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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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
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spelling doaj-d4cd83f85528443595971575385538222020-11-24T20:40:25ZengUniversitatea Dunarea de JosAnalele Universităţii "Dunărea de Jos" Galaţi: Fascicula III, Electrotehnică, Electronică, Automatică, Informatică1221-454X2008-07-013116775Fast Acting Robust Controller for Pitch Control System of AircraftP. S. KHUNTIADebjani MITRAIn 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.http://www.ann.ugal.ro/eeai/archives/2008/Lucrare-11-Khuntia1.pdfcharacteristic ratiosgeneralized time constantButterworth polynomialovershoot reduction
collection DOAJ
language English
format Article
sources DOAJ
author P. S. KHUNTIA
Debjani MITRA
spellingShingle P. S. KHUNTIA
Debjani MITRA
Fast Acting Robust Controller for Pitch Control System of Aircraft
Analele Universităţii "Dunărea de Jos" Galaţi: Fascicula III, Electrotehnică, Electronică, Automatică, Informatică
characteristic ratios
generalized time constant
Butterworth polynomial
overshoot reduction
author_facet P. S. KHUNTIA
Debjani MITRA
author_sort P. S. KHUNTIA
title Fast Acting Robust Controller for Pitch Control System of Aircraft
title_short Fast Acting Robust Controller for Pitch Control System of Aircraft
title_full Fast Acting Robust Controller for Pitch Control System of Aircraft
title_fullStr Fast Acting Robust Controller for Pitch Control System of Aircraft
title_full_unstemmed Fast Acting Robust Controller for Pitch Control System of Aircraft
title_sort fast acting robust controller for pitch control system of aircraft
publisher Universitatea Dunarea de Jos
series Analele Universităţii "Dunărea de Jos" Galaţi: Fascicula III, Electrotehnică, Electronică, Automatică, Informatică
issn 1221-454X
publishDate 2008-07-01
description 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.
topic characteristic ratios
generalized time constant
Butterworth polynomial
overshoot reduction
url http://www.ann.ugal.ro/eeai/archives/2008/Lucrare-11-Khuntia1.pdf
work_keys_str_mv AT pskhuntia fastactingrobustcontrollerforpitchcontrolsystemofaircraft
AT debjanimitra fastactingrobustcontrollerforpitchcontrolsystemofaircraft
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