System integration and control design of a maglev platform for space vibration isolation

被引:26
作者
Gong, Zhaopei [1 ]
Ding, Liang [1 ]
Yue, Honghao [1 ]
Gao, Haibo [1 ]
Liu, Rongqiang [1 ]
Deng, Zongquan [1 ]
Lu, Yifan [1 ]
机构
[1] Harbin Inst Technol, State Key Lab Robot & Syst, Harbin, Heilongjiang, Peoples R China
基金
中国国家自然科学基金;
关键词
Active vibration control; vibration isolation; maglev actuator; optimum allocation; nonlinear compensation; MICRO-VIBRATION; VERIFICATION; POSITIONER; MODEL;
D O I
10.1177/1077546319836892
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Micro-vibration has been a dominant factor impairing the performance of scientific experiments which are expected to be deployed in a micro-gravity environment such as a space laboratory. The micro-vibration has serious impact on the scientific experiments requiring a quasi-static environment. Therefore, we proposed a maglev vibration isolation platform operating in six degrees of freedom (DOF) to fulfill the environmental requirements. In view of the noncontact and large stroke requirement for micro-vibration isolation, an optimization method was utilized to design the actuator. Mathematical models of the actuator's remarkable nonlinearity were established, so that its output can be compensated according to a floater's varying position and a system's performance may be satisfied. Furthermore, aiming to adapt to an energy-limited environment such as space laboratory, an optimum allocation scheme was put forward, considering that the actuator's nonlinearity, accuracy, and minimum energy-consumption can be obtained simultaneously. In view of operating in 6-DOF, methods for nonlinear compensation and system decoupling were discussed, and the necessary controller was also presented. Simulation and experiments validate the system's performance. With a movement range of 10 x 10 x 8 mm and rotations of 200 mrad, the decay ratio of -40 dB/Dec between 1 and 10 Hz was obtained under close-loop control.
引用
收藏
页码:1720 / 1736
页数:17
相关论文
共 30 条
  • [1] Model building and verification for active control of microvibrations with probabilistic assessment of the effects of uncertainties
    Aglietti, GS
    Langley, RS
    Rogers, E
    Gabriel, SB
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2004, 218 (04) : 389 - 399
  • [2] Design and Implementation of a New Six-DOF Maglev Positioner With a Fluid Bearing
    Chen, Mei-Yung
    Huang, Sheng-Chih
    Hung, Shao-Kang
    Fu, Li-Chen
    [J]. IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2011, 16 (03) : 449 - 458
  • [3] DeLombard R, 1997, 4 INT MICR COMB WORK, P323
  • [4] Greenwood D T., 2006, Advanced Dynamics
  • [5] Gu J, 2004, J DYNAMIC SYSTEMS ME, V127, P433
  • [6] Hansen C., 2012, ACTIVE CONTROL NOISE
  • [7] Sensors and control of a space-based six-axis vibration isolation system
    Hauge, GS
    Campbell, ME
    [J]. JOURNAL OF SOUND AND VIBRATION, 2004, 269 (3-5) : 913 - 931
  • [8] Development of a maglev lens driving actuator for off-axis control and adjustment of the focal point in laser beam machining
    He, Dongjue
    Shinshi, Tadahiko
    Nakai, Takahiro
    [J]. PRECISION ENGINEERING-JOURNAL OF THE INTERNATIONAL SOCIETIES FOR PRECISION ENGINEERING AND NANOTECHNOLOGY, 2013, 37 (02): : 255 - 264
  • [9] Study on the Sliding Mode Control System for Air Gap of Electrical Maglev based on the Feedback Linearization
    He, Zhiyuan
    Wei, Wei
    [J]. 2008 7TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION, VOLS 1-23, 2008, : 8008 - 8011
  • [10] High-Performance Tracking of Piezoelectric Positioning Stage Using Current-Cycle Iterative Learning Control With Gain Scheduling
    Huang, Deqing
    Xu, Jian-Xin
    Venkataramanan, Venkatakrishnan
    The Cat Tuong Huynh
    [J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2014, 61 (02) : 1085 - 1098