Fast Acting Robust Controller for Pitch Control System

dc.contributor.author	Khuntia, P.S.
dc.contributor.author	Mitra, Debja
dc.date.accessioned	2016-01-21T09:10:01Z
dc.date.available	2016-01-21T09:10:01Z
dc.date.issued	2008
dc.identifier.uri	http://10.11.10.50/xmlui/handle/123456789/3911
dc.description	The Annals of "Dunarea de Jos" University of Galati	en_US
dc.description.abstract	In this paper a classical feedback controller has been designed to furnish fast acting characteristics in the face of parametric perturbation using two parameters, Generalized Time Constant and Characteristic Ratios. The design is extended to develop a controller for the pitch control of a BRAVO fighter aircraft. This design allows reduction of overshoot, control of speed of the response and robust stability with parametric perturbation.	en_US
dc.language.iso	en	en_US
dc.publisher	"Dunarea de Jos' University of Galati	en_US
dc.subject	characteristic ratios	en_US
dc.subject	generalized time constant	en_US
dc.subject	Butterworth polynomial	en_US
dc.title	Fast Acting Robust Controller for Pitch Control System	en_US
dc.type	Article	en_US