Design of Fuzzy self-tuning PID controller for pitch control system of aircraft autopilot
Nima Beygi, Maani Beigy, Mehdi Siahi

TL;DR
This paper introduces a fuzzy self-tuning PID controller for aircraft autopilot pitch control, demonstrating improved dynamic response and disturbance rejection over conventional PID and proportional controllers through simulation studies.
Contribution
The paper presents a novel fuzzy self-tuning PID controller that adaptively adjusts parameters online, enhancing aircraft pitch control performance especially under disturbances and parameter tuning issues.
Findings
FSPID outperforms CPID and proportional controllers in damping oscillations.
FSPID shows superior anti-disturbance capabilities in short-period simulations.
FSPID adaptively tunes parameters for optimal response despite poor initial tuning.
Abstract
A variety of control systems have been proposed for aircraft autopilot systems. Traditional approaches such as proportional controller and conventional PID (CPID) controller are widely used. PID controller has a good static performance especially for linear and time-invariant systems, but a weak dynamic performance and discouraging function on nonlinear, time-varying, and uncertain systems. Fuzzy control theory can improve dynamic response in various conditions of system performance. This paper designs fuzzy self-tuning PID (FSPID) controller to improve disadvantages of conventional PID in aircraft autopilots. We apply proposed controller to pitch angle of aircraft then the abilities of proposed controller will be compared to the conventional PID and proportional controller. Inner feedback loop acts as oscillation damper in traditional schemes, but here is removed to compare the…
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Taxonomy
TopicsAdaptive Control of Nonlinear Systems · Fuzzy Logic and Control Systems · Advanced Control Systems Design
