Fast Acting Robust Controller for Pitch Control System of Aircraft

  • P. S. Khuntia Durgapur Institute of Advanced Technology and Management
  • Debjani Mitra Indian School of Mines, Dhanbad
Keywords: characteristic ratios, generalized time constant, Butterworth polynomial, overshoot reduction

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.

Published
2008-06-30
How to Cite
1.
Khuntia P, Mitra D. Fast Acting Robust Controller for Pitch Control System of Aircraft. The Annals of “Dunarea de Jos“ University of Galati. Fascicle III, Electrotechnics, Electronics, Automatic Control, Informatics [Internet]. 30Jun.2008 [cited 4May2024];31(1):67-5. Available from: https://www.gup.ugal.ro/ugaljournals/index.php/eeaci/article/view/655
Issue
Vol 31 No 1 (2008)
Section
Articles

@ "Dunarea de Jos" University of Galati

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