Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/25833
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dc.contributor.authorSergeyev, Igor-
dc.date.accessioned2017-03-29T11:22:26Z-
dc.date.available2017-03-29T11:22:26Z-
dc.date.issued2016-10-
dc.identifier.isbn978-1-5090-1052-3-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/25833-
dc.description.abstractGeneralized structural scheme of the measurement converter which uses iteratively integrating conversion method is described. Analysis of its conversion equation and errors was produced. Basic expressions for the calculation are listed. It is shown that the conversion equation for the steady state does not depend on the conversion coefficients of direct circuit blocks, which affect only a dynamic quality of converter that allows you to set low requirements to the said block at high precision converter as a whole.uk_UA
dc.language.isoen_USuk_UA
dc.publisherKyiv, “Osvita Ukrainy”uk_UA
dc.relation.ispartofseriesCFP1652Y-PRT;IEEE 4th International Conference-
dc.relation.ispartofseriesMethods and Systems of Navigation and Motion Control;210-213-
dc.subjectGeneralized structural scheme; iteratively integrating conversion method; conversion equation; integrator; iterative additive correction of errors; dynamics of the iterative process; steady stateuk_UA
dc.titleGeneralized Structural Scheme of the Measurement Converter Using an Iteratively Integrating Conversion Methoduk_UA
dc.typeArticleuk_UA
Appears in Collections:Матеріали наукових, науково-практичних конференцій кафедри авіаційних комп'ютерно-інтегрованих комплексів

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