Type-2 fuzzy adaptive sliding mode control of hypersonic flight
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所属单位：自动化学院
发表刊物：Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.
摘要：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号：0954-4100
是否译文：否
发表时间：2019-06-01
合写作者：Jiao, Xin,Fidan, Baris,Kamel, Mohamed
通讯作者：江驹