Affiliation of Author(s):自动化学院
Journal:Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.
Abstract:This paper proposes a type-2 fuzzy adaptive sliding mode control scheme for tracking control of hypersonic aircraft with uncertainties. This method uses full-state feedback to linearize the nonlinear model of hypersonic aircraft. Combining the interval type-2 fuzzy approach and adaptive sliding mode control keeps the system stable in the existence of uncertain parameters. For rapid stabilization of the system, the adaptive laws are designed using a direct constructive Lyapunov analysis together with a well-established type-2 fuzzy logic control. Simulation test results indicate that the proposed control scheme provides enhancement of robustness to parametric uncertainty and improvement in tracking performance of the hypersonic aircraft. © IMechE 2017.
ISSN No.:0954-4100
Translation or Not:no
Date of Publication:2019-06-01
Co-author:Jiao, Xin,Fidan, Baris,Kamel, Mohamed
Correspondence Author:Jiang Ju
Date of Publication:2019-06-01