Dynamic Testing of UAV Navigation System

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.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.identifier.isbn978-1-5386-1816-5
dc.identifier.otherIEEE Catalog Number: CFP1729V-PRT
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/36063
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.specialityUAV Equipmentuk_UA
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

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