Interval type-2 fuzzy PID cascade control of quadrotor based on non-dominated sorting genetic algorithm-II

Abstract It is known that interval type-2 fuzzy logic controllers (IT2FLC) with footprint of uncertainty (FOU) in terms of membership function (MF) have been developed as an effective control method to ensure control in systems where uncertainties and nonlinear situations are high, such as quadrotor control, and have been the subject of many studies. Designing and optimising parameters of IT2FLC controllers is complex and time-consuming. To overcome this situation, an optimisation method based on NSGA-II (Non-dominated Sorting Genetic Algorithm) was applied. ITAE (Integral Time Absolute Error) was chosen as the performance criterion. IT2FLC-NSGA-PID and NSGA-PID controllers were compared and it was observed that the IT2FLC-NSGA-PID controller gave better results. As a result, the superiority of the proposed controller over the other controllers is a better overshoot ratio, a faster settling time, a lower steady state error and a robust system response against uncertainties and disturbances in nonlinear systems.

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Publication Details

Journal
The Aeronautical Journal
Published
2025-05-05
DOI
https://doi.org/10.1017/aer.2024.162
Primary Topic
Fuzzy Logic and Control Systems
Type
article
Field-Weighted Citation Impact
0.00
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article

Interval type-2 fuzzy PID cascade control of quadrotor based on non-dominated sorting genetic algorithm-II

Ö. Fatih Keçecioğlu, Halit Ufacik
The Aeronautical Journal
Fuzzy Logic and Control Systems
article

Interval type-2 fuzzy PID cascade control of quadrotor based on non-dominated sorting genetic algorithm-II

Ö. Fatih Keçecioğlu, Halit Ufacik
article en

Abstract

Abstract It is known that interval type-2 fuzzy logic controllers (IT2FLC) with footprint of uncertainty (FOU) in terms of membership function (MF) have been developed as an effective control method to ensure control in systems where uncertainties and nonlinear situations are high, such as quadrotor control, and have been the subject of many studies. Designing and optimising parameters of IT2FLC controllers is complex and time-consuming. To overcome this situation, an optimisation method based on NSGA-II (Non-dominated Sorting Genetic Algorithm) was applied. ITAE (Integral Time Absolute Error) was chosen as the performance criterion. IT2FLC-NSGA-PID and NSGA-PID controllers were compared and it was observed that the IT2FLC-NSGA-PID controller gave better results. As a result, the superiority of the proposed controller over the other controllers is a better overshoot ratio, a faster settling time, a lower steady state error and a robust system response against uncertainties and disturbances in nonlinear systems.

The Aeronautical JournalVol. 129(1337)
Kahramanmaraş Sütçü İmam University (TR), Gaziantep University (TR)
Openalex Percentile: Top 96%
Fuzzy Logic and Control Systems
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