FRACTIONAL ORDER-BASED PID CONTROLLER DESIGN WITH GENETIC ALGORITHM (FOPID-GA) FOR AIRCRAFT LANDING GEAR SHOCK ABSORBER MECHANISM

Yıl 2024, , 169 - 183, 26.06.2024

Idriss Dagal , Bilal Erol

https://doi.org/10.55071/ticaretfbd.1479499

Öz

Deterioration conditions of the runway surface (deep track, cracking, raveling, and potholes ) and contaminants greatly affect the landing performance of the aircraft. In this research study, an optimal fractional order proportional integral and derivative controller (FOPID-GA) is designed with a genetic algorithm for the smooth operation of aircraft landing gear systems. To prove the effectiveness, performance, and accuracy of the proposed approach, a comparative study of the new technique and the traditional controllers such as PID, PID-TD, FOPID-TD, and PID-GA controllers was conducted on the MATLAB/Simulink platform. The simulation results clearly show that the proposed FOPID-GA controller outperforms the existing controllers in terms of performance, and damping accuracy. The effectiveness of the FOPID-GA controller is evaluated through simulation studies, demonstrating its potential to enhance aircraft landing gear performance and safety under adverse conditions.

Anahtar Kelimeler

FOPID controller, landing, MATLAB/Simulink, runway, performance

Proje Numarası

Fractional Order based PID Controller Design with Genetic Algorithm (FOPID-GA) for Aircraft Landing Gear Shock Absorber Mechanism

UÇAK İNİŞ TAKIMI AMORTİSÖR MEKANİZMASI İÇİN KESİR DERECELİ PID KONTROLÖRÜN GENETİK ALGORİTMA (FOPID-GA) İLE TASARIMI

Öz

Hava araçlarına yönelik pist yüzlerinde meydana gelen bozulmalar (derin iz, çatlama, çökme ve çukurlar) ve kirletici yabancı maddeler uçağın iniş performansını büyük ölçüde etkiler. Bu çalışmada, uçak iniş takımı sistemlerinin sorunsuz çalışması için genetik algoritma kullanılarak, optimal kesirli dereceli oransal integral ve türev kontrolör (FOPID-GA) tasarlanmıştır. Önerilen yaklaşımın etkinliğini, performansını ve doğruluğunu göstermek amacıyla, PID, PID-TD, FOPID-TD ve PID-GA kontrolörleri gibi geleneksel kontrolörlerin MATLAB/Simulink platformu üzerinde karşılaştırmalı bir çalışması yapılmıştır. Simülasyon sonuçları, önerilen FOPID-GA denetleyicinin performans ve sönümleme doğruluğu açısından mevcut geleneksel kontrolörlerden daha iyi performans gösterdiğini açıkça göstermektedir. FOPID-GA kontrolörünün etkinliği simülasyon çalışmaları ile irdelenmiş, olumsuz koşullar altında uçak iniş takımı performansını ve güvenliğini artırma potansiyeli gösterilmiştir.

Anahtar Kelimeler

FOPID kontrolörü, iniş, MATLAB/Simulink, performans, pist

Etik Beyan

No funding has been acknowledged for this work

Destekleyen Kurum

Not applicable for this manuscript

Proje Numarası

Fractional Order based PID Controller Design with Genetic Algorithm (FOPID-GA) for Aircraft Landing Gear Shock Absorber Mechanism

Kaynakça

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