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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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
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Zusammenfassung: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 aircraft. Fuzzy logic is used to tune each parameter of Proportional-integral-derivative (PID) controller by selecting appropriate fuzzy rules through simulation in Mat lab and Simulink. Comparative assessment based on time response specifications between conventional PID controller with self-tuning fuzzy PID for an autopilot of longitudinal dynamic in pitch aircraft is investigated and analyzed. Simulation results show that, the performance of a pitch control system has improved significantly using self-tuning fuzzy PID compared to conventional PID controller.
ISBN:1467308862
9781467308861
ISSN:2166-0662
DOI:10.1109/ISMS.2012.27