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...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	2012 Third International Conference on Intelligent Systems Modelling and Simulation S. 19 - 24
Hauptverfasser:	Wahid, Nurbaiti, Hassan, Nurhaffizah
Format:	Tagungsbericht
Sprache:	Englisch
Veröffentlicht:	IEEE 01.02.2012
Schlagworte:	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
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!