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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">gyroscopy</journal-id><journal-title-group><journal-title xml:lang="ru">Гироскопия и навигация</journal-title><trans-title-group xml:lang="en"><trans-title>Giroskopiya i Navigatsiya</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">0869-7035</issn><issn pub-type="epub">2075-0927</issn><publisher><publisher-name>AO «Концерн «ЦНИИ «Электроприбор»</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.17285/0869-7035.2015.23.4.173-182</article-id><article-id custom-type="elpub" pub-id-type="custom">gyroscopy-345</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>Грубая выставка вертикали безгироскопной инерциальной навигационной системы</article-title><trans-title-group xml:lang="en"><trans-title>Gyro-free INS coarse alignment</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>Вакнин</surname><given-names>Е.</given-names></name><name name-style="western" xml:lang="en"><surname>Vaknin</surname><given-names>E.</given-names></name></name-alternatives><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Клейн</surname><given-names>И.</given-names></name><name name-style="western" xml:lang="en"><surname>Klein</surname><given-names>I.</given-names></name></name-alternatives><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru"><institution>Rafael Advanced Defense Systems Ltd., Хайфа</institution><country>Израиль</country></aff><aff xml:lang="en"><institution>Rafael Advanced Defense Systems Ltd.</institution><country>Israel</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2016</year></pub-date><pub-date pub-type="epub"><day>01</day><month>12</month><year>2025</year></pub-date><volume>24</volume><issue>1</issue><fpage>173</fpage><lpage>182</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Вакнин Е., Клейн И., 2025</copyright-statement><copyright-year>2025</copyright-year><copyright-holder xml:lang="ru">Вакнин Е., Клейн И.</copyright-holder><copyright-holder xml:lang="en">Vaknin E., Klein I.</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://www.gyroscopy.ru/jour/article/view/345">https://www.gyroscopy.ru/jour/article/view/345</self-uri><abstract><p>Грубая выставка на неподвижном основании используется для начального определения ориентации инерциальной навигационной системы (ИНС) с помощью векторов силы тяжести и угловой скорости вращения Земли. В безгироскопной ИНС используются только акселерометры, следовательно, в такой системе невозможно измерить и вычислить угол рыскания. В статье описывается процесс грубой выставки вертикали и выводятся характеристики погрешностей безгироскопной системы, сравниваются различные конфигурации акселерометров.</p></abstract><trans-abstract xml:lang="en"><p>For a stationary system, coarse alignment is used to initially determine the orientation of the INS by utilizing the Earth gravity and rotation vectors. Yet, a gyro-free INS has only accelerometers and hence cannot measure the Earth rotation vector and thus cannot deduce its yaw angle. In this paper, we formulate the coarsealignment procedure and derive error characteristics for a gyro-free system. In addition, a comparison between different configurations of accelerometers is being conducted.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>Грубая выставка</kwd><kwd>точная выставка</kwd><kwd>вертикаль</kwd><kwd>безгироскопная инерциальная навигационная система</kwd><kwd>неподвижная система</kwd><kwd>акселерометр</kwd><kwd>векторы силы тяжести и угловой скорости вращения Земли.</kwd></kwd-group><kwd-group xml:lang="en"><kwd>Сoarse alignment</kwd><kwd>fine alignment</kwd><kwd>gyro-free INS</kwd><kwd>stationary system</kwd><kwd>accelerometer</kwd><kwd>Earth gravity and rotation vectors.</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">Titterton, D.H. and Weston J.L, Strapdown Inertial Navigation Technology, The Institution of Electrical Engineers, 2004.</mixed-citation><mixed-citation xml:lang="en">Titterton, D.H. and Weston J.L, Strapdown Inertial Navigation Technology, The Institution of Electrical Engineers, 2004.</mixed-citation></citation-alternatives></ref><ref id="cit2"><label>2</label><citation-alternatives><mixed-citation xml:lang="ru">Britting, K.R., Inertial Navigation Systems Analysis, John Wiley &amp; Sons Inc., 1971. 3. 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