Dynamic Surface Control for Hypersonic Aircraft Using Fuzzy Logic System

Author

Gao, DaoXiang ; Sun, Zengqi ; Du, TianRong

Author_Institution

Tsinghua Univ., Beijing

fYear

2007

fDate

18-21 Aug. 2007

Firstpage

2314

Lastpage

2319

Abstract

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.

Keywords

adaptive control; aircraft control; closed loop systems; control nonlinearities; fuzzy control; stability; adaptive fuzzy control; back-stepping method; closed-loop system; control law; dynamic surface control; error modeling; flight condition; fuzzy logic system; hypersonic aircraft; nonlinearities; stability; Adaptive control; Adaptive systems; Aerospace control; Aircraft; Control systems; Explosions; Fuzzy control; Fuzzy logic; Nonlinear dynamical systems; Programmable control; Adaptive fuzzy control; Back-stepping; Dynamic surface control; Flight control; Hypersonic aircraft;

fLanguage

English

Publisher

ieee

Conference_Titel

Automation and Logistics, 2007 IEEE International Conference on

Conference_Location

Jinan

Print_ISBN

978-1-4244-1531-1

Type

conf

DOI

10.1109/ICAL.2007.4338963

Filename

4338963