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Optimal Control of Reinforced Plate Based on the Minimum Energy

机译:基于最小能量的钢筋板最优控制

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摘要

An optimal control method based on the minimum energy of the vibration system is proposed for piezoelectric damping control of the reinforced aircraft plate.Subsequently,the dynamic equations of the piezoelectric damping reinforced plate system and the state space equations are derived.The method to determine the weight matrix of the system is presented based on the minimum energy of the vibration system.In order to obtain the optimal controller,the control parameters of the feedback controller are obtained by using the optimal method.A piezoelectric vibration optimal control experiment platform is designed to control the vibration of reinforced aircraft plate.The experimental results show that the method has good control performances.

著录项

  • 来源
    《南京航空航天大学学报(英文版)》 |2016年第2期|166-172|共7页
  • 作者单位

    State Key Laboratory of Mechanics and Control of Mechanical Structures, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China;

    School of Transportation and Vehicle Engineering, Shandong University of Technology, Zibo 255049, P.R.China;

    State Key Laboratory of Mechanics and Control of Mechanical Structures, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China;

    Nanjing University of Aeronautics and Astronautics;

    School of Transportation and Vehicle Engineering at Shandong University of Technology;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 非线性振动;减振、隔振理论;
  • 关键词

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