Adaptive mode switching of hypersonic morphing aircraft based on type-2 TSK fuzzy sliding mode control

被引：0
作者：
JIAO Xin [1 ]
FIDAN Baris [2 ]
JIANG Ju [1 ]
KAMEL Mohamed [2 ]
机构：
[1] Nanjing University of Aeronautics and Astronautics
[2] University of Waterloo
来源：
Science China(Information Sciences) | 2015年 / 58卷 / 07期
基金：
中国国家自然科学基金;
关键词：
hypersonic morphing aircraft; mode switching; type-2 TSK fuzzy logic system; adaptive control; sliding mode control;
D O I：
暂无
中图分类号：
V249.1 [飞行控制];
学科分类号：
081105 ;
摘要：
This paper presents a novel adaptive mode switching scheme for hypersonic morphing aircraft with retracted winglets based on type-2 Takagi-Sugeno-Kang(TSK) fuzzy sliding mode control. For each of retracting and stretching modes, a specific sliding mode controller has been adopted. Drawing upon input/output linearization to globally linearize the nonlinear model of the hypersonic aircraft at first, a type-2 TSK fuzzy logic system is devised for robust mode switching between these sliding mode controllers. For rapid stabilization of the system, the adaptive law for mode switching is designed using a direct constructive Lyapunov analysis.Simulation results demonstrate the stability and smooth transition using the proposed switched control scheme.
引用
收藏
页码：59 / 73
页数：15
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  • [1] Second-order terminal sliding mode control for hypersonic vehicle in cruising flight with sliding mode disturbance observer
    Zhang R.
    Sun C.
    Zhang J.
    Zhou Y.
    [J]. Journal of Control Theory and Applications, 2013, 11 (2): : 299 - 305
  • [2] Non-fragile switching tracking control for a flexible air-breathing hypersonic vehicle based on polytopic LPV model[J]. Huang Yiqing,Sun Changyin,Qian Chengshan,Wang Li.Chinese Journal of Aeronautics. 2013(04)
  • [3] 淡化器仿真与设计
    豆国辉
    高正红
    [J]. 科学技术与工程, 2012, 12 (11) : 2621 - 2625
  • [4] Fuzzy tracking control design for hypersonic vehicles via T-S model[J]. GAO DaoXiang 1 & SUN ZengQi 2 1 School of Technology, Beijing Forestry University, Beijing 100083, China;2 State Key Laboratory of Intelligent Technology and System, Department of Computer Science and Technology, Tsinghua University, Beijing 100084, China.Science China(Information Sciences). 2011(03)
  • [5] Adaptive neural control based on HGO for hypersonic flight vehicles[J]. XU Bin 1,2 , GAO DaoXiang 3 & WANG ShiXing 1 1 Department of Computer Science and Technology, Tsinghua University, Beijing 100084, China;2 Autonomous System Lab, ETH Zurich Zurich 8092, Switzerland;3 School of Technology, Beijing Forestry University, Beijing 100083, China.Science China(Information Sciences). 2011(03)
  • [6] Guaranteed transient performance based control with input saturation for near space vehicles[J] . Mou Chen,QinXian Wu,ChangSheng Jiang,Bin Jiang.Science China Information Sciences . 2014 (5)
  • [7] DYNAMIC SURFACE CONTROL OF CONSTRAINED HYPERSONIC FLIGHT MODELS WITH PARAMETER ESTIMATION AND ACTUATOR COMPENSATION
    Xu, Bin
    Huang, Xiyuan
    Wang, Danwei
    Sun, Fuchun
    [J]. ASIAN JOURNAL OF CONTROL, 2014, 16 (01) : 162 - 174
  • [8] Continuous high order sliding mode controller design for a flexible air-breathing hypersonic vehicle[J] . Jie Wang,Qun Zong,Rui Su,Bailing Tian.ISA Transactions . 2014
  • [9] Quasi-continuous high-order sliding mode controller and observer design for flexible hypersonic vehicle
    Zong, Qun
    Wang, Jie
    Tian, Bailing
    Tao, Yang
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 27 (01) : 127 - 137
  • [10] On-line RNN compensated second order nonsingular terminal sliding mode control for hypersonic vehicle
    Zhang, Ruimin
    Wang, Li
    Zhou, Yingjiang
    [J]. INTERNATIONAL JOURNAL OF INTELLIGENT COMPUTING AND CYBERNETICS, 2012, 5 (02) : 186 - 205
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