Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/36063
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dc.contributor.authorSineglazov, V.M.-
dc.contributor.authorDolgorukov, S.O.-
dc.date.accessioned2018-09-17T10:37:23Z-
dc.date.available2018-09-17T10:37:23Z-
dc.date.issued2017-10-
dc.identifier.isbn978-1-5386-1816-5-
dc.identifier.otherIEEE Catalog Number: CFP1729V-PRT-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/36063-
dc.description.abstractThe paper considers dynamic test table system for navigation sensors testing and verification. The problem of test table confidence margin is considered taking into account different sources of errors. Estimation of frequency characteristics of sensors is shown by special test table criteria.The paper describes inertial navigation system experiment on dynamic test table in order to compensate navigation system parameters.uk_UA
dc.publisherKyiv, “Osvita Ukrainy”uk_UA
dc.relation.ispartofseriesIEEE 4th International Conference;October 17-19, 2017, Kyiv, Ukraine-
dc.relation.ispartofseries“Actual Problems of Unmanned Aerial Vehicles Developments” (APUAVD);211-214-
dc.subjectNavigation systemuk_UA
dc.subjectthree-axis test tableuk_UA
dc.subjectunmanned aerial vehicleuk_UA
dc.subjectdynamic test table systemuk_UA
dc.titleDynamic Testing of UAV Navigation Systemuk_UA
dc.typeTechnical Reportuk_UA
dc.specialityUAV Equipmentuk_UA
Appears in Collections:Матеріали наукових, науково-практичних конференцій кафедри авіаційних комп'ютерно-інтегрованих комплексів

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