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

被引：23
|
作者：
Lan XueJing [1 ]
Wang YongJi [1 ]
Liu Lei [1 ]
机构：
[1] Huazhong Univ Sci & Technol, Sch Automat, Natl Key Lab Sci & Technol Multispectral Informat, Wuhan 430074, Peoples R China
来源：
SCIENCE CHINA-INFORMATION SCIENCES | 2015年 / 58卷 / 09期
基金：
中国国家自然科学基金;
关键词：
HFV; polytopic LPV model; reference model; LMIs; dynamic decoupling; DIAGONAL DOMINANCE; DESIGN;
D O I：
10.1007/s11432-015-5339-1
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
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-infinity 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.
引用
收藏
页码：1 / 14
页数：14
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