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

基于二型TSK模糊滑模控制的可变翼高超声速飞行器自适应模态切换

  • Research Paper
  • Special Focus on Advanced Nonlinear Control of Hypersonic Flight Vehicles
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Abstract

This paper presents a novel adaptive mode switching scheme for hypersonic morphing aircraftwith retracted winglets based on type-2 Takagi-Sugeno-Kang (TSK) fuzzy sliding mode control. For each ofretracting and stretching modes, a specific sliding mode controller has been adopted. Drawing upon input/outputlinearization to globally linearize the nonlinear model of the hypersonic aircraft at first, a type-2 TSK fuzzylogic system is devised for robust mode switching between these sliding mode controllers. For rapid stabilizationof 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.

创新点

本文提出一种新的基于二型TSK模糊滑模控制的可变翼高超声速飞行器自适应模态切换方法。对于小翼收回和伸出两个模态, 采用滑模控制使其稳定。对于小翼伸缩的切换过程, 首先利用输入输出反馈线性化使飞行器的非线性模型精确线性化, 然后设计二型TSK模糊逻辑系统使小翼收回和伸出两个模态的滑模控制器实现平滑切换。为了使系统能够快速稳定, 利用李雅普诺夫稳定性理论设计模态切换的自适应律。仿真结果表明本文所提出的切换控制方法能够实现模态切换的稳定性和平滑性。

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Authors and Affiliations

  1. Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

    Xin Jiao & Ju Jiang

  2. University of Waterloo, Waterloo N2L 3G1, Canada

    Baris Fidan & Mohamed Kamel

Authors
  1. Xin Jiao
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  2. Baris Fidan
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  3. Ju Jiang
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  4. Mohamed Kamel
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Correspondence to Ju Jiang.

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Jiao, X., Fidan, B., Jiang, J. et al. Adaptive mode switching of hypersonic morphing aircraft based on type-2 TSK fuzzy sliding mode control. Sci. China Inf. Sci. 58, 1–15 (2015). https://doi.org/10.1007/s11432-015-5349-z

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  • DOI: https://doi.org/10.1007/s11432-015-5349-z

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