Type 2 Fuzzy Control for Twin Rotor

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DC Field	Value	Language
dc.contributor.author	Reguibi, Noureddine	-
dc.contributor.author	Bahloul, Omar	-
dc.date.accessioned	2015-05-05T10:04:54Z	-
dc.date.available	2015-05-05T10:04:54Z	-
dc.date.issued	2015-05-05	-
dc.identifier.issn	YA	-
dc.identifier.uri	http://dspace.univ-ouargla.dz/jspui/handle/123456789/8575	-
dc.description	University of Kasdi Merbah Ouargla Faculty of New Technology of Information and Communiction Department of Electronics and Communications	en_US
dc.description.abstract	The helicopter dynamic includes nonlinearities, parametric uncertainties and is subject to unknown external disturbances. Such complicated dynamics involve designing sophisticated control algorithms that can deal with these difficulties. In this paper, a type 2 fuzzy logic controller is proposed for TRMS (twin rotor mimo-system) control problem. Using triangular membership functions and based on a human operator experience, two controllers are designed to control the position of the yaw and the pitch angles of the TRMS. Simulation results are given to illustrate the effectiveness of the proposed control scheme.	en_US
dc.description.sponsorship	Kafi Mohammed Redouane	en_US
dc.language.iso	en	en_US
dc.relation.ispartofseries	2015;	-
dc.subject	Type 2 fuzzy logic	en_US
dc.subject	Dynamic modeling	en_US
dc.subject	TRMS system	en_US
dc.subject	Nonlinear system	en_US
dc.title	Type 2 Fuzzy Control for Twin Rotor	en_US
dc.type	Article	en_US
Appears in Collections:	Département des télécommunications et contrôle Mastériales

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