Design and Implementation of A Low-Cost Parachute Landing System for Fixed-Wing Mini Unmanned Aerial Vehicles

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dc.authorid0000-0003-3348-3814
dc.authorid0000-0001-8663-241X
dc.contributor.authorKırteke, Emre
dc.contributor.authorYıldırım Dalkıran, Fatma
dc.date.accessioned2025-02-05T09:59:06Z
dc.date.available2025-02-05T09:59:06Z
dc.date.issued2024en_US
dc.departmentKapadokya Üniversitesi, Kapadokya Meslek Yüksekokulu, Uçak Teknolojisi Bölümü
dc.description.abstractFixed-wing mini-UAVs (Unmanned Aerial Vehicles) face difficulties due to the need for runways during take-off and landing. While fixed-wing UAVs are capable of using catapults during take-off, various landing systems are required for landing. Therefore, in this study, a parachute system design and production were carried out for the safe landing of fixed-wing mini-UAVs. The produced parachute utilized ultra-lightweight ripstop nylon fabric and suspension lines, while a carbon fiber tube was chosen for the launching system for its lightweight and strength. The parachute deployment system was triggered by a servo motor with low power consumption and high torque. During tests, the parachute was activated at a height of 47 meters during flight. The parachute deployment was completed in 1.42 seconds, and the descent with the parachute lasted 11 seconds. The vertical descent speed of the parachute during landing was measured at 4.27 m/s. The produced parachute landing system was manufactured at 71% lower cost compared to existing parachute landing systems in the literature and on the market. Additionally, the ultra-light ripstop parachute weighed 56 grams, making it 12% lighter than similar systems. Considering the advantages in terms of cost and weight, it is anticipated that parachute landing systems will be increasingly used for fixed-wing UAVs in the future.
dc.identifier.citationYıldırım Dalkıran, F., & Kırteke, E. (2024). Design and Implementation of A Low-Cost Parachute Landing System for Fixed-Wing Mini Unmanned Aerial Vehicles. Journal of Aviation, 8(3), 198-205.
dc.identifier.endpage205en_US
dc.identifier.issn2587-1676
dc.identifier.issue3en_US
dc.identifier.startpage198en_US
dc.identifier.urihttps://doi.org/10.30518/jav.1479457
dc.identifier.urihttps://hdl.handle.net/20.500.12695/3217
dc.identifier.volume8en_US
dc.institutionauthorKırteke, Emre
dc.language.isoen
dc.relation.ispartofJournal of Aviation
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectFixed UAV
dc.subjectParachute
dc.subjectParachute Landing System
dc.subjectParachute Fabric
dc.titleDesign and Implementation of A Low-Cost Parachute Landing System for Fixed-Wing Mini Unmanned Aerial Vehicles
dc.typeArticle

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