Design of adaptive switching control for hypersonic aircraft. (19th October 2015)

• Record Type: Journal Article
• Authors: Jiao, Xin; Jiang, Ju
• Is Part Of: Advances in mechanical engineering. Volume 7:Number 10(2015:Oct.)
• Publication Date: 2015-10-19
• Subjects: Interval type-2 TSK fuzzy -- sliding mode control -- switching control -- hypersonic aircraft -- adaptive; Mechanical engineering -- Periodicals; 621.05
• DOI: 10.1177/1687814015610465
• Languages: English
• ISSNs: 1687-8132

Abstract

This article proposes a novel adaptive switching control of hypersonic aircraft based on type-2 Takagi–Sugeno–Kang fuzzy sliding mode control and focuses on the problem of stability and smoothness in the switching process. This method uses full-state feedback to linearize the nonlinear model of hypersonic aircraft. Combining the interval type-2 Takagi–Sugeno–Kang fuzzy approach with sliding mode control keeps the adaptive switching process stable and smooth. For rapid stabilization of the system, the adaptive laws use a direct constructive Lyapunov analysis together with an established type-2 Takagi–Sugeno–Kang fuzzy logic system. Simulation results indicate that the proposed control scheme can maintain the stability and smoothness of switching process for the hypersonic aircraft.