A Novel SHLNN Based Robust Control and Tracking Method for Hypersonic Vehicle under Parameter Uncertainty

被引:3
|
作者
Li, Chuanfeng [1 ,2 ]
Wu, Hao [3 ]
Yang, Zhile [4 ]
Wang, Yongji [5 ]
Sun, Zeyu [1 ]
机构
[1] Luoyang Inst Sci & Technol, Sch Comp & Informat Engn, Luoyang 471023, Peoples R China
[2] Queens Univ Belfast, Sch Elect Elect Engn & Comp Sci, Belfast BT9 5AH, Antrim, North Ireland
[3] Beijing Aerosp Automat Control Inst, Beijing 100854, Peoples R China
[4] Chinese Acad Sci, Shenzhen Inst Adv Technol, Shenzhen 518055, Guangdong, Peoples R China
[5] Huazhong Univ Sci & Technol, Sch Automat, Wuhan 430074, Hubei, Peoples R China
基金
英国工程与自然科学研究理事会; 中国国家自然科学基金;
关键词
GUARANTEED COST CONTROL; ADAPTIVE-CONTROL; NONLINEAR-SYSTEMS; CONTROL LAW; MODEL; PERFORMANCE; STATE;
D O I
10.1155/2017/6034786
中图分类号
O1 [数学];
学科分类号
0701 ; 070101 ;
摘要
Hypersonic vehicle is a typical parameter uncertain system with significant characteristics of strong coupling, nonlinearity, and external disturbance. In this paper, a combined system modeling approach is proposed to approximate the actual vehicle system. The state feedback control strategy is adopted based on the robust guaranteed cost control (RGCC) theory, where the Lyapunov function is applied to get control law for nonlinear system and the problem is transformed into a feasible solution by linear matrix inequalities (LMI) method. In addition, a nonfragile guaranteed cost controller solved by LMI optimization approach is employed to the linear error system, where a single hidden layer neural network (SHLNN) is employed as an additive gain compensator to reduce excessive performance caused by perturbations and uncertainties. Simulation results show the stability and well tracking performance for the proposed strategy in controlling the vehicle system.
引用
收藏
页数:14
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