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Duan Liucheng, Li Haiquan, Liu Xiaofeng, Cai Guoping. DEPLOYMENT DYNAMICS OF FLEXIBLE SOLAR ARRAYS CONSIDERING FRICTIONAL JOINT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2014, 46(6): 957-970. doi: 10.6052/0459-1879-14-152
Citation: Duan Liucheng, Li Haiquan, Liu Xiaofeng, Cai Guoping. DEPLOYMENT DYNAMICS OF FLEXIBLE SOLAR ARRAYS CONSIDERING FRICTIONAL JOINT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2014, 46(6): 957-970. doi: 10.6052/0459-1879-14-152


doi: 10.6052/0459-1879-14-152
Funds:  The project was supported by the Natural Science Foundation of China (11132001, 11272202), the Aviation Science Foundation of China (20120157002) and the Key Project of Shanghai Scientific Research (14ZZ021).
  • Received Date: 2014-05-30
  • Rev Recd Date: 2014-08-11
  • Publish Date: 2014-11-18
  • The deployment and locking of solar arrays of a free-floating spacecraft is studied in this paper. The rigid-flexible coupling dynamic model for describing the deployment and locking process is established using the Jourdain's velocity variational principle and the approach of forward recursive formulation. The contribution of joint friction to the dynamic equation of the system is derived based on the virtual power principle. The 3-D bristle friction model is introduced to study the influence of joint friction on the deployment dynamics of solar arrays. The validity of the proposed model is verified through the comparison of simulation results with those using the commercial software ADAMS and NASTRAN, and this model is available for predicting the deployment process of solar arrays and the attitude motion of spacecraft.


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  • Kuang JL, Meehan PA, Leung AYT, et al. Nonlinear dynamic of a satellite with deployable solar panels. International Journal of Non-Linear Mechanics, 2004, 39(7): 1161-1179  
    Gao EW, Zhang XP, Yao ZQ. Simulation and analysis of flexible solar panels' deployment and locking processes. Journal of Shanghai Jiaotong University, 2008, 13(3): 275-279  
    Wie B, Furumoto N, Banerjee AK, et al. Modeling and simulation of spacecraft solar array deployment. Journal of Guidance, Control, and Dynamics, 1986, 9(5): 593-598  
    Oskar W, Simon W. Simulation of deployment of a flexible solar array. Multibody System Dynamics, 2002, 7: 101-125  
    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. 机械设计与制造, 2004, 4: 71-72 (Guo Feng, Huang Zhenhua, Deng Yangming. Test simulation of deployment motion of satellite solar array using ADAMS. Machinery Design and Manufacture, 2004, 4: 71-72(in Chinese))
    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. 系统仿真学报, 2009, 21(13): 3975-3979 (Bai Zhengfeng, Tian Hao, Zhao Yang. Dynamics simulation of deployment of solar panels in different layouts based on ADAMS. Journal of System Simulation, 2009, 21(13): 3975-3979(in Chinese))
    游斌弟, 王兴贵, 陈军. 卫星太阳阵展开锁紧过程冲击振动. 机械工程学报, 2012, 48(21): 67-76 (You Bindi, Wang Xinggui, Chen Jun. Vibration and impact for deployable solar array of satellite with locking hinges. Journal of Mechanical Engineering, 2012, 48(21): 67-76(in Chinese))
    Birhanu F, Chen ZB, Ma WS. Modeling simulation of satellite solar panel deployment and Locking. Information Technology Journal, 2010, 9(3): 600-604  
    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. 机械设计与制造, 2006, 11: 124-126 (Bai Zhengfeng, Tian Hao, Zhao Yang. Dynamics simulation of deployment and locking of spacecraft solar panel using ADAMS. Machinery Design and Manufacture, 2006, 11: 124-126(in Chinese))
    吴爽, 赵寿根, 吴大方 等. 太阳翼铰链结构的动力学试验与非线性动力学建模. 宇航学报, 2013, 34(12): 1550-1556 (Wu Shuang, Zhao Shougen, Wu Dafang, et al. Dynamic experiments and nonlinear dynamics modeling of joints in solar array. Journal of Astronautics, 2013, 34(12): 1550-1556(in Chinese))
    Li JL, Yan SZ, Guo F, et al. Effects of damping, friction, gravity, and flexibility on the dynamic performance of a deployable mechanism with clearance. Journal of Mechanical Engineering Science, 2013, 227(8): 1791-1803  
    王天舒, 孔宪仁, 王本利 等. 太阳帆板绳索联动同步机构的机理和功能分析. 宇航学报, 2001, 21(3): 29-33 (Wang Tianshu, Kong Xianren, Wang Benli, et al. The research on principle and function of closed loop configuration of solar arrays. Journal of Astronautics, 2001, 21(3): 29-33(in Chinese))
    Daniel WK. Techniques for using ADAMS in spacecraft applications. ADAMS: Mechanical dynamics-customer service. In: Proc. of 16th European MDI User Conference, Berchtesgaden, Germany, 2001
    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. 航天器工程, 2011, 20(3): 86-92 (Wang Xian, Chen Tianzhi, Chai Hongyou. Dynamics simulation analysis of solar array ground deployment and locking. Spacecraft Engineering, 2011, 20(3): 86-92(in Chinese))
    罗晓明. 多体系统中铰内摩擦接触分析.[博士论文]. 大连: 大连理工大学, 2011 (Luo Xiaoming. Frictional contact analysis of joints in multi-body system [PhD Thesis]. Dalian: Dalian University of Technology, 2011(in Chinese))
    Liang JX, Fillmore S, Ma O. An extended bristle friction force model with experimental validation. Mechanism and Machine Theory, 2012, 56: 123-137  
    Haessig DA, Friedland B. On the modeling and simulation of friction. Journal of Dynamic Systems, Measurement, and Control, 1991, 113(3): 354-362  
    洪嘉振. 计算多体系统动力学. 北京: 高等教育出版社, 2003 (Hong Jiazhen. Computational Dynamics of Multibody Systems. Beijing: High Education Press, 1999(in Chinese))
    李东旭. 挠性航天器结构动力学. 北京: 科学出版社, 2010(Li Dongxun. Structural Dynamics of Flexible Spacecraft. Beijing: Science Press, 2010(in Chinese))
    刘澜涛. 太阳能帆板关节展开机构的设计与实现.[硕士论文]. 上海: 上海交通大学, 2013 (Liu Lantao. Design and realization of the joint deployment mechanism oriented to solar panels [Master Thesis]. Shanghai: Shanghai Jiaotong University, 2013(in Chinese))
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