Adaptive mode switching of hypersonic morphing aircraft based on type-2 TSK fuzzy sliding mode control View Full Text


Ontology type: schema:ScholarlyArticle     


Article Info

DATE

2015-07

AUTHORS

Xin Jiao, Baris Fidan, Ju Jiang, Mohamed Kamel

ABSTRACT

This paper presents a novel adaptive mode switching scheme for hypersonic morphing aircraftwith retracted winglets based on type-2 Takagi-Sugeno-Kang (TSK) fuzzy sliding mode control. For each ofretracting and stretching modes, a specific sliding mode controller has been adopted. Drawing upon input/outputlinearization to globally linearize the nonlinear model of the hypersonic aircraft at first, a type-2 TSK fuzzylogic system is devised for robust mode switching between these sliding mode controllers. For rapid stabilizationof the system, the adaptive law for mode switching is designed using a direct constructive Lyapunov analysis.Simulation results demonstrate the stability and smooth transition using the proposed switched control scheme. More... »

PAGES

1-15

Identifiers

URI

http://scigraph.springernature.com/pub.10.1007/s11432-015-5349-z

DOI

http://dx.doi.org/10.1007/s11432-015-5349-z

DIMENSIONS

https://app.dimensions.ai/details/publication/pub.1025408129


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