International Journal of Aeronautical and Space Sciences

  • 제16권1호
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  • Pages.28-40
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  • 2015
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  • 2093-274X(pISSN)
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  • 2093-2480(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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Experimental Study of Adaptive Sliding Mode Control for Vibration of a Flexible Rectangular Plate

  • Yang, Jingyu (Joint Laboratory of Spacecraft Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Liu, Zhiqi (Joint Laboratory of Spacecraft Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Cui, Xuanming (Joint Laboratory of Spacecraft Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Qu, Shiying (Joint Laboratory of Spacecraft Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Wang, Chu (Joint Laboratory of Spacecraft Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Lanwei, Zhou (The State Key Laboratory of Mechanics and Control for Mechanical Structures, Nanjing University of Aeronautics and Astronautics) ;
  • Chen, Guoping (The State Key Laboratory of Mechanics and Control for Mechanical Structures, Nanjing University of Aeronautics and Astronautics)
  • 투고 : 2014.11.05
  • 심사 : 2015.03.02
  • 발행 : 2015.03.30
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초록

This paper aims to address the intelligent active vibration control problem of a flexible rectangular plate vibration involving parameter variation and external disturbance. An adaptive sliding mode (ASM) MIMO control strategy and smart piezoelectric materials are proposed as a solution, where the controller design can deal with problems of an external disturbance and parametric uncertainty in system. Compared with the current 'classical' control design, the proposed ASM MIMO control strategy design has two advantages. First, unlike existing classical control algorithms, where only low intelligence of the vibration control system is achieved, this paper shows that high intelligent of the vibration control system can be realized by the ASM MIMO control strategy and smart piezoelectric materials. Second, the system performance is improved due to two additional terms obtained in the active vibration control system. Detailed design principle and rigorous stability analysis are provided. Finally, experiments and simulations were used to verify the effectiveness of the proposed strategy using a hardware prototype based on NI instruments, a MATLAB/SIMULINK platform, and smart piezoelectric materials.

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피인용 문헌

  1. Novel Distributed PZT Active Vibration Control Based on Characteristic Model for the Space Frame Structure vol.2016, 2016, https://doi.org/10.1155/2016/5928270