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.
Type-2 fuzzy adaptive sliding mode control of hypersonic flight
2019-06-01
14 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Adaptive Sliding Mode Control Design for a Hypersonic Flight Vehicle
Online Contents | 2004
|Adaptive Sliding Mode Control of a Hypersonic Flight Vehicle (AAS 01-240)
British Library Conference Proceedings | 2001
|Adaptive Sliding Mode Control of a Hypersonic Flight Vehicle (AAS 01-240)
British Library Conference Proceedings | 2001
|