Optics and Precision Engineering, Volume. 22, Issue 3, 745(2014)

Dynamic simulation and application of deployable mechanism of satellite solar panels

JIN Guang1... XIE Xiao-guang1,2,*, GU Song1 and ZHANG Di3 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    References(13)

    [1] [1] HOKER W.A set r-dynamics attitude equations for an N-body satellite having roational degrees of freedon [J].AIAA.J., 1970, 8(7): 1205-1209.

    [2] [2] CHEN L M.Analysis of deployment motion of satellite solar wing[J].Chinese Space Science and Technology, 1992, 12(2): 21-26.(in Chinese)

    [3] [3] Deployment Analysis[R].MBB Tethnical Report.D3SA-AN-1000-8g-01A.1990.

    [4] [4] SUN J D.Design and Analysis of Satellite Structure[M].Beijing: Yu Hang Publishing Company, 2004.(in Chinese)

    [5] [5] XU F X.Introduction of Satellite Engineering[M].Beijing: Yu Hang Publishing Company, 2003.(in Chinese)

    [6] [6] CHEN L M, ZHAO J CH.Universal standard of satellite solar array [S].National Standard for Military Use, GJB 4083-2000.(in Chinese)

    [7] [7] GUO F, HUANG ZH H, DENG Y M.Test simulation of deployment motion of satellite solar array using ADAMS [J].Machinery Desing and Manufacture, 2004, 8(4): 71-73.(in Chinese)

    [8] [8] SUN J.Parameter design of solar wing hinge spiral spring [J].Spacecraft Engineering, 2000, 9(3): 37-43.(in Chinese)

    [9] [9] LIU J Y, HONG J ZH.Dynamic analysis of spacecraft deployable mechanism with contact impact[J].Journal of Astronautic, 1997, 18(2): 19-25.(in Chinese)

    [10] [10] STEFAN V D.Analysis of large flexible body deformation in multibody system using absolute coordinates[J].Multibody System Dynamics (S1384-5640), 2002, 8: 409-432.

    [11] [11] WANG Y ZH, GU Y H.Influence analysis for the characteristics of the solar panes hinge[J].Journal of Suzhou University: Engineering Science Edition, 2010, 30(3): 22-25.(in Chinese)

    [12] [12] AN Y, GU S, JIN G.Analysis and simulation of deployment of satellite solar array[J].Chiense Journal Optics and Applied Optics, 2000, 2(1): 29-35.(in Chinese)

    CLP Journals

    [1] HUANG Tie-qiu, MO Yi-hua, WANG Jiang. Quickest deployable curve of linear-rotary actuator[J]. Optics and Precision Engineering, 2015, 23(6): 1642

    [2] XUAN Ming, ZHANG Dao-wei, GU Song, YANG Lin, CHENG Long. Design of hold-down and release mechanism for solar panel of micro-satellite[J]. Optics and Precision Engineering, 2017, 25(4): 979

    [3] XU Wei, JIN Guang, WANG Jia-qi. Optical imaging technology of JL-1 lightweight high resolution multispectral remote sensing satellite[J]. Optics and Precision Engineering, 2017, 25(8): 1969

    [4] HAN Xue-feng, LIU Xiao-dong, MA Wu-yuan, MA Qing, YUAN Dong-ming. Optimization and experiments of deployment performance for folding wing mechanism of an aircraft[J]. Optics and Precision Engineering, 2016, 24(9): 2262

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    JIN Guang, XIE Xiao-guang, GU Song, ZHANG Di. Dynamic simulation and application of deployable mechanism of satellite solar panels[J]. Optics and Precision Engineering, 2014, 22(3): 745

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    Paper Information

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    Received: May. 15, 2013

    Accepted: --

    Published Online: Apr. 24, 2014

    The Author Email: Xiao-guang XIE (7801046ab@163.com)

    DOI:10.3788/ope.20142203.0745

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