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考虑铰摩擦的太阳翼展开动力学研究

段柳成 李海泉 刘晓峰 蔡国平

段柳成, 李海泉, 刘晓峰, 蔡国平. 考虑铰摩擦的太阳翼展开动力学研究[J]. 应用数学和力学, 2014, 35(12): 1308-1319. doi: 10.3879/j.issn.1000-0887.2014.12.003
引用本文: 段柳成, 李海泉, 刘晓峰, 蔡国平. 考虑铰摩擦的太阳翼展开动力学研究[J]. 应用数学和力学, 2014, 35(12): 1308-1319. doi: 10.3879/j.issn.1000-0887.2014.12.003
DUAN Liu-cheng, LI Hai-quan, LIU Xiao-feng, CAI Guo-ping. Deployment Dynamics for Solar Wings With Joint Friction[J]. Applied Mathematics and Mechanics, 2014, 35(12): 1308-1319. doi: 10.3879/j.issn.1000-0887.2014.12.003
Citation: DUAN Liu-cheng, LI Hai-quan, LIU Xiao-feng, CAI Guo-ping. Deployment Dynamics for Solar Wings With Joint Friction[J]. Applied Mathematics and Mechanics, 2014, 35(12): 1308-1319. doi: 10.3879/j.issn.1000-0887.2014.12.003

考虑铰摩擦的太阳翼展开动力学研究

doi: 10.3879/j.issn.1000-0887.2014.12.003
基金项目: 国家自然科学基金(11132001;11272202);航空科学基金(20120157002);高等学校博士学科点专项科研基金(20110073110008);上海市教委科研重点项目(14ZZ021)
详细信息
    作者简介:

    段柳成(1989—),男,湖南人,硕士生(Tel: +86-21-34204413; E-mail: sjtudlc@sjtu.edu.cn);蔡国平(1965—),男,河南人,教授,博士,博士生导师(通讯作者. Tel: +86-21-34204798;E-mail: caigp@sjtu.edu.cn).

