期刊文献+

压电材料控制悬臂梁升力面颤振研究

Piezoelectric Control of Lifting Surface Flutter
下载PDF
导出
摘要 利用压电材料建立了单输入单输出理论模型并得到颤振方程及其状态空间方程。同时应用NASTRAN、MATLAB计算软件和自行编制的程序进行了气动力拟合,并且对模型的结构动力学特性及颤振特性进行了分析。计算结果表明,通过主动控制控制律的实施,达到了颤振主动抑制的目的。 Piezoelectric material was used to establish a single input/single output (SISO) model of a lifting surface with distributed piezoelectric actuators and piezoelectric sensors. The flutter equations and state space equations of piezoelectric laminated structures were also derived. MATLAB, NASTRAN and other software programs compiled by the authors also were used to analyze the flutter and dynamic characteristics. The stability of the closed-loop was analyzed for the SISO. The result indicates that the control law can be employed for flutter suppression.
出处 《重庆建筑大学学报》 EI CSCD 北大核心 2008年第6期76-80,共5页 Journal of Chongqing Jianzhu University
基金 重庆市自然科学基金资助(CSTC 2007BB6132)
关键词 压电材料 单输入单输出 控制律 颤振 piezoelectric material single input/single output (SISO) control law flutter
  • 相关文献

参考文献11

  • 1NAM, CHANGHO. Active Aeroelastic wing design for gust load alleviation and flutter suppression[C]// 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, and AIAA/ASME/AHS Adaptive Structures Forum. Collection of Technical Papers. Reston : AIAA, 1997: 729-737.
  • 2GREGORY W REICH. An active aeroelastic wing model for vibration and flutter suppression[C]//36th AIAA/ ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and AIAA/ASME Adaptive Structures Forum. New Orleans: AIAA, 1995: 314-324.
  • 3ZHOU R C ,LAI Z H, XUE B P. Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method[J]. Journal of AIAA, 1995, 33 (6):1098-1105.
  • 4ZHOU R C, MEI C, HUANG J K. Suppression of nonlinear panel flutter at supersonic speeds and elevated temperature[J]. Journal of AIAA, 1996, 34 (2): 347-354.
  • 5JONES R T. The unsteady lift of a wing of finite aspect ratio[J]. Journal of aerospace engineering, 1941, 155: 19-25.
  • 6吴志刚.主动气动弹性机翼颤振主动抑制控制律设计与分析[C]//中国空气动力学会.第七届全国空气弹性学术交流会论文集.北京:中国空气动力学会,2001:166-173.
  • 7BRUCE C M. Principal component analysis in linear systems: controllability, observability, and model reduction[J]. IEEE Transactions on Automsatic Contril, 1981,26(1) : 11-19.
  • 8ALAN J L. Computation of system balancing transformations and other applications of simultaneous diagonalization algorithms[J]. IEEE Tans on Automatic Control, 1987,32 (2):115-121.
  • 9安德森,JB莫尔.线性最优控制[M].尤支程,译.北京:科学出版社,1982.
  • 10LEONARD R A. Order reduction of aeroelastic models through LK transformation and riccati iteration [C]// AIAA Guidance, Navigation and Control Conference. Monterey : AIAA, 1993 : 865-870.

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部