A Blending Method Control of Switched LPV Systems with Slow-varying Parameters and Its Application to an F-16 Aircraft Model

被引:0
|
作者
He Xu [1 ]
Zhao Jun [1 ]
Dimirovski, Georgi M.
机构
[1] Northeastern Univ, State Key Lab Integrated Automat Proc Ind, Shenyang 110819, Peoples R China
关键词
Blending method; Switched LPV systems; Induced L-2-norm; F-16; aircraft; H-INFINITY CONTROL;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a controller design method using a blending method based on a common Lyapunov function for the induced L-2-norm problem for switched linear parameter varying (LPV) systems with slowly-varying parameters. The parameter region is divided into two overlapped subsets, and Lyapunov existence conditions are proposed in terms of linear matrix inequalities (LMIs) for each subset. Based on each Lyapunov function in each subset, the blending method is used to construct a blended Lyapunov function for the whole parameter set. The proposed method is applied to an F-16 aircraft longitudinal model and simulation result demonstrate the effectiveness of the approach.
引用
收藏
页码:1765 / 1770
页数:6
相关论文
共 44 条
  • [1] Control of Switched LPV Systems Using Common Lyapunov Function Method and an F-16 Aircraft Application
    He, Xu
    Dimirovski, Georgi M.
    Zhao, Jun
    2010 IEEE INTERNATIONAL CONFERENCE ON SYSTEMS, MAN AND CYBERNETICS (SMC 2010), 2010,
  • [2] MULTIPLE LYAPUNOV FUNCTIONS WITH BLENDING FOR INDUCED L2-NORM CONTROL OF SWITCHED LPV SYSTEMS AND ITS APPLICATION TO AN F-16 AIRCRAFT MODEL
    He, Xu
    Zhao, Jun
    ASIAN JOURNAL OF CONTROL, 2014, 16 (01) : 149 - 161
  • [3] Blending methodology of linear parameter varying control synthesis of F-16 aircraft system
    Shin, JY
    Balas, GJ
    Kaya, MA
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2002, 25 (06) : 1040 - 1048
  • [4] Optimal blending functions in linear parameter varying control synthesis for F-16 aircraft
    Shin, JY
    Balas, GJ
    PROCEEDINGS OF THE 2002 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 2002, 1-6 : 41 - 46
  • [5] Switching LPV control of an F-16 aircraft via controller state reset
    Lu, B
    Wu, F
    Kim, S
    IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2006, 14 (02) : 267 - 277
  • [6] Model reference adaptive control for switched LPV systems and its application
    Xie, Jing
    Zhao, Jun
    IET CONTROL THEORY AND APPLICATIONS, 2016, 10 (17): : 2204 - 2212
  • [7] Probabilistic robust linear parameter-varying control of an F-16 aircraft
    Lu, Bei
    Wu, Fen
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2006, 29 (06) : 1454 - 1460
  • [8] Simultaneous fault detection and control for switched LPV systems with inexact parameters and its application
    Zhu, Kongwei
    Zhao, Jun
    INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, 2017, 48 (14) : 2909 - 2920
  • [9] Stabilization for Switched LPV Systems with Markovian Jump Parameters and Its Application
    Yang, Dong
    Zhao, Jun
    ASIAN JOURNAL OF CONTROL, 2017, 19 (01) : 11 - 21
  • [10] INTEGRATED FAULT TOLERANT FLIGHT CONTROL DESIGN WITH APPLICATION TO AN F-16 AIRCRAFT
    Fekih, Afef
    CONTROL AND INTELLIGENT SYSTEMS, 2011, 39 (03) : 159 - 167