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Development of a MEMs-Based IMU Unit

dc.contributor.authorKocer, Basaran Bahadir
dc.contributor.authorOmurlu, Vasfi Emre
dc.contributor.authorAkdogan, Erhan
dc.contributor.authorTufekci, Celal Sami
dc.date.accessioned2026-06-27T13:27:30Z
dc.date.issued2013
dc.description.abstractIn this study, gyroscope-free inertial measurement unit interface is developed to simulate new system configurations called YILDIZ using known calculation methods and implementation of MEMs accelerometers based on cubic arrangement. Additionally significant effect of different sensing directions and sensor allocations are taken into consideration. Throughout the project, simulation studies, realization of sample gyro-free MEMs-based INS systems, and collection of data through data acquisition systems are performed in given order. Using simulation of the system, parameter-dependent errors are aimed to be minimized on the system output. Then, near-ideal geometry and the sensor configurations can be reached and the system can be realized. Prototype outputs are processed and efficient algorithms are developed using Matlab-Simulink environment.en
dc.identifier.endpage393
dc.identifier.isbn978-1-4673-6396-9; 978-1-4673-6395-2
dc.identifier.startpage389
dc.identifier.urihttps://hdl.handle.net/20.500.14981/52796
dc.identifier.wos000332043900055
dc.language.isoeng
dc.publisherIEEE
dc.relation.conference6th International Conference on Recent Advances in Space Technologies (RAST)
dc.relation.ispartofPROCEEDINGS OF 6TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST 2013)
dc.subjectInertial Measurement Unit
dc.subjectMEMs
dc.subjectGF-INS
dc.subjectEngineering
dc.titleDevelopment of a MEMs-Based IMU Unit
dc.typeProceedings Paper
dspace.entity.typePublication
local.import.sourceWOS

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