Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/28340
Full metadata record
DC FieldValueLanguage
dc.contributor.authorV. V. Chikovani-
dc.contributor.authorH. V.Tsiruk-
dc.date.accessioned2017-05-26T10:11:01Z-
dc.date.available2017-05-26T10:11:01Z-
dc.date.issued2014-
dc.identifier.issn1990-5548-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/28340-
dc.description.abstractThis work presents investigation of differential Coriolis vibratory gyroscope ability to external shock suppression. First of all pulse amplitude in voltage caused by external mechanical shock of 100 g is estimated for the two sensor designs. Then, using differential Coriolis vibratory gyroscope Simulink model, output signals of two measurement channels are analyzed. It is shown that differential Coriolis vibratory gyroscope damps amplitude of erroneous angle rate caused by shock directed along sensing axis of no less than 3 times in comparison with non differential Coriolis vibratory gyroscope. Influence of lateral shock is also analyzeduk_UA
dc.language.isoenuk_UA
dc.publisherВД "Освіта України"uk_UA
dc.relation.ispartofseriesElectronics and Control Systems;№ 4(42): 79-83-
dc.subjectDifferential Coriolis vibratory gyroscope; shock; error angle rateuk_UA
dc.titleSHOCK RESISTANCE OF DIFFERENTIAL TYPE RING-LIKE RESONATOR VIBRATORY GYROSCOPEuk_UA
dc.typeArticleuk_UA
Appears in Collections:Наукові статті кафедри аерокосмічних систем управління

Files in This Item:
File Description SizeFormat 
Chikovani_EACS 4_2014.pdf413.09 kBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.