Dynamic surface control for hypersonic aircraft using fuzzy logic system

被引：51

作者：

Gao, DaoXiang ^{[1
]}

Sun, ZengQi ^{[1
]}

Du, TianRong ^{[1
]}

机构：

[1] Tsing Hua Univ, Dept Comp Sci & Technol, State Key Lab Intelligent Technol & Syst, Beijing 100084, Peoples R China

来源：

2007 IEEE INTERNATIONAL CONFERENCE ON AUTOMATION AND LOGISTICS, VOLS 1-6 | 2007年

关键词：

back-stepping; dynamic surface control; adaptive fuzzy control; flight control; hypersonic aircraft;

D O I：

10.1109/ICAL.2007.4338963

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

An adaptive fuzzy control strategy is proposed for the hypersonic aircraft Fuzzy logic system is used to compensate the unknown nonlinearities and modeling errors caused by changes of flight conditions. The DSC method eliminates the "explosion of terms" inherent existing in the conventional back-stepping method. Stability analysis shows that the control law can guarantee the semi-globally uniform boundedness of the solution of the closed-loop system. Numerical simulation use the longitudinal model of a hypersonic aircraft to demonstrate the effectiveness of the proposed strategy.

引用

页码：2314 / 2319

页数：6

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