Self-Tuning Fuzzy PID Controller Design for Aircraft Pitch Control

In this paper self-tuning fuzzy PID controller is developed to improved the performance for a pitch control of aircraft system. The controller is designed based on the dynamic modeling of system begins with a derivation of suitable mathematical model to describe the longitudinal motion of an aircraf...

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Vydané v:	2012 Third International Conference on Intelligent Systems Modelling and Simulation s. 19 - 24
Hlavní autori:	Wahid, Nurbaiti, Hassan, Nurhaffizah
Médium:	Konferenčný príspevok..
Jazyk:	English
Vydavateľské údaje:	IEEE 01.02.2012
Predmet:	Aerospace control Aircraft Atmospheric modeling autopilot Control systems Equations flight control Fuzzy logic longitudinal dynamics Mathematical model PID pitch self-tuning fuzzy PID
ISBN:	1467308862, 9781467308861
ISSN:	2166-0662
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