Novel linear parameter-varying modeling and flutter suppression control of a smart airfoil

被引:0
|
作者
Al-Hajjar, Ali M. H. [1 ]
Swei, Sean Shan-Min [2 ]
Zhu, Guoming [1 ,3 ]
机构
[1] Michigan State Univ, Dept Mech Engn, E Lansing, MI 48823 USA
[2] NASA Ames Res Ctr, Intelligent Syst Div, Mountain View, CA USA
[3] Michigan State Univ, Dept Elect & Comp Engn, E Lansing, MI 48823 USA
关键词
Linear parameter-varying; linear parameter-varying modeling and control; gain-scheduling control; control with hard constraints; flutter suppression; smart airfoil; GAIN; DESIGN; LMIS; IDENTIFICATION;
D O I
10.1177/0959651818804377
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this article, two novel linear parameter-varying modeling and control techniques are proposed for active flutter suppression of a smart airfoil model. The smart airfoil model is instrumented with a moving mass that can be used to actively control the airfoil pitching and plunging motions. The first linear parameter-varying modeling approach makes use of the moving mass position as a scheduling parameter, and the hard constraint at the boundaries is imposed by proper selection of the parameter-varying function. The second modeling technique utilizes nonlinear springs and dampers, which are added to both ends of the airfoil groove to confine the motion of the moving mass. A state-feedback-based linear parameter-varying gain-scheduling controller with the guaranteed H infinity performance is proposed by utilizing the dynamics of the moving mass. In this study, both the position of the moving mass and the free-stream airspeed are considered as the scheduling parameters. The numerical simulations demonstrate the effectiveness of the proposed linear parameter-varying control architectures by significantly improving the performance, while increasing the flutter speed and reducing the control effort.
引用
收藏
页码:609 / 624
页数:16
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