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
相关论文
共 50 条
  • [1] Comparing linear parameter-varying gain-scheduled control techniques for active flutter suppression
    Barker, JM
    Balas, GJ
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2000, 23 (05) : 948 - 955
  • [2] LINEAR PARAMETER-VARYING CONTROL OF A WING-SECTION STALL FLUTTER
    Fan, Wen
    Liu, Hugh H. T.
    Kwong, Raymond H. S.
    7TH ANNUAL DYNAMIC SYSTEMS AND CONTROL CONFERENCE, 2014, VOL 1, 2014,
  • [3] A Vibroacoustic Application of Modeling and Control of Linear Parameter-Varying Systems
    De Caigny, Jan
    Camino, Juan F.
    Oliveira, Ricardo C. L. F.
    Peres, Pedro L. D.
    Swevers, Jan
    JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2010, 32 (04) : 409 - 419
  • [4] Subspace Identification of an Aircraft Linear Parameter-Varying Flutter Model
    Buchholz, Michael
    Larimore, Wallace E.
    2013 AMERICAN CONTROL CONFERENCE (ACC), 2013, : 2263 - 2267
  • [5] Linear parameter-varying modeling and control of the steam temperature in a Canadian SCWR
    Sun, Peiwei
    Zhang, Jianmin
    Su, Guanghui
    NUCLEAR ENGINEERING AND DESIGN, 2017, 313 : 225 - 235
  • [6] Linear Parameter-Varying Polytopic Modeling and Control Design for Guided Projectiles
    Vinco, Gian Marco
    Sename, Olivier
    Strub, Guillaume
    Theodoulis, Spilios
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2024, 47 (03) : 433 - 447
  • [7] Linear Parameter-varying Approach for Modeling and Control of Rapid Thermal Processes
    Trudgen, Mark
    Velni, Javad Mohammadpour
    INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 2018, 16 (01) : 207 - 216
  • [8] Linear Parameter-varying Approach for Modeling and Control of Rapid Thermal Processes
    Mark Trudgen
    Javad Mohammadpour Velni
    International Journal of Control, Automation and Systems, 2018, 16 : 207 - 216
  • [9] Modeling and H∞ control for switched linear parameter-varying missile autopilot
    Lim, SY
    How, JP
    IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2003, 11 (06) : 830 - 838
  • [10] Linear parameter-varying modeling and control of structural dynamics with aerothermoelastic effects
    Lind, R
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2002, 25 (04) : 733 - 739