Dynamic decoupling tracking control for the polytopic LPV model of hypersonic vehicle

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• 作者：XueJing Lan ; YongJi Wang ; Lei Liu
• 关键词：HFV ; polytopic LPV model ; reference model ; LMIs ; dynamic decoupling ; ; LPV ; /li> ; /li> 092203
• 刊名：SCIENCE CHINA Information Sciences
• 出版年：2015
• 出版时间：September 2015
• 年：2015
• 卷：58
• 期：9
• 页码：1-14
• 全文大小：567 KB
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• 作者单位：XueJing Lan (1)
  YongJi Wang (1)
  Lei Liu (1)
  
  1. National Key Laboratory of Science and Technology on Multispectral Information Processing, School of Automation, Huazhong University of Science and Technology, Wuhan, 430074, China
  
• 刊物类别：Computer Science
• 刊物主题：Chinese Library of Science
  Information Systems and Communication Service
  
• 出版者：Science China Press, co-published with Springer
• ISSN：1869-1919

文摘

The dynamic decoupling problem of the hypersonic flight vehicle (HFV) is considered in this paper. The Linear Parameter-Varying (LPV) model of the HFV is firstly obtained and smoothly transformed into a polytopic form by the Tensor-Product (TP) model transformation method. After that, a dynamic decoupling control method is derived by minimizing the H /sub> norm of a virtual system, which is composed by the controlled system and the no coupling reference model. The necessary and sufficient condition for the existence of the controller is derived based on Linear Matrix Inequalities (LMIs). Next, the decoupling controller for the polytopic LPV model of HFV is designed. And the simulation results show that the proposed method has perfect performance in terms of dynamic decoupling.