Optics and Precision Engineering, Volume. 18, Issue 1, 149(2010)

Implementation of variable structure and speed-changed integration control for flywheels

WU Jun-feng1...2,*, WU Yi-hui1, AN Jing1,2, BAI Yue1, LI Hai-wen1 and XUAN Ming1 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
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    References(9)

    [1] [1] JIA H G, ZHAO H B, WU Y H, et al.. Single axis double flywheels integrated power and attitude control system[J].Opt. Precision Eng.,2004,12(3):504-509. (in Chinese).

    [4] [4] CHENG H , GE S M, LIU F CH, et al.. The design of torque mode control for reaction wheel system[J]. Journal of Astronautics,2006(6):1248-1253. (in Chinese)

    [5] [5] GUO Y D, LU J H. Study on braking switch of flywheel[J]. Small & Special Electrical Machines, 1998(3):2-5. (in Chinese)

    [6] [6] WANG H, YANG Y, TIAN W F, et al.. Braking current analysis of a satellite attitude control system[J]. Small & Special Electrical Machines,2005(9):5-37. (in Chinese)

    [7] [7] DU K M, LI T C. Controlling system of inertial flywheel through torque servo motor[J]. Electric Machines and Control, 2001,5(2):119-120. (in Chinese)

    CLP Journals

    [1] CHEN Mao-sheng, JIN Guang, AN Yuan, WU Jun-feng, ZHANG Liu, QU Hong-song. Design of angular momentum wheel in SGCMG using adaptive compensation PI control[J]. Optics and Precision Engineering, 2011, 19(5): 1075

    [2] WANG Hui, WU Jun-feng, LI Yin, WU Yi-hui. Design of reaction flywheel systems for small satellites[J]. Optics and Precision Engineering, 2014, 22(2): 331

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    WU Jun-feng, WU Yi-hui, AN Jing, BAI Yue, LI Hai-wen, XUAN Ming. Implementation of variable structure and speed-changed integration control for flywheels[J]. Optics and Precision Engineering, 2010, 18(1): 149

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    Paper Information

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    Received: Apr. 28, 2009

    Accepted: --

    Published Online: Aug. 31, 2010

    The Author Email: Jun-feng WU (awublack@126.com)

    DOI:

    CSTR:32186.14.

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