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Article Navigation> JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY> 2015> 24(3): 413-421
CAO Hai-qing, WANG Yu, YAO Zhi-ying. On a novel non-smooth output feedback controller for the attitude control of a small float satellite antenna[J]. JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2015, 24(3): 413-421. doi: 10.15918/j.jbit1004-0579.201524.0320
Citation: CAO Hai-qing, WANG Yu, YAO Zhi-ying. On a novel non-smooth output feedback controller for the attitude control of a small float satellite antenna[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2015, 24(3): 413-421.doi:10.15918/j.jbit1004-0579.201524.0320
shu

On a novel non-smooth output feedback controller for the attitude control of a small float satellite antenna

doi:10.15918/j.jbit1004-0579.201524.0320
  • 1.

    School of Information, Capital University of Economics and Business, Beijing 100070, China;School of Automation, Beijing Institute of Technology, Beijing 100081, China

  • 2.

    School of Automation, Beijing Institute of Technology, Beijing 100081, China

  • 3.

    School of Logistics, Beijing Wuzi University, Beijing 101149, China

  • Received Date:2014-01-21
    Abstract
  • A novel non-smooth controller of the second order double integrator system with a bounded disturbance is proposed, which stability is proved and which disturbance rejection capability is analyzed by MATLAB simulation experiments. The novel non-smooth output feedback controller and tracking differentiator are applied to control the azimuth servo system of the small floating satellite antenna. The MATLAB simulation and hardware in the loop simulation experiments are conducted. The experiment results validate that the non-smooth output feedback controller with stronger surge and sudden disturbance rejection capability can realize the stable azimuth servo control of the small floating antenna to ensure the communication between the target satellite and the antenna with high quality.
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    • References (13)
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