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

Idriss Dagal; Bilal Erol

Makale detayları

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

Yazarlar:

Idriss Dagal | Bilal Erol

Yayıncı:

Istanbul Ticaret University

Ana Başlıklar:

Otonom Araç Sistemleri

Dergi:

İstanbul Ticaret Üniversitesi Fen Bilimleri Dergisi Vol.23 Issue 45, pp.169-183

Belge Tipi:

Makale

Yayın Tarihi:

6/2024

Belge Dili:

İngilizce

Document ID (Org No.):

2001318569

pISSN:

1305-7820

Anahtar kelimeler:

Özet:

 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 MATLABSimulink 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.

 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 MATLABSimulink 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.

 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 MATLABSimulink 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.

 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 MATLABSimulink 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.

Makale detayları

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

Yazarlar:

Idriss Dagal | Bilal Erol

Yayıncı:

Istanbul Ticaret University

Ana Başlıklar:

Otonom Araç Sistemleri

Dergi:

İstanbul Ticaret Üniversitesi Fen Bilimleri Dergisi Vol.23 Issue 45, pp.169-183

Belge Tipi:

Makale

Yayın Tarihi:

6/2024

Belge Dili:

İngilizce

Document ID (Org No.):

2001318569

pISSN:

1305-7820

FOPID controller

landing

MATLAB/Simulink

runway

performanceFOPID kontrolörü

iniş

MATLAB/Simulink

performans

pist

Sayı

Makale detayları

Yazarlar: Idriss Dagal | Bilal Erol

Yayıncı: Istanbul Ticaret University

Ana Başlıklar: Otonom Araç Sistemleri

Dergi: İstanbul Ticaret Üniversitesi Fen Bilimleri Dergisi Vol.23 Issue 45, pp.169-183

Belge Tipi: Makale

Yayın Tarihi: 6/2024

Belge Dili: İngilizce

Document ID (Org No.): 2001318569

pISSN: 1305-7820

Sayı

Yazarlar:

Idriss Dagal | Bilal Erol

Yayıncı:

Istanbul Ticaret University

Ana Başlıklar:

Otonom Araç Sistemleri

Dergi:

İstanbul Ticaret Üniversitesi Fen Bilimleri Dergisi Vol.23 Issue 45, pp.169-183

Belge Tipi:

Makale

Yayın Tarihi:

6/2024

Belge Dili:

İngilizce

Document ID (Org No.):

2001318569

pISSN:

1305-7820