Direct Adaptive Type-2 Fuzzy Logic Control of a Generic Hypersonic Flight Vehicle

被引：0
|
作者：
Yang, Fang [1 ]
Yuan, Ruyi [1 ]
Yi, Jianqiang [1 ]
Fan, Guoliang [1 ]
Tan, Xiangmin [1 ]
机构：
[1] Chinese Acad Sci, Inst Automat, Beijing 100190, Peoples R China
来源：
PROCEEDINGS OF THE 2013 FOURTH INTERNATIONAL CONFERENCE ON INTELLIGENT CONTROL AND INFORMATION PROCESSING (ICICIP) | 2013年
关键词：
SYSTEMS; DESIGN;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A direct adaptive type-2 fuzzy logic controller is designed in this paper. The longitudinal dynamics of a generic hypersonic flight vehicle is high-order, highly nonlinear, tight coupling and most of all includes big uncertainties. The computing of the dynamic inversion control signal is cost ineffective and an adaptive interval type-2 fuzzy logic system is used to approximate it. A H-infinity controller is implemented in order to attenuate the fuzzy approximation error and the system uncertainty. Signals' high-order derivatives are obtained by tracking differentiators and nonlinear state observers. The closed-loop stability is guaranteed by Lyapunov theory. Simulation results validate the effectiveness and robustness of the proposed controller.
引用
收藏
页码：581 / 586
页数：6
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