safety

HTML全文

参考文献(15)

[1]	欧阳自远.月球科学概论[M].北京:中国宇航出版社,2005:251-306 Ou’yang Ziyuan.Overview of the moon[M].Beijing:Astronautics Press,2005:251-306(in Chinese)
[2]	孙宏金.嫦娥一号探月卫星揭秘[M].北京:中国青年出版社,2007:238-261 Sun Hongjin.Lunar orbiter revelation of Chang’e-1 [M].Beijing:China Youth Press,2007:238-261(in Chinese)
[3]	Mueller E,Bilimoria K D,Frost C.Effects of control power and inceptor sensitivity on lunar lander handling qualities [J].Journal of Spacecraft and Rockets,2011,48(3):454-466
[4]	Ploen S R,Seraji H,Kinney C E.Determination of spacecraft landing footprint for safe planetary landing[J].Journal Transactions on Aerospace and Electronic systems,2009,45(1):3-16
[5]	曾福明,杨建中,朱汪,等.月球着陆器着陆缓冲性能研究[J].航天器工程,2010,19(5):43-49 Zeng Fuming,Yang Jianzhong,Zhu Wang,et al.Research on landing impact attenuation performance of lunar lander [J].Spacecraft Engineering,2010,19(5):43-49(in Chinese)
[6]	王闯,刘荣强,邓宗全,等.月球着陆器着陆过程动力学分析[J].北京航空航天大学学报,2008,34(4):381-385 Wang Chuang,Liu Rongqiang,Deng Zongquan,et al.Dynamics analysis of lunar lander’s landing process[J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(4):381-385(in Chinese)
[7]	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)
[8]	Batterson S,Benson H,Gault D,et al.NASA space vehicle design criteria(environment) lunar surface models.NASA,1969
[9]	Solver T,Amelin M.State duration based Monte Carlo simulation model with independent failures for distribution system reliability analysis [C]//9th International Conference on Probabilistic Methods Applied to Power Systems KTH.Stockholm,Sweden:2006 1-8
[10]	网易新闻.中国探月二期工程月球着陆器模型亮相 [OL]. [2010-11-16].http:[C]//war.news.163.com/photoview/4CA50001/11855.html#p=6LJO8T2G4CA50001
[11]	Cheatham D C,Bennett F V.Apollo lunar module landing strategy [R].Apollo Lunar Landing Symposium,1966
[12]	Zupp G A.A mathern atical procedure for predicting the touchdown dynamics of a soft-Landing vehicle [R].NASA,1971
[13]	Blanchard U J.Full-scale dynamic landing-impact investigation of a prototype lunar module landing gear [R].NASA,1969
[14]	Lafontaine J de,Ulitsky A,Tripp J W,et al.LAPS the development of a scanning lidar system with GNC for autonomous hazard avoidance and precision landing [C]// Proceedings of SPIE de Lafontaine.2004,5418:81-93
[15]	Robert E L,George C.Monte Carlo approach to touchdown dynamics for soft lunar landing [R].NASA,1965