航空学报 > 2014, Vol. 35 Issue (2): 541-554   doi: 10.7527/S1000-6893.2013.0396

深空探测着陆器数字化设计及着陆性能影响因素

陈金宝1, 聂宏2, 万峻麟3   

  1. 1. 南京航空航天大学 航天学院, 江苏 南京 210016;
    2. 南京航空航天大学 航空宇航学院, 江苏 南京 210016;
    3. 中国电子科技集团公司第二十八研究所, 江苏 南京 210016
  • 收稿日期:2013-07-01 修回日期:2013-09-20 出版日期:2014-02-25 发布日期:2013-10-15
  • 通讯作者: 陈金宝,Tel.:025-84896516-6203 E-mail:chenjbao@nuaa.edu.cn E-mail:chenjbao@nuaa.edu.cn
  • 作者简介:陈金宝 男,博士,副教授。主要研究方向:航天器结构动力学,飞行器着陆缓冲装置设计。Tel:025-84896516-6203 E-mail:chenjbao@nuaa.edu.cn;聂宏 男,博士,教授,博士生导师。主要研究方向:飞行器着陆缓冲装置设计。Tel:025-84892411 E-mail:hnie@nuaa.edu.cn
  • 基金资助:

    国家自然科学基金(51105196);江苏省自然科学基金(BK2011733);南京航空航天大学基本科研业务费(NS2013086)

Digital Design and Landing Performance Influence Factors of Deep Space Lander

CHEN Jinbao1, NIE Hong2, WAN Junlin3   

  1. 1. College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
    2. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
    3. The Ttwenty-eighth Research Institute of China Electronic Technology Group Corporation, Nanjing 210016, China
  • Received:2013-07-01 Revised:2013-09-20 Online:2014-02-25 Published:2013-10-15
  • Supported by:

    National Natural Science Foundation of China (51105196); National Natural Science Foundation of Jiangsu (BK2011733); NUAA Fundamental Research Funds (NS2013086)

摘要:

以对称分布四腿悬架式月球着陆器为研究对象,建立了着陆器软着陆过程六自由度动力学模型并改进了月壤摩擦系数模型;在以上动力学模型基础上,以月球着陆器为例编制了着陆器软着陆六自由度动力学分析程序,利用该程序分析了探测器全机月面软着陆性能,重点研究了动力学模型中的月面等效弹性系数、月面摩擦系数和月面倾斜角度等参数对探测器着陆性能的影响。研究表明上述影响因素对着陆器着陆缓冲性能影响显著,通过对以上参数的合理选择可以有效缓解月球探测器月面软着陆的着陆冲击过载。

关键词: 着陆器, 动力学, 数字化, 月壤, 缓冲

Abstract:

Symmetrical four-legged suspension lunar lander as the research object, a six-degree-of-freedom dynamic model is established and the model of the lunar soil friction coefficient is improved. Based on the above dynamic models, six degrees of freedom dynamic analysis program on lunar lander soft-landing is applied to analyze soft-landing performance of total lunar lander. The parameters about lunar surface equivalent elastic coefficient, frictional coefficient, inclination angle and so on are studied to analyze the influence on landing performance of the lunar lander. The results show that landing and buffering performance is influenced dramatically on the above factors, and reasonable parameters are chosen to relieve effectively the impact overload of lunar lander soft-landing.

Key words: lander, dynamics, digitalization, lunar soil, buffering

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