Volume 39 Issue 5
Sep.  2019
Turn off MathJax
Article Contents
Article Navigation >  Chinese Journal of Space Science  > 2019  >  39(5): 684-693
HAN Wei, JIANG Zhijie, HUANG Yiyong, CHEN Xiaoqian. Research on Rigid-flexible Coupling Dynamics of Flexible Cone-probe Docking Mechanism[J]. Chinese Journal of Space Science, 2019, 39(5): 684-693. doi: 10.11728/cjss2019.05.684
Citation: HAN Wei, JIANG Zhijie, HUANG Yiyong, CHEN Xiaoqian. Research on Rigid-flexible Coupling Dynamics of Flexible Cone-probe Docking Mechanism[J]. Chinese Journal of Space Science, 2019, 39(5): 684-693. doi: 10.11728/cjss2019.05.684
shu

Research on Rigid-flexible Coupling Dynamics of Flexible Cone-probe Docking Mechanism

doi: 10.11728/cjss2019.05.684 cstr: 32142.14.cjss2019.05.684

  • National Innovation Institute of Defense Technology, Academy of Military Sciences, Beijing 100071

Funds:

Supported by the National Natural Science Foundation of China (91216201, 11725211)

More Information
  • Author Bio:

    HAN Wei,15211132998@163.com

  • Received Date: 2018-10-10
  • Rev Recd Date: 2019-03-04
  • Publish Date: 2019-09-15
    Abstract
  • In this paper,a new kind of flexible cone composed of the thin-walled plates based on space probe-cone docking mechanism for small-sized spacecraft is presented.The theoretical model of docking impact dynamics,which takes into account the additional stiffness terms,is derived based on Lagrange Analytical Mechanics theory and Hertz contact theory.Finite element method is employed for the discretization of the thin-walled plate.The results show that the traditional dynamic model without considering the additional stiffness terms will be difficult to reach steady state.The method proposed in this paper can correctly predict the dynamic behavior of the system.

     

    • FullText(HTML)
  • loading
    • References(21)
  • [1]
    PHILIP N K, ANANTHASAYANAM M R. Relative position and attitude estimation and control schemes for the final phase of an autonomous docking mission of spacecraft[J]. Acta Astronaut., 2003, 52:511-522
    [2]
    LAMASSOURE E, SALEH J H, HASTINGS D E. Space systems flexibility provided by on-orbit servicing:part 2[J]. J. Spacecraft Rockets, 2002, 39:561-570
    [3]
    KAWANO I, MOKUNO M, KASAI T, et al. Result of autonomous rendezvous and docking experiment of engineering test satellite-VⅡ[J]. AIAA J. Spacec. Rockets, 2001, 38:105-111
    [4]
    HAYS A B, TCHORYK P, PAVLICH J C, et al. Advancements in design of an autonomous satellite docking system[J]. SPIE, 2004, 5419:107-118
    [5]
    FEHSE W. Automated Rendezvous and Docking of Spacecraft[M]. Cambridge:Cambridge University Press, 2003
    [6]
    WIERZBIZKI T, NURICK GN. Large deformation of thin plates under localized impulsive loading[J]. Int. J. Impact Eng., 1996, 18:899-918
    [7]
    LIU Z S, LEE H P, LU C. Structural intensity study of plates under low-velocity impact[J]. Int. J. Impact Eng., 2005, 31:957-975
    [8]
    LIDÉN E, JOHANSSON B, LUNDBERG B. Effect of thin oblique moving plates on long rod projectiles:a reverse impact study[J]. Int. J. Impact Eng., 2006, 32:1696-1720
    [9]
    ABDULHAMID H, KOLOPP A, BOUVET C, et al. Experimental and numerical study of AA5086-H111 aluminum plates subjected to impact[J]. Int. J. Impact Eng., 2013, 51:1-12
    [10]
    YOO H H, CHUNG J. Dynamics of rectangular plates undergoing prescribed overall motion[J]. J. Sound Vib., 2001, 239(1):123-137
    [11]
    CAI G P, HONG J Z, YANG S X. Model study and active control of a rotating flexible cantilever beam[J]. Int. J. Mech. Sci., 2004, 46:871-889
    [12]
    LIU J Y, HONG J Z. Geometric stiffening effect on rigid-flexible coupling dynamics of an elastic beam[J]. J. Sound Vib., 2004, 278:1147-1162
    [13]
    YANG H, HONG J Z, YU Z Y. Dynamics modeling of a flexible hub-beam system with a tip mass[J]. J. Sound Vib., 2003, 266:759-774
    [14]
    LIU J Y, HONG J Z. Geometric nonlinear formulation and discretization method for a rectangular plate undergoing large overall motions[J]. Mech. Res. Commun., 2005, 32:561-571
    [15]
    HERTZ H. Über die Berührung fester elastischer Körper[J]. J. Reine Angew. Math., 1881, 92:156-171
    [16]
    JOHNSON K L. Contact Mechanics[M]. Cambridge:Cambridge University Press, 1999
    [17]
    YIGIT A S, ULSOY A G, SCOTT R A. Spring-dashpot models for the dynamics of a radially rotating beam with impact[J]. J. Sound Vib., 1990, 142:515-525
    [18]
    LANKARANI H M, NIKRAVESH P E. A contact force model with hysteresis damping for impact analysis of multibody systems[J]. ASME J. Mech. Design, 1990, 112:369-375
    [19]
    GILARDI G, SHARF I. Literature survey of contact dynamics modeling[J]. Mech. Mach. Theory, 2002, 37:1213-1239
    [20]
    MACHADO M, MOREIRA P, FLORES P, et al. Compliant contact force models in multibody dynamics:evolution of the Hertz contact theory[J]. J. Mech. Mach. Theory, 2012, 53:99-121
    [21]
    HAN W, HUANG Y Y, CHEN X Q, et al. Flexible cone impact dynamics based on space probe-cone docking mechanism[J]. Sci. China Phys.:Mech. Astron., 2014, 57:128-137
    • Relative Articles
    • 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(1088) PDF Downloads(100) Cited by()
    Proportional views
    Related

    Journal Introduction

    ISSN 0254-6124       CN 11-1783/V

    Copyright © Editorial Office of Chinese Journal of Space Science.  京ICP备08100722号

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

    x Close Forever Close

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return