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

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dc.contributor.authorDagal, Idrıss
dc.contributor.authorErol, Bilal
dc.date.accessioned2025-03-09T10:53:15Z
dc.date.available2025-03-09T10:53:15Z
dc.date.issued2024
dc.departmentİstanbul Beykent Üniversitesi
dc.description.abstractDeterioration 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.
dc.identifier.doi10.55071/ticaretfbd.1479499
dc.identifier.endpage183
dc.identifier.issn1305-7820
dc.identifier.issn2587-165X
dc.identifier.issue45
dc.identifier.startpage169
dc.identifier.trdizinid1243483
dc.identifier.urihttps://doi.org/10.55071/ticaretfbd.1479499
dc.identifier.urihttps://search.trdizin.gov.tr/tr/yayin/detay/1243483
dc.identifier.urihttps://hdl.handle.net/20.500.12662/4759
dc.identifier.volume23
dc.indekslendigikaynakTR-Dizin
dc.language.isoen
dc.relation.ispartofİstanbul Ticaret Üniversitesi Fen Bilimleri Dergisi
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_TR_20250310
dc.subjectMATLAB/Simulink
dc.subjectFOPID controller
dc.subjectlanding
dc.subjectrunway
dc.subjectperformance.
dc.titleFRACTIONAL ORDER-BASED PID CONTROLLER DESIGN WITH GENETIC ALGORITHM (FOPID-GA) FOR AIRCRAFT LANDING GEAR SHOCK ABSORBER MECHANISM
dc.typeArticle

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