Advanced Search
Volume 38 Issue 2
Feb.  2012
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (2): 185-190.
WU Cun-hao, YANG Jia-ling, ZANG Shu-guang, et al. Study of Bird Impact Loading Model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(3): 332-335. (in Chinese)
Citation: Luo Songbai, Zhao Yongjia. Dynamic analysis and simulation of soft-landing for lunar lander[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (2): 185-190. (in Chinese)
shu

Dynamic analysis and simulation of soft-landing for lunar lander

  • School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 10 Nov 2010
  • Publish Date: 29 Feb 2012
    Abstract
  • Taking the four-leg lunar lander as the study object, the lander's component structure and lunar physical attribute was analyzed. When studying the lander's dynamics, a block parameter simulation method based on structure was proposed, which analyzes the lander's dynamic behavior during the landing moment, derives the buffers' and foot pads' dynamic model individually and integrates each model through simplifying lander's structure. Technology of visual simulation was introduced and simulation of lunar-landing was realized. The effects of different initial conditions, such as slop of lunar surface and lading velocity, stiffness coefficient and damping coefficient were measured through simulation. The result verifies the validity of the method. This method has already successfully applied in engineering research of lunar-landing.

     

    • FullText(HTML)
    • References(9)
  • [1]
    Hilderman R A,Mantus M,Lerner E.Landing dynamics of the lunar excursion module(method of analysis) .AIAA-66A-42771,1966
    [2]
    王少纯,邓宗全,高海波,等.微小型月球着陆器冲击隔离着陆腿研究[J].哈尔滨工业大学学报,2004,36(2):180-182 Wang Shaochun,Deng Zongquan,Gao Haibo,et al.Design of impact isolating landing legs for micro-miniature lunar lander[J].Journal of Harbin Institute of Technology,2004,36(2):180-182(in Chinese)
    [3]
    Thompson W C.Dynamic model investigation of the rough-water landing characteristics of a spacecraft .AIAA Paper-67-23281,1967
    [4]
    蒋万松,黄伟,王海涛.ADAMS用户子程序在软着陆动力学仿真中的应用[J].航天返回与遥感,2009,30(4):11-18 Jiang Wansong,Huang Wei,Wang Haitao.Application of DAMS user-written subroutine to simulation of soft-landing dynamics[J].Spacecraft Recovery and Remote Sensing,2009,30(4):11-18(in Chinese)
    [5]
    Jooahn L,John C.Lunar lander conceptual design[M].US:NASA,1989
    [6]
    陈金宝,聂宏,赵金才.月球探测器软着陆缓冲机构关键技术研究进展[J].宇航学报,2008,29(3):731-735 Chen Jinbao,Nie Hong,Zhao Jincai.Review of the development of soft-landing buffer for lunar explorations [J].Journal of Astronautics,2008,29(3):731-735 (in Chinese)
    [7]
    胡亚冰,孙毅.月球探测器软着陆机构[J].上海航天,2010(1):43-50 Hu Yabing,Sun yi.Soft lander of lunar lander[J].Aerospace Shanghai,2010(1):43-50(in Chinese)
    [8]
    张文斌,周晓军.液压缓冲器特性计算与仿真分析[J].农业机械学报,2008,39(7):164-168 Zhang Wenbin,Zhou Xiaojun.Simulation and characteristic analysis of hydraulic bumper[J].Transactions of the Chinese Society of Agricultural Machinery,2008,39(7):164-168(in Chinese)
    [9]
    Russell Smith.Open dynamics engine .
    • Relative Articles

  • Relative Articles

    [1]QIN H L，ZHANG Y，SHI G T，et al. Doppler positioning technology based on Globalstar opportunity signals[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：360-367 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0013.
    [2]DENG C J，CHEN Q J，ZHANG T S，et al. NHC lever arm estimation algorithm for vehicle-integrated navigation systems based on dead reckoning[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：668-675 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0035.
    [3]HOU Z Q，MA J Y，HAN R X，et al. A fast long-term visual tracking algorithm based on deep learning[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2391-2403 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0645.
    [4]ZHANG Anqi, CAO Ronggang, ZHOU Yu, LI Jiawu, CAO Yuxi, YU Yongbin. Research on Fast and High Precision Signal Processing Method for FM Fuze Based on 2D-FFT and 2D-CFAR[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0827
    [5]WANG Haipeng, LIU Haina, WANG Zhendong, MOU Cunxiao, ZHANG He, YE Wen. Pod integrated navigation system elastic lever arm error compensation method[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0155
    [6]XU J M，HUANG Z G，LI R. LEO satellite positioning method and simulation verification aided by airborne navigation equipment[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3230-3238 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0759.
    [7]CHEN X M，ZHU Y C，LING J，et al. Energy-efficiency characteristic investigation of rotational inertia hydraulic converter[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1982-1990 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0570.
    [8]WU Hao, LIU Meng, WANG Jun. Effect of balance chamber on rapid pressure regulation ability of outflow valve[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0248
    [9]ZHOU B J，YU C Q，TAN L L，et al. Fast leveling control technology of vehicle platform based on interference compensation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1495-1503 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0447.
    [10]CHENG Z Y，YANG Y X，ZHANG X C，et al. Rapid evaluation method for aerodynamic characteristics of distributed electric propulsion aircraft concept scheme[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3047-3058 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0771.
    [11]ZHANG Q S，LIU T T，HAO C L，et al. Rapid detection analysis method of thermal runaway gas composition and risk of lithium ion battery[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2227-2233 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0668.
    [12]XING Xiao-bing, TAN Jian-feng, YANG Yu-xiao, YONG Tian, YU Ling-jun, WU Rui. An efficient analysis method of helicopter fuselage bullet damage based on bullet penetration theory[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0450
    [13]WANG Z X，WAN Z Q，WANG X Z，et al. Fast stability analysis method for composite panel with variable angle tow fiber[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：353-366 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0259.
    [14]LEI Lu, WU Ming-yu, GUO Zhi-bo, QIAO Xiao-li. Research on fast sign-off method for wiring harness topological drawings[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0427
    [15]BAN Huan-heng, ZHOU Cong, YAN Xiao-dong. Rapid Trajectory Planning Method for Lunar Direct Ascent and Rendezvous under Emergency Condition[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0160
    [16]ZHANG P，ZHOU Q X，YU H Q，et al. Fast detection method of mental fatigue based on EEG signal characteristics[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（1）：145-154 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0211.
    [17]XIE C C，ZHANG D Y，AN C. Reduced order method for large flexible wing structure based on dynamic response data[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1319-1330 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0439.
    [18]CHEN Qingyang, XIN Hongbo, WANG Yujie, TANG Zhongnan, JIA Gaowei, ZHU Bingjie. A rapid path planning method for multiple UAVs to cooperative strike[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1145-1153. doi: 10.13700/j.bh.1001-5965.2021.0022
    [19]SU Donglin, CUI Shuo, BAI Jiangfei, LI Yaoyao. Fast prediction method for radiated and scattered coupled fields in complex electromagnetic environment[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1553-1560. doi: 10.13700/j.bh.1001-5965.2022.0705
    [20]LI Wenxuan, JIAO Wenhai, WANG Kai, QIU Ruijin, SUN Shuxian. Monitoring and analysis on GPS P(Y) code power enhancement[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2193-2203. doi: 10.13700/j.bh.1001-5965.2021.0676
    • 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(2691) PDF downloads(703) 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