• Optics and Precision Engineering
  • Vol. 28, Issue 7, 1539 (2020)
LIU Guo-yong1,*, HOU Yong-tao1,2, LIU Hai-ping1, ZHAO Peng-peng1, and ZHU Dong-mei1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.37188/ope.20202807.1539 Cite this Article
    LIU Guo-yong, HOU Yong-tao, LIU Hai-ping, ZHAO Peng-peng, ZHU Dong-mei. Variable stiffness friction damper for dual-state isolation of flywheel on satellite[J]. Optics and Precision Engineering, 2020, 28(7): 1539 Copy Citation Text show less
    References

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    [2] XU P, HUANG CH N, WANG Y T, et al..Simulation analysis of the influence of satellite vibration on image quality [J]. Journal of Astronautics, 2003, 24(3): 259-263. (in Chinese)

    [3] LUO Q, LI D, ZHOU W, et al.. Dynamic modelling and observation of micro-vibrations generated by a single gimbal control moment gyro [J]. Journal of Sound and Vibration, 2013, 332(19): 4496-4516.

    [4] ZHOU W, LI D, LUO Q, et al.. Analysis and testing of micro-vibrations produced by momentum wheel assemblies [J]. Chinese Journal of Aeronautics, 2012, 25(4): 640-649.

    [5] FIRTH J, BLACK J. Vibration interaction in a multiple flywheel system [J]. Journal of Sound and Vibration, 2012, 331(7): 1701-1714.

    [6] NARAYAN S S, NAIR P S, GHOSAL A. Dynamic interaction of rotating momentum wheels with spacecraft elements [J]. Journal of Sound and Vibration, 2008, 315(4-5): 970-984.

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    [8] YANG C, LI D, CHENG L. Dynamic vibration absorbers for vibration control within a frequency band [J]. Journal of Sound and Vibration, 2011, 330(8): 1582-1598.

    [9] YU Z F, ZHOU X B, SHEN J F, et al.. Design of joint vibration reduction system combined isolation and absorbtion for flywheel [J]. Opt. Precision Eng., 2014, 22(4): 897-903.(in Chinese)

    [10] OH C S, LEE W, BANG H. Passive jitter isolation for reaction wheel of satellites[C].2006 SICE-ICASE International Joint Conference. IEEE, 2006: 3891-3895.

    [11] PENDERGAST K J, SCHAUWECKER C J. Use of a passive reaction wheel jitter isolation system to meet the advanced X-ray astrophysics facility imaging performance requirements[C].Space Telescopes and Instruments V. International Society for Optics and Photonics, 1998, 3356: 1078-1095.

    [12] LIU X T, KONG X S, SHEN J F, et al.. Vibration isolator with relaxation type damping for micro-vibration isolation from satellite remote sensors [J]. Opt. Precision Eng., 2017, 25(9): 2448-2453.(in Chinese)

    [13] LI T P. Research on Micro Vibration and Its Isolation of Spacecraft[D]. Harbin: Harbin Institute of Technology, 2013. (in Chinese)

    [14] WANG G Y, GUAN X, CHEN X, et al.. Parameter design and experimental study of a two state nonlinear isolator [J]. Journal of Astronautics, 2011, 32(1): 7-14. (in Chinese)

    [15] PENG L Y. Theoretical Analysis and Application Research on Energy Dissipating Restraint [D]. Beijing: Beijing University of Technology, 2004. (in Chinese)

    [16] LI CH. Friction Damper Development and Application [D]. Beijing: China Academy of Building Research, 2011. (in Chinese).

    LIU Guo-yong, HOU Yong-tao, LIU Hai-ping, ZHAO Peng-peng, ZHU Dong-mei. Variable stiffness friction damper for dual-state isolation of flywheel on satellite[J]. Optics and Precision Engineering, 2020, 28(7): 1539
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