Volume 36 Issue 3
May  2016
Turn off MathJax
Article Contents
LI Aijun, LI Jingchen, WANG Changqing, DONG Zhe. Study on Flexible Tether Critical Length at Equilibrium State[J]. Journal of Space Science, 2016, 36(3): 373-379. doi: 10.11728/cjss2016.03.373
Citation: LI Aijun, LI Jingchen, WANG Changqing, DONG Zhe. Study on Flexible Tether Critical Length at Equilibrium State[J]. Journal of Space Science, 2016, 36(3): 373-379. doi: 10.11728/cjss2016.03.373

Study on Flexible Tether Critical Length at Equilibrium State

doi: 10.11728/cjss2016.03.373
  • Received Date: 2015-03-20
  • Rev Recd Date: 2015-11-08
  • Publish Date: 2016-05-15
  • In order to determine flexible tether critical length at equilibrium,based on orbital motion of tether system,the tether equilibrium equations are established considering the atmospheric drag,tether extensibility and tether mass.Then,the load stress distribution is analyzed,and load equilibrium equations are established for determining the needed initial condition of tether equilibrium equations.Furthermore,the condition that tether length reaches critical value and the computing method of tether critical length are both given.Finally,different tether critical lengths are respectively calculated under three conditions including different load masses,tether diameters and load ballistic coefficients.Three different critical length equations are given by fitting.The impacts on critical length are analyzed under these three different conditions.

     

  • loading
  • [1]
    XU Xiujuan, CHEN Yaowu. Variation of ionospheric electron density in 100~200,km height region at low latitudes[J]. Chin. J. Space Sci., 1992, 12(4):305-312(徐秀娟, 陈耀武. 低纬100~200,km间电子数密度的变化[J]. 空间科学学报, 1992, 12(4):305-312)
    [2]
    BERRYMAN J, SCHAUB H. Static equilibrium confi-gurations in GEO Coulomb spacecraft formations[C]//AAS/AIAA Space Flight Mechanics Meeting. San Diego:American Astronautical Society, 2005
    [3]
    XU Zhongbin, JIN Dongping. Experimental study on robust control of a tethered-payload system[J]. Chin.~J. hbox Appl. Mech., 2010, 27(3):450-455(徐忠宾, 金栋平. 绳系单体系统鲁棒控制实验研究[J]. 应用力学学报, 2010, 27(3):450-455)
    [4]
    NATARAJAN A. A Study of Dynamics and Stability of Two-craft Coulomb Tether Formations[D]. Blacksburg:Virginia Polytechnic Institute and State University, 2007
    [5]
    PETTAZZI L, IZZO D. Self-assembly of large structures in space using intersatellite Coulomb forces[C]//56th International Astronautical Congress. Fukuoka:International Astronautical Federation/AIAA (IAF), 2005
    [6]
    YU Bensong. Dynamics and Control of Flexible Tethered Satellite under the Complex Space Environment[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2011(余本嵩. 复杂太空环境下柔性绳系卫星动力学与控制[D]. 南京:南京航空航天大学, 2011)
    [7]
    WILLIAMS P, TRIVAILO P. On the optimal deployment and retrieval of tethered satellites[C]//41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Tucson, Arizona:AIAA, 2005
    [8]
    RODNIKOV A V. Motion of a load along a cable fastened to a two-body-tethered spacecraft[J]. Cosm. Res., 2004, 42(4):427-431
    [9]
    MENON C, KRUIJFF M, VAVONLIOTIS A. Design and testing of a space mechanism for tether deploy-ment[J]. J. Spacecraft Rockets, 2007, 44(4):927-939. DOI:10.2514/1. 23454
    [10]
    YURIY Z. Introduction of Motion Dynamics and Control of Space Tether System[M]. Beijing:Science Publishing Company, 2013:105-115(YURIY Z. 空间系绳系统运动动力学与控制导论[M]. 北京:科学出版社, 2013:105-115)
    [11]
    ZHOU Hong, HUANG Xiancong. The performance and applications of Dyneema[J]. Hi-tech Fiber Appl., 1998, 23(5):28-35(周宏, 黄献聪. 迪尼玛(Dyneema)的性能及其应[J].高科技纤维与应用, 1998, 23(5):28-35)
    [12]
    ZHAO Hanyuan. Dynamics and Guidance of Spacecraft Reentry[M]. Changsha:National University of Defense Technology Press, 1997:16-19(赵汉元.飞行器再入动力学和制导[M]. 长沙:国防科技大学出版社, 1997:16-19)
    [13]
    WANG Xiaonan, GAO Shan, CHENG Bolin. Extraction of ballistic coefficient of smooth reentry warhead based on unscented Kalman filtering[J]. Fire Comm. Control, 2011, 36(6):89-92(王晓楠, 高山, 程柏林. 基于不敏卡尔曼滤波平滑的再入弹头弹道系数提取[J]. 火力与指挥控制, 2011, 36(6):89-92)
    [14]
    JIN Wenbin, LIU Yongxiang, LI Xiang, et al. Research on estimation of mass-to-drag ratio of reentry objects[J]. J. Natl. Univ. Defense Technol., 2004, 26(5):46-51(金文彬, 刘永祥, 黎湘, 等. 再入目标质阻比估计算法研究[J]. 国防科技大学学报, 2004, 26(5):46-51)
  • 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

    Article Metrics

    Article Views(898) PDF Downloads(1042) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return