Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/28611
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dc.contributor.authorO. A. Sushchenko-
dc.contributor.authorO. V. Shirokii-
dc.date.accessioned2017-05-30T07:05:04Z-
dc.date.available2017-05-30T07:05:04Z-
dc.date.issued2016-
dc.identifier.issn1990-5548-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/28611-
dc.description.abstractThe paper deals with H2/H∞-approach to design of the inertially stabilized platforms operated at vehicles of the different types including unmanned aerial ones. The formulation of the vector optimization problem is represented. The robust optimization algorithm and results of the synthesied system simulation are shown. Comparative analysis of the results of the parametrical optimization using the Nelder-Mead method and genetic algorithm are given. Proposed approach ensures functioning of the inertially stabilized platforms in the difficult conditions of real operation.uk_UA
dc.language.isoenuk_UA
dc.publisherKyiv, "Osvita Ukrainy"uk_UA
dc.subjectH2/H∞-approach; parametrical synthesis; robust systems; vector optimization; genetic algorithm.uk_UA
dc.subjectH2/H∞-підхід; параметричний синтез; робастні системи; векторна оптимізація; генетичний алгоритм.uk_UA
dc.titleH2/H∞ OPTIMIZATION OF INERTIALLY STABILIZIED PLATFORMSuk_UA
dc.title.alternativeH2/H∞-оптимізація інерціальних стабілізованих платформuk_UA
dc.typeArticleuk_UA
Appears in Collections:Наукові статті кафедри аерокосмічних систем управління

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