Avionics Design for a Subsonic Rocket Carrying a Scientific Experiment Unit

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dc.contributor.authorBakirci, Murat
dc.contributor.authorOzer, Muhammed Mirac
dc.date.accessioned2025-03-17T12:25:39Z
dc.date.available2025-03-17T12:25:39Z
dc.date.issued2022
dc.departmentTarsus Üniversitesi
dc.description2nd International Conference on Computing and Machine Intelligence (ICMI) -- JUL 15-16, 2022--AG289 Istanbul, TURKEY
dc.description.abstractIn this study, the avionics system of a solid propellant rocket flying at subsonic speed, which can carry, distribute and safely recover a payload carrying out a scientific experiment unit at an altitude of 10000 feet, is designed within the scope of the specified functionality and requirements of the system. The main avionics system is designed to contain components used to document flight data, transmit them instantaneously to the ground station, and perform recovery. In addition, a redundant avionics system has been designed to ensure safe operation and recovery in case of potential problems. Based on the analysis of the system requirements, an avionics system scheme has been proposed that offers efficient, low-cost, reliable flight and mission capability. Methods of minimizing the effects of in-flight vibrational effects on the payload and avionics system were also discussed. All analyzes and tests of the designed systems are provided to ensure that engineers extract as much information as possible to verify the design, ensure a safe flight and a successful payload mission.
dc.description.sponsorshipIEEE Turkey Sect,Istanbul Atlas Univ, Dept Comp Engn
dc.identifier.doi10.1109/ICMI55296.2022.9873799
dc.identifier.endpage153
dc.identifier.isbn978-1-6654-7484-9
dc.identifier.isbn978-1-6654-7483-2
dc.identifier.scopus2-s2.0-85139010253
dc.identifier.scopusqualityN/A
dc.identifier.startpage148
dc.identifier.urihttps://doi.org/10.1109/ICMI55296.2022.9873799
dc.identifier.urihttps://hdl.handle.net/20.500.13099/1800
dc.identifier.wosWOS:001340389000030
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherIeee
dc.relation.ispartof2022 2nd International Conference On Computing and Machine Intelligence, Icmi 2022
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WOS_20250316
dc.subjectrocket avionics
dc.subjectconceptual design
dc.subjectflight computer
dc.subjectMEMS sensors
dc.subjectsystem architecture
dc.titleAvionics Design for a Subsonic Rocket Carrying a Scientific Experiment Unit
dc.typeConference Object

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