The Adaptive Fuzzy control of Hypersonic Vehicle

被引：0

作者：

Guan Ping ^{[1
]}

Xue Li ^{[1
]}

Liu Xiao-he ^{[1
]}

Wang Sai ^{[1
]}

机构：

[1] Beijing Informat Sci & Technol Univ, Dept Automat Control, Beijing 100192, Peoples R China

来源：

PROCEEDINGS OF THE 2012 24TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC) | 2012年

关键词：

Hypersonic vehicle; Adaptive fuzzy control; Robustness; CONTROL 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：

In this paper, the adaptive fuzzy control is applied to the hypersonic vehicle and the detailed design procedure of the fuzzy control system is presented. According to the tracking errors, ruler parameters of the fuzzy system are adjusted on-line to enable the system to approximate the uncertain nonlinear functions of the Hypersonic Vehicle. With Lyapunov theory, the adaptive law is derived and it is proven that the overall system is uniformly ultimately bounded. Simulations results show the proposed control law can suppress the perturbation effectively and have better dynamic and static performances.

引用

页码：2722 / 2727

页数：6

共 4 条

[1] A STABILITY APPROACH TO FUZZY CONTROL DESIGN FOR NONLINEAR-SYSTEMS
HWANG, GC
LIN, SC
[J]. FUZZY SETS AND SYSTEMS, 1992, 48 (03) : 279 - 287
[2] Tong Shaocheng, 2003, IEEE T FUZZY SYST, V11, P315
[3] Robust nonlinear control of a hypersonic aircraft
Wang, Q
Stengel, RF
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2000, 23 (04) : 577 - 585
[4] Adaptive sliding mode control design for a hypersonic flight vehicle
Xu, HJ
Mirmirani, MD
Ioannou, PA
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2004, 27 (05) : 829 - 838

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