Fast Acting Robust Controller for Pitch Control System of Aircraft

Fast Acting Robust Controller for Pitch Control System of Aircraft

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 fig...

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Bibliographic Details
Main Authors: P. S. KHUNTIA, Debjani MITRA
Format: Article
Language:English
Published: Universitatea Dunarea de Jos 2008-07-01
Series:Analele Universităţii "Dunărea de Jos" Galaţi: Fascicula III, Electrotehnică, Electronică, Automatică, Informatică
Subjects:
characteristic ratios
generalized time constant
Butterworth polynomial
overshoot reduction
Online Access:http://www.ann.ugal.ro/eeai/archives/2008/Lucrare-11-Khuntia1.pdf
Description
Summary: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.
ISSN:1221-454X

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