Optics and Precision Engineering, Volume. 23, Issue 11, 3138(2015)

Design and verification of double-loop control electromechanical actuator system

ZHANG Yue* and HAN Xue-feng
Author Affiliations
  • [in Chinese]
  • show less
    References(16)

    [1] [1] WANG J L, XIE F Q, LIU Y H. The reasearch status and development of missileelectromechanical actuator [J].Winged Missile Journal, 2008(3): 42-46.(in Chinese)

    [2] [2] LIN ZH W.Study on actuation DC servo system based on DSP[D]. Xian: Northwestern Polytechnical University, 2011.(in Chinese)

    [3] [3] VACULIK S A. A framework for electromechanical actuator design [D]. State of Texas: The University of Texas at Austin, 2008.

    [4] [4] LI Y F.Study on the controller of electromechanical actuator[D].Beijing: Beijing Institute of Technology, 2006.(in Chinese)

    [5] [5] HABIBI S S, ROACH J, LUECKE G. Inner-loop control for electromechanical (EMA) flight surface actuation systems [J]. Journal of dynamic systems, measurement, and control, 2008, 130: 0510021-13.

    [6] [6] HEWSON R. Air-to-air missiles beyond visual range, United States AIM-120 AMRAAM [C]. Janes Air Launched Weapons, 2005.

    [7] [7] HAN X F.Research on the Key Technology of Rigid-flexible Coupling Electric Actuator Servo System with Clearance[D].Changchun: Chang-chun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Science, 2011.(in Chinese)

    [8] [8] XIAO Q J. Identification and compensation of nonlinearity for electromechanical actuator servo system [J].Opt. Precision Eng.. 2013, 8(21): 2038-2047. (in Chinese)

    [9] [9] ZHANG M Y. Servo system of harmonic drive electromechanical actuator using improvedADRC [J].Opt. Precision Eng., 2014, 1(22): 99-108. (in Chinese)

    [10] [10] CUI Y B. Feasibility of bandwidth four rudder wings electromechanical actuator [J].ELECTRIC MACHINES AND CONTROL, 2012, 12(16): 87-93. (in Chinese)

    [11] [11] WANG L.Dynamic Simulation for Electromechanical Actuator Servo System of High-speed Vehicle[D].Harbin: Harbin Institute of Technology, 2013.(in Chinese)

    [12] [12] WANG G X, HE ZH. Control System Design [M]. Beijing: Tsinghua University Press, 2008.(in Chinese)

    [13] [13] ZHANG J B, et al..Model identification and corrector design for servo system ofelectromechanical actuator [J].Opt. Precision Eng., 2008, 10(16): 1971-1976. (in Chinese)

    [14] [14] ZHANG J B.Parameter balance design of electromechanical actuator [J].Journal of ProjectilesRockets Missiles and Guidance, 2013, 5(33): 29-34. (in Chinese)

    [15] [15] HAN X F, LIU B.Design and analysis of power system of micro-electromechanical actuator [C].IEEE 2010 2nd International Conference on Industrial Mechatronics and Automation, 2010, 298-302.

    [16] [16] HAN X F, GE M.The effect of backlash nonlinear on resonance frequency of actuator transmission system [C].IEEE 2011 3rd International Conference on Advanced Computer Control, 2011, 586-590.

    Tools

    Get Citation

    Copy Citation Text

    ZHANG Yue, HAN Xue-feng. Design and verification of double-loop control electromechanical actuator system[J]. Optics and Precision Engineering, 2015, 23(11): 3138

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category:

    Received: Dec. 9, 2014

    Accepted: --

    Published Online: Jan. 25, 2016

    The Author Email: Yue ZHANG (zhangyue@ciomp.ac.cn)

    DOI:10.3788/ope.20152311.3138

    Topics