%0 Journal Article
%T Fast Acting Robust Controller for Pitch Control System of Aircraft
%A P. S. KHUNTIA
%A Debjani MITRA
%J Annals of Dunarea de Jos
%D 2008
%I Universitatea Dunarea de Jos
%X 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.
%K characteristic ratios
%K generalized time constant
%K Butterworth polynomial
%K overshoot reduction
%U http://www.ann.ugal.ro/eeai/archives/2008/Lucrare-11-Khuntia1.pdf