Advanced Search
Volume 39 Issue 1
Jan.  2013
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2013  >  (1): 11-15.
Zhang Pengfei, Cheng Wei, Zhao Yuet al. Measure of reaction wheels disturbance considering coupling effect[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(8): 948-952. (in Chinese)
Citation: Liang Dongping, Chai Hongyou, Zeng Fuminget al. Nonlinear finite element modeling and simulation for landing leg of lunar lander[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, (1): 11-15. (in Chinese)
shu

Nonlinear finite element modeling and simulation for landing leg of lunar lander

  • Beijing Institute of Spacecraft System Engineering, Beijing 100094, China

  • Received Date: 08 Oct 2011
  • Publish Date: 31 Jan 2013
    Abstract
  • In order to accurately predict the load attenuation and energy absorption capabilities of landing leg during the landing event for supporting the design and optimization of landing gear mechanism, a new approach of using nonlinear finite element method in landing impact dynamic analysis was proposed. A detailed finite element model of landing leg was constructed and ABAQUS/Explicit was selected as the solver. Mass scaling technique was used to increase computational efficiency. Landing dynamic simulation of two landing scenarios were carried out, and the validity of analysis results were verified by comparison with test data. Results indicate that nonlinear finite element model with varied nonlinear factors can predict the landing performance of landing leg precisely. The flexibility of landing leg has a great effect on the friction between the inner and outer cylinders of leg struts, and the friction force can be decreased by increasing the leg stiffness.

     

    • FullText(HTML)
    • References(9)
  • [1]
    William F R.Apollo experience report-lunar module landing gear subsystem.NASA TN D-6850,1972
    [2]
    Merchant D H,Sawdy D T.Monte Carlo dynamic analysis for lunar module landing loads[J].Journal of Spacecraft and Rockets,1970,8(1):48-55
    [3]
    Doiron H H,George A Z.Apollo lunar module landing dynamics//The 41st Structures,Structural Dynamics,and Materials Conference and Exhibit.Washington:AIAA/ASME/ASCE/AHS/ASC,2000
    [4]
    Andrew L B,James R C,Ralph D L,et al.Planetary landers and entry probes[M].New York:Cambridge University Press,2007
    [5]
    Masahiro N,Akira M.Modeling for lunar lander by mechanical dynamics software//Modeling and Simulation Technologies Conference and Exhibit.Washington:AIAA,2005
    [6]
    Hilchenbach M,Kuchemann O,Rosenbauer H.Impact on a comet:Rosetta lander simulations[J].Planetary and Space Science,2000,48(5):361-369
    [7]
    朱汪,杨建中.月球探测器软着陆机构着陆腿模型与仿真分析[J].宇航学报,2008,29(6):1723-1728
    Zhu Wang,Yang Jianzhong.Modeling and simulation of landing leg for lunar landing gear system [J].Journal of Astronautics,2008,29(6):1723-1728(in Chinese)
    [8]
    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)
    [9]
    杨艳静.模拟月壤和月球车车轮相互作用的数值仿真和试验研究.北京:中国空间技术研究院,2010
    Yang Yanjing.Numerical and experimental research of lunar soil stimulant and lunar rover wheel interaction.Beijing:China Academy of Space Technology,2010(in Chinese)
    • Relative Articles

  • Relative Articles

    [1]TIAN D K，ZHANG J W，JIN L，et al. Design and analysis of morphing wing mechanism based on equilateral Bennett mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：742-752 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0139.
    [2]XIONG F，LI Q，LI J，et al. Time-triggered traffic scheduling-oriented virtual network embedding method[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1982-1990 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0511.
    [3]YANG X X，JIANG Z J，ZHANG Y，et al. Distributed cooperative guidance strategy based on virtual negotiation and rolling horizon optimization[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：61-76 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0174.
    [4]GENG Z T，ZHAO J Q. Design and development of virtual simulation experiment software of composite piezoelectric materials[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3377-3381 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0826.
    [5]GENG Z W，ZHANG J，KONG N，et al. Design and analysis of space repeatable mechanical locking and electromagnetic unlocking mechanisms[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3947-3956 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0918.
    [6]LI Y，ZHANG X X，SUN F Q，et al. Belief reliability modeling for assembly accuracy of spaceborne SAR antenna deployable mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：134-143 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0234.
    [7]TIAN Xinyu, WANG Shaoping, WANG Xingjian, ZHANG Yuwei, WEI Yi. Ankle prosthesis control method inspired by central pattern generator[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0665
    [8]LIN Jun-ting, NI Ming-jun. Adaptive model predictive control of virtual coupled based on artificial potential field[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0544
    [9]WANG Y L，FENG S，BU C，et al. Stability characteristics of hybrid wing-body aircraft based on virtual flight[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2337-2344 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0684.
    [10]ZHANG Yang, QIN Ning-ning. Dual-Dimensional Partition Localization Algorithm Under AP Virtual Location Perception[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0274
    [11]ZHANG Z，WANG P，ZHOU H Y. Reliability analysis of nozzle adjustment mechanism with interval distribution parameters[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3377-3385 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0089.
    [12]HE T Y，DONG Y，WANG H，et al. Design and optimization of modular parabolic deployable mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2473-2481 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0652.
    [13]YANG Z J，WANG G，ZHAO R J，et al. Dynamic analysis of deployment impact of trim-wing mechanism of Mars entry capsules[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：422-429 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0234.
    [14]ZHANG Y X，WANG X J，WANG S P，et al. Mechanism of butterfly forward flight and prototype verification based on characteristic motion observation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1651-1660 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0497.
    [15]YANG Yi-feng, WANG Yi, LIU Ao-yu, LI Jia, XIE Li-yang. Calculation and error analysis of kinematic accuracy reliability of VSV adjustment mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0410
    [16]HE L T，FANG H R，CHEN Y F，et al. Design and performance analysis of spatial large extension parallel mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1722-1734 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0548.
    [17]DU Xianchen, LIU Xue'ao, DONG Yang, WANG Hui, HE Tianyu, WANG Chunjie. Design and dimensional synthesis of a variable wing sweep mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2502-2509. doi: 10.13700/j.bh.1001-5965.2021.0125
    [18]NIE Liangyi, DING Huafeng, WANG Jun, BI Shusheng. Branch graph method for crank judgement of complex multi-loop linkage[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1863-1874. doi: 10.13700/j.bh.1001-5965.2021.0152
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2083) PDF downloads(1004) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return