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：

ScienceChina(InformationSciences) | 2015年 / 58卷 / 07期

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

页码：59 / 73

页数：15

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