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<article article-type="research-article" dtd-version="1.3" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xml:lang="ru"><front><journal-meta><journal-id journal-id-type="publisher-id">caht</journal-id><journal-title-group><journal-title xml:lang="ru">Научный вестник МГТУ ГА</journal-title><trans-title-group xml:lang="en"><trans-title>Civil Aviation High Technologies</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">2079-0619</issn><issn pub-type="epub">2542-0119</issn><publisher><publisher-name>Moscow State Technical University of Civil Aviation (MSTU CA)</publisher-name></publisher></journal-meta><article-meta><article-id custom-type="elpub" pub-id-type="custom">caht-864</article-id><article-categories><subj-group subj-group-type="heading"><subject>Research Article</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="ru"><subject>Статьи</subject></subj-group></article-categories><title-group><article-title>ВОПРОСЫ ИЗБЫТОЧНОСТИ В ЗАДАЧЕ ОПРЕДЕЛЕНИЯ МЕСТОПОЛОЖЕНИЯ ВОЗДУШНОГО СУДНА РАЗНОСТНО-ВРЕМЕННЫМ МЕТОДОМ</article-title><trans-title-group xml:lang="en"><trans-title>REDUNDANCY IN TDOA METHOD OF AIRCRAFT POSITION ESTIMATION</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Машошин</surname><given-names>А. О.</given-names></name><name name-style="western" xml:lang="en"><surname>Mashoshin</surname><given-names>A. O.</given-names></name></name-alternatives><bio xml:lang="ru"><p>аспирант кафедры ОРТЗИ</p></bio><email xlink:type="simple">tonches918@gmail.com</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff xml:lang="ru" id="aff-1"><institution>МГТУ ГА</institution><country>Russian Federation</country></aff><pub-date pub-type="collection"><year>2016</year></pub-date><pub-date pub-type="epub"><day>27</day><month>12</month><year>2016</year></pub-date><volume>0</volume><issue>224</issue><fpage>147</fpage><lpage>156</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Машошин А.О., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Машошин А.О.</copyright-holder><copyright-holder xml:lang="en">Mashoshin A.O.</copyright-holder><license xml:lang="ru" license-type="creative-commons-attribution" xlink:href="https://creativecommons.org/licenses/by/4.0/" xlink:type="simple"><license-p>Данная работа распространяется под лицензией Creative Commons Attribution 4.0.</license-p></license><license xml:lang="en" license-type="creative-commons-attribution" xlink:href="https://creativecommons.org/licenses/by/4.0/" xlink:type="simple"><license-p>This work is licensed under a Creative Commons Attribution 4.0 License.</license-p></license></permissions><self-uri xlink:href="https://avia.mstuca.ru/jour/article/view/864">https://avia.mstuca.ru/jour/article/view/864</self-uri><abstract><p>В статье рассмотрены основные методы решения уравнений с избыточностью для последующего моделирования наземной многопозиционной системы как части системы анализа аэронавигационных данных. Рассмотрены такие математические модели, как метод наименьших квадратов и метод рядов Тейлора. Произведено математическое моделирование с учетом случайных факторов, влияющих на результат работы системы. Определены факторы, оказывающие наибольшее влияние на точностные характеристики наземной многопозиционной системы, проведен сравнительный анализ математических моделей.</p></abstract><trans-abstract xml:lang="en"><p>The paper deals with the main methods for solving equations with redundancy. It is subsequently used for modelling the ground many-positional system as a part of a system for analysis of air navigation data as a whole. In particular, the least square method and the Taylor series method are modelled taking into account the impact of stochastic factors influencing the system output. The factors with maximal effect on the accuracy of the functioning of the ground many-positional system are determined; a comparative analysis of the methods is carried on.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>АЗН-В</kwd><kwd>информационная безопасность</kwd><kwd>РВП</kwd><kwd>линейный МНК</kwd><kwd>метод рядов Тейлора</kwd></kwd-group><kwd-group xml:lang="en"><kwd>ADS-B</kwd><kwd>TDOA</kwd><kwd>Information Security</kwd><kwd>Least Squares</kwd><kwd>Taylor series</kwd></kwd-group></article-meta></front><back><ref-list><title>References</title><ref id="cit1"><label>1</label><citation-alternatives><mixed-citation xml:lang="ru">Концепция создания и развития Аэронавигационной системы России (одобрена на заседании Правительства Российской Федерации от 4 октября 2006 г.). 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