Type-2 fuzzy adaptive sliding mode control of hypersonic flight-Reference-Cited by-同舟云学术

Type-2 fuzzy adaptive sliding mode control of hypersonic flight

Published:2017-07-12 Issue:8 Volume:233 Page:2731-2744
ISSN:0954-4100
Container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Author:

Jiao Xin¹,Fidan Baris²,Jiang Ju¹,Kamel Mohamed³

Affiliation:

1. Deparment of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing, China

2. Department of Mechanical and Mechatronics Engineering, University of Waterloo, Waterloo, ON, Canada

3. Department of Electrical and Computer Engineering, University of Waterloo, Waterloo, ON, Canada

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.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1177/0954410017712329

Reference29 articles.

1. Robust Nonlinear Control of a Hypersonic Aircraft

2. Adaptive Sliding Mode Control Design for a Hypersonic Flight Vehicle

3. Robust nonlinear flight control of a high-performance aircraft

4. Robust Linear Output Feedback Control of an Airbreathing Hypersonic Vehicle

5. Nonlinear Robust Adaptive Control of Flexible Air-Breathing Hypersonic Vehicles

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