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dc.contributor.authorErcan, Hamdi
dc.contributor.authorUlucan, Hamdi
dc.contributor.authorCan, Muharrem Selim
dc.date.accessioned2022-11-10T06:49:45Z
dc.date.available2022-11-10T06:49:45Z
dc.date.issued2022en_US
dc.identifier.citationErcan, H., Ulucan, H., Can, M.S. (20229. Investigation of wind effect on different quadrotors. Aircraft Engineering and Aerospace Technology, 94 (8), pp. 1275-1288. https://doi.org/10.1108/AEAT-09-2021-0288en_US
dc.identifier.issn0002-2667
dc.identifier.urihttps://doi.org/10.1108/AEAT-09-2021-0288
dc.identifier.urihttps://hdl.handle.net/20.500.12508/2229
dc.description.abstractPurpose – Although windy weather conditions have a significant effect on the flight safety and stability of any aircraft, the fact that quadrotors are lighter than other aircraft makes them more sensitive to the wind. This study aims to examine the extent to which quadrotors and their sensors, which are used in many fields and whose use is expected to increase significantly in the future, are affected by wind. Design/methodology/approach – Flight experiments were carried out on different routes assigned by using Pixhawk Holybro 4 and Radiolink flight controllers. In these flight experiments, quadrotors were exposed to winds at different speeds and directions. Findings – In the flight experiments, the deviation amounts in the quadrotor’s route at which wind speed was determined, and it was seen that these deviations were very serious and affected the safe flight at high wind speeds. According to the sensor information obtained from both different quadrotors’ flight experiments at different wind speeds, it was determined that the wind decreased the sensors’ accuracy. Practical implications – It is foreseen that the data obtained in this study will be a source to be used in the design of quadrotors to be used in public areas in the future and to take the wind into account for safe flight. Originality/value – In this study, numerous flight tests were carried out experimentally at various speeds from low speeds to high speeds on different routes using different flight controllers. The deviation data on the obtained routes and the effect of the wind on the sensors are experienced in real atmospheric conditions.en_US
dc.language.isoengen_US
dc.publisherEmerald Group Holdings Ltd.en_US
dc.relation.isversionof10.1108/AEAT-09-2021-0288en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectQuadrotoren_US
dc.subjectWind effecten_US
dc.subjectTrajectory trackingen_US
dc.subject.classificationController
dc.subject.classificationAltitude Control
dc.subject.classificationVertical Takeoff and Landing
dc.subject.classificationEngineering
dc.subject.classificationElectrical Engineering, Electronics & Computer Science - Automation & Control Systems - Multi Agent Systems
dc.subject.otherAircraft
dc.subject.otherWind effects
dc.subject.otherDesign/methodology/approach
dc.subject.otherExposed to
dc.subject.otherFlight controllers
dc.subject.otherFlight experiments
dc.subject.otherFlight safety
dc.subject.otherFlight stability
dc.subject.otherQuad rotors
dc.subject.otherSafety and stabilities
dc.subject.otherTrajectory-tracking
dc.subject.otherWind speed
dc.titleInvestigation of wind effect on different quadrotorsen_US
dc.typearticleen_US
dc.relation.journalAircraft Engineering and Aerospace Technologyen_US
dc.contributor.departmentHavacılık ve Uzay Bilimleri Fakültesi -- Havacılık Elektrik ve Elektroniği Bölümüen_US
dc.identifier.volume94en_US
dc.identifier.issue8en_US
dc.identifier.startpage1275en_US
dc.identifier.endpage1288en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.contributor.isteauthorCan, Muharrem Selim
dc.relation.indexWeb of Science - Scopusen_US
dc.relation.indexWeb of Science Core Collection - Science Citation Index Expanded


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