  • 中图分类号: O313.7; V412.4+2

Deployment Dynamics for Solar Wings With Joint Friction

Funds: The National Natural Science Foundation of China(11132001; 11272202)
  • 摘要: 研究了空间漂浮航天器太阳翼的展开动力学与控制问题.采用单项递推组集方法建立了太阳翼展开与锁定过程的动力学模型,利用虚功率原理推导了铰摩擦对系统动力学方程的贡献,通过补充含摩擦铰物体的系统动平衡方程构建了系统封闭的动力学方程.通过与ADAMS软件仿真结果的对比,验证了所建模型的正确性.研究结果显示,所建模型能够有效地对太阳翼的展开过程进行描述,铰摩擦会对系统的动力学行为产生影响,PD控制方法能够较好地抑制太阳翼展开所引起的航天器的姿态漂移.
  • [1] Wie B, Furumoto N, Banerjee A K, Barba P M. Modeling and simulation of spacecraft solar array deployment[J]. Journal of Guidance, Control, and Dynamics,1986,9(5): 593-598.
    [2] 周志成, 曲广吉. 航天器太阳阵多体展开的动力学分析[J]. 力学与实践, 1990,12(6): 53-57.(ZHOU Zhi-cheng, QU Guang-ji. Deployment analysis of spacecraft solar array[J]. Mechanics in Engineering,1990,12(6): 53-57.(in Chinese))
    [3] Oskar W, Simon W. Simulation of deployment of a flexible solar array[J]. Multibody System Dynamics,2002,7(1): 101-125.
    [4] 郭峰, 黄振华, 邓扬明. 基于ADAMS航天器刚性太阳帆板动力学仿真分析[J]. 机械设计与制造, 2004(4): 71-72. (GUO Feng, HUNG Zhen-hua, DENG Yang-ming. Test simulation of deployment motion of satellite solar array using ADAMS[J]. Machinery Design and Manufacture,2004(4): 71-72.(in Chinese))
    [5] 白争锋, 田浩, 赵阳. 基于ADAMS航天器太阳帆板展开与锁定动力学仿真[J]. 机械设计与制造, 2006(11): 124-126. (BAI Zheng-feng, TIAN Hao, ZHAO Yang. Dynamics simulation of deployment and locking of spacecraft solar panel using ADAMS[J]. Machinery Design and Manufacture,2006(11): 124-126. (in Chinese))
    [6] Yasushi K, Shigemune T, Yoshiaki O. Dynamic simulation of stick-slip motion of a flexible solar array[J]. Special Section on Large Scale Systems,2008,16(6): 724-735.
    [7] Birhanu F, Chen Z B, Ma W S. Modeling simulation of satellite solar panel deployment and locking[J]. Information Technology Journal,2010, 9(3): 600-604.
    [8] 王晛, 陈天智, 柴洪友. 太阳翼地面展开锁定的动力学仿真分析[J]. 航天器工程, 2011,20(3): 86-92.(WANG Xian, CHEN Tian-zhi, CHAI Hong-you. Dynamics simulation analysis of solar array ground deployment and locking[J]. Spacecraft Engineering,2011,20(3): 86-92.(in Chinese))
    [9] 游斌弟, 王兴贵, 陈军. 卫星太阳阵展开锁紧过程冲击振动[J]. 机械工程学报, 2012,48(21): 67-76.(YOU Bin-di, WANG Xing-gui, CHEN Jun. Vibration and impact for deployable solar array of satellite with locking hinges[J]. Journal of Mechanical Engineering,2012,48(21): 67-76.(in Chinese))
    [10] 吴爽, 赵寿根, 吴大方, 罗敏. 太阳翼铰链结构的动力学试验与非线性动力学建模[J]. 宇航学报, 2013,34(12): 1550-1556.(WU Shuang, ZHAO Shou-gen, WU Da-fang, LUO Min. Dynamic experiments and nonlinear dynamics modeling of joints in solar array[J]. Journal of Astronautics,2013,34(12): 1550-1556.(in Chinese))
    [11] Li J L, Yan S Z, Guo F, Guo P F. Effects of damping, friction, gravity, and flexibility on the dynamic performance of a deployable mechanism with clearance[J]. Proceedings of the Institution of Mechanical Engineers, Part C, Journal of Mechanical Engineering Science,2013,227(8): 1791-1803.
    [12] 肖宁聪, 李彦锋, 黄洪钟. 卫星太阳翼展开机构的可靠性分析方法研究[J]. 宇航学报, 2009,30(4): 1704-1710.(XIAO Ning-cong, LI Yan-feng, HUANG Hong-zhong. Reliability analysis method of deployment mechanism of a satellite solar arrays[J]. Journal of Astronautics,2009,30(4): 1704-1710.(in Chinese))
    [13] 王天舒, 孔宪仁, 王本利, 马兴瑞. 太阳帆板绳索联动同步机构的机理和功能分析[J]. 宇航学报, 2001,21(3): 29-33.(WANG Tian-shu, KONG Xian-ren, WANG Ben-li, MA Xing-rui. The research on principle and function of closed loop configuration of solar arrays[J]. Journal of Astronautics,2001,21(3): 29-33.(in Chinese))
    [14] 白争锋, 田浩, 赵阳. 基于虚拟样机的太阳帆板展开动力学仿真[J]. 系统仿真学报, 2009,21(13): 3975-3979.(BAI Zheng-feng, TIAN Hao, ZHAO Yang. Dynamics simulation of deployment of solar panels in different layouts based on ADAMS[J]. Journal of System Simulation,2009,21(13): 3975-3979.(in Chinese))
    [15] 梁小光, 陈照波. 阻尼器对卫星太阳翼锁定冲击力矩影响的研究[J]. 噪声与振动控制, 2011,31(1): 127-130.(LIANG Xiao-guang, CHEN Zhao-bo. Study on influence of damper on locking wallop of deployable solar array of satellite[J]. Noise and Vibration Control,2011,31(1): 127-130.(in Chinese))
    [16] Daniel W K. Techniques for using ADAMS in spacecraft applications[C]// ADAMS: Mechanical Dynamics-Customer Service, 16th European MDI User Conference. Berchtesgaden, Germany, 2001.
    [17] 罗晓明. 多体系统中铰内摩擦接触分析[D]. 博士学位论文. 大连: 大连理工大学, 2011.(LUO Xiao-ming. Frictional contact analysis of joints in multibody system[D]. PhD Thesis. Dalian: Dalian University of Technology, 2011.(in Chinese))
    [18] BAI Zheng-feng, ZHAO Yang, CHEN Jun. Dynamics analysis of planar mechanical system considering revolute clearance joint wear[J]. Tribology International,2013,64: 85-98.
    [19] 洪嘉振. 计算多体系统动力学[M]. 北京: 高等教育出版社, 2003.(HONG Jia-zhen. Computational Dynamics of Multibody Systems [M]. Beijing: Higher Education Press, 2003.(in Chinese))
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出版历程
  • 收稿日期:  2014-06-06
  • 修回日期:  2014-10-11
  • 刊出日期:  2014-12-15

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