引用本文:张子健,徐敏,陈士橹,罗翔.抑制机翼主动颤振的输出微分调节器[J].控制理论与应用,2009,26(10):1143~1147.[点击复制]
ZHANG Zi-Jian,XU Min,CHEN Shi-lu,LUO Xiang.Output-rate-weighted regulator for suppressing active flutter on flapping wing[J].Control Theory and Technology,2009,26(10):1143~1147.[点击复制]
抑制机翼主动颤振的输出微分调节器
Output-rate-weighted regulator for suppressing active flutter on flapping wing
摘要点击 1850  全文点击 1221  投稿时间:2008-05-05  修订日期:2008-12-30
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DOI编号  10.7641/j.issn.1000-8152.2009.10.CCTA080412
  2009,26(10):1143-1147
中文关键词  颤振抑制  最优控制  输出微分
英文关键词  flutter suppression  optimal control  output rate weighted
基金项目  高等学校博士学科点专向科研基金资助项目(20070699054); 国家自然科学基金重大研究计划资助项目(90405002).
作者单位E-mail
张子健* 西北工业大学航天学院 yuqiuyashi2006@sina.com 
徐敏 西北工业大学 航天学院  
陈士橹 西北工业大学 航天学院  
罗翔 西北工业大学 365研究所  
中文摘要
      机翼的主动颤振抑制技术是现代弹性飞行器设计的重点, 传统的基于输出量最小化设计的线性二次最优调节器(LQRY)由于引入的信息量少, 其抑制颤振的效果并不理想. 本文提出了一种基于输出微分项推导的最优调节器(ORW)设计方法. 与LQRY方法相比, 该方法引入了更多的系统信息, 能够有效抑制无法直接测量的输出微分项的振动, 从而更快地抑制输出的振动. 最后对典型的气动弹性主动控制系统(BACT)模型, 分别采用LQRY和ORW调节器对机翼颤振进行抑制, 仿真结果表明, 新方法能够更加快速有效地抑制机翼的颤振.
英文摘要
      The suppression of active flutter on a flapping wing is a major topic in the design of modern flexible airplanes; but the traditional linear quadratic optimal regulator(LQRY) based on the minimization of the weighted output doesn’t work well for this purpose. A new optimal regulator based on the minimization of the output rate weighted minimizing(ORW) is developed. Being different from the LQRY, this regulator makes use of more system information. It minimizes the time-rate of the output, which is not available for a direct measurement, thereby suppressing the flutter more quickly. Simulation is performed on a Benchmark Active Control Technology(BACT) system by using the ORWregulator and the LQRY regulator respectively. The results show that the ORW regulator provides a better performance.