Enhancing Dynamic Control and Stability Assessment of Cessna 172 Aircraft with a PID Controller for New Pilot Trainees

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dc.authoridDAGAL, IDRISS/0000-0002-2073-8956
dc.authoridFENDZI MBASSO, Wulfran/0000-0002-4049-0716
dc.authoridHARRISON, AMBE/0000-0002-4353-1261
dc.contributor.authorDagal, Idriss
dc.contributor.authorErol, Bilal
dc.contributor.authorHarrison, Ambe
dc.contributor.authorMbasso, Wulfran Fendzi
dc.contributor.authorIbrahim, AL-Wesabi
dc.date.accessioned2025-03-09T10:49:04Z
dc.date.available2025-03-09T10:49:04Z
dc.date.issued2025
dc.departmentİstanbul Beykent Üniversitesi
dc.description.abstractThis research proposes a novel approach to enhance the dynamic control and stability assessment of the Cessna 172 aircraft for new pilot trainees by incorporating a proportional-integral-derivative (PID) controller. The PID controller is designed to improve the aircraft's responsiveness to control inputs, reduce overshoot and settling time, and enhance overall stability. The study involves developing a mathematical model of the Cessna 172's longitudinal dynamics, designing a PID controller, and conducting simulations to evaluate the performance of the PID-controlled aircraft. The evaluation focuses on key metrics such as stability, responsiveness, overshoot, and settling time. The results of the study demonstrate that the PID controller effectively enhances the dynamic control and stability of the Cessna 172, providing new pilot trainees with a safer and more efficient learning experience. The PID controller's ability to mitigate the effects of pilot errors and disturbances contributes to improved flight performance and reduced risk of accidents. Future research directions include exploring the use of adaptive PID controllers, integrating PID controllers with other advanced flight control systems, and conducting flight tests to validate the performance of the PID-controlled Cessna 172 in real-world conditions.
dc.description.sponsorshipBeykent University
dc.description.sponsorshipThe author declared that this work does not receive any funding.
dc.identifier.doi10.1007/s42405-025-00899-6
dc.identifier.issn2093-274X
dc.identifier.issn2093-2480
dc.identifier.scopus2-s2.0-85217625937
dc.identifier.scopusqualityQ2
dc.identifier.urihttps://doi.org/10.1007/s42405-025-00899-6
dc.identifier.urihttps://hdl.handle.net/20.500.12662/4716
dc.identifier.wosWOS:001415210400001
dc.identifier.wosqualityQ2
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherSpringer
dc.relation.ispartofInternational Journal of Aeronautical and Space Sciences
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_WOS_20250310
dc.subjectAircraft stability
dc.subjectDynamic control
dc.subjectPilot training
dc.subjectPID controller
dc.subjectCessna flight dynamics
dc.titleEnhancing Dynamic Control and Stability Assessment of Cessna 172 Aircraft with a PID Controller for New Pilot Trainees
dc.typeArticle

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