帮助 关于我们

返回检索结果

采用分布式压电驱动器升力面的颤振主动抑制
Flutter Suppression using distributed piezoelectric actuators

查看参考文献9篇

陈伟民 1   管德 2   李敏 3   诸德超 2  
文摘 对采用分布式压电驱动器升力面的颤振主动抑制进行了理论与试验研究。应用LQG最优控制法设计了主动控制律,在控制律降阶时提出了平衡实现与LK法结合使用的新途径,在对不定常气动力进行有理函数拟合时对LS法进行了改进。试验中利用激光测速仪非接触测量模型的速度响应并在地面共振试验中用压电驱动器激振模型。颤振风洞试验结果表明,理论计算合理并与试验结果吻合良好。
其他语种文摘 An analytical and experimental investigation of a lifting surface with distributed piezoelectric actuators for active flutter suppression is described. Equations such like structure dynamic equation, flutter equation and state space equation of piezoelectric laminated structure are developed, based on investigating mechanic-electric coupling. LQG control law was used for active flutter suppression. Random disturbance existing in measuring singal being considered, so Kalman filter was designed for states estimating. The order reduction of control law is discussed on two hands. First, the physical reduction of state-space equations, meanwhile the reduction of aerodynamic lag terms based upon modification of aerodynamic simulation; Second, after discussed balance realization and LK method, a combed balance realization and LK method was developed. Ground tests preparing for wind-tunnel test were implemented after manufacturing model. By non-contact exicting and non-contact laser measuring, the accuracy of vibration tests improved pretty well. The control laws were implemented using real time digital control computer, then the open-loop response of model-control system was tested. When wind-tunnel tests were conducted employing laser vibrameter and digital control computer, both of open-loop and close-loop velocity response was recorded in tests in order to compare them, additionally control voltage applied to piezoelectric actuators also recorded in close loop tests. Tests demonstrate that the test results agree well with that of analysis, and distributed piezoelectric actuators can be employed for flutter suppression with an increase in flutter speed of 12%.
来源 力学学报 ,2002,34(5):756-763 【核心库】
关键词 颤振 ; 主动抑制 ; 压电 ; 驱动器 ; 风洞实验
地址

1. 北京大学力学与工程科学系, 北京, 100871  

2. 北京航空航天大学飞行器设计与应用力学系, 北京, 100083  

3. 中国科学院力学研究所, 北京, 100080

语种 中文
文献类型 研究性论文
ISSN 0459-1879
学科 力学
基金 国家自然科学基金 ;  中国博士后科学基金
文献收藏号 CSCD:1013723

参考文献 共 9 共1页

1.  Heeg J. Analytical and experimental investigation of flutter suppression by piezoelectric actuation. NASA TP 3241,1993 被引 1    
2.  Lazarus K B. Multivariable active lifting surface control using strain actuation: analytical and experimental results. journal of Aircraft,1997,34(3):313-321 被引 4    
3.  Lin C Y. Open- and closed-loop results of a strain-actuated active aeroelastic wing. Journal of Aircraft,1996,33(5):987-994 被引 5    
4.  Tzou H S. Distributed dynamic identification and controls of flexible shell: theory and finite element development. AIAA 90-1089 CP 被引 1    
5.  Hwang W-S. Finite element modeling of piezoelectric sensors and actuators. AIAA Journal,1993,31(5):930-937 被引 25    
6.  陈伟民. 不定常气动力的有理函数拟合研究,1992 被引 1    
7.  Moore B C. Principal component analysis in linear systems: controllability, observability and model reaction. IEEE Transactions on Automatic Control (AC),1981,26(1):17-31 被引 148    
8.  . Reduced-Order Aeroelastic Models via Dynamic Residualization. J Aircraft,1990,27(5):449-455 被引 1    
9.  Anderson L R. Order reduction of aeroelastic models through LK transformation and raccati iteration. AIAA 93-3795 CP 被引 1    
引证文献 4

1 李敏 压电驱动器的气动弹性应用 航空学报,2009,30(12):2301-2310
被引 6

2 杨超 多控制面飞机的全机颤振主动抑制设计 航空学报,2010,31(8):1501-1508
被引 7

显示所有4篇文献

论文科学数据集
PlumX Metrics
相关文献

 作者相关
 关键词相关
 参考文献相关

版权所有 ©2008 中国科学院文献情报中心 制作维护:中国科学院文献情报中心
地址:北京中关村北四环西路33号 邮政编码:100190 联系电话:(010)82627496 E-mail:cscd@mail.las.ac.cn 京ICP备05002861号-4 | 京公网安备11010802043238号