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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">10.17285/0869-7035.2016.24.4.059-075</article-id><article-id custom-type="elpub" pub-id-type="custom">gyroscopy-375</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>Характеристики системы IRNSS при решении задачи позиционирования</article-title><trans-title-group xml:lang="en"><trans-title>Comparative Evaluation of IRNSS Performance with Special Reference to Positional Accuracy</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>Парамешвара</surname><given-names>В. М.</given-names></name><name name-style="western" xml:lang="en"><surname>Vasudha</surname><given-names>M.P.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Парамешвара Васудха Майсур, аспирант.</p></bio><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Гарудачар</surname><given-names>Р.</given-names></name><name name-style="western" xml:lang="en"><surname>Raju</surname><given-names>G.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Гарудачар Раджу, профессор. </p></bio><xref ref-type="aff" rid="aff-2"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru"><institution>Джайнистский университет, факультет электроники и техники связи (Бангалор).</institution><country>Индия</country></aff><aff xml:lang="en"><institution>Jain University, Department of Electronics and Communication Engineering, Bangalore</institution><country>India</country></aff></aff-alternatives><aff-alternatives id="aff-2"><aff xml:lang="ru"><institution>Джайнистский университет, факультет электроники и техники связи, кафедра приборостроения (Бангалор).</institution><country>Индия</country></aff><aff xml:lang="en"><institution>Jain University, Department of Electronics and Communication Engineering, Bangalore</institution><country>India</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2016</year></pub-date><pub-date pub-type="epub"><day>03</day><month>12</month><year>2025</year></pub-date><volume>24</volume><issue>4</issue><fpage>59</fpage><lpage>75</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Парамешвара В., Гарудачар Р., 2025</copyright-statement><copyright-year>2025</copyright-year><copyright-holder xml:lang="ru">Парамешвара В., Гарудачар Р.</copyright-holder><copyright-holder xml:lang="en">Vasudha M., Raju G.</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/375">https://www.gyroscopy.ru/jour/article/view/375</self-uri><abstract><p>Индийская региональная навигационная спутниковая система IRNSS состоит из семи спутников, разработанных Индийской организацией космических исследований (ISRO), и предоставляет два вида услуг: стандартное позиционирование для гражданского применения и позиционирование для пользователей с особыми правами (включая военных) с гарантированной повышенной точностью. Система предназначена как для работы на территории Индии, так и за ее пределами. Область покрытия системы IRNSS включает всю территорию Пакистан и Афганистана, большую часть Китая и Ближнего Востока и Индийский океан. IRNSS является двухчастотной системой и использует сигналы в диапазонах S1 и L5. В настоящее время индийские пользователи имеют доступ и к гражданским сигналам GPS, обеспечивающим погрешность позиционирования на уровне 5 м. Предполагается, что система IRNSS обеспечит погрешность позиционирования не более 10 м на территории Индии и не более 20 м в Индийском океане и на территории, отстоящей от границ Индии до 1500 км. Управление и контроль работы упомянутых семи спутников осуществляют 15 наземных станций, расположенных по всей стране. Сопоставление характеристик IRNSS и GPS показывает, что имеющееся в составе IRNSS число спутников достаточно для региональной навигационной системы и обеспечивает лучшие по сравнению с GPS результаты. В данной работе мы исследовали следующие основные параметры системы: орбитальные характеристики, погрешность позиционирования, включая круговое вероятное отклонение (CEP), вариации в определении вертикальной координаты, фактор геометрического снижения точности (GDOP) в зависимости от количества спутников, а также влияние отношения сигнал/шум (C/N0) и сцинтилляционного эффекта на характеристики GPS и IRNSS. Наш анализ показал, что IRNSS целесообразно использовать как автономную систему.</p></abstract><trans-abstract xml:lang="en"><p>The Indian Regional Navigation Satellite System (IRNSS) is a seven-satellite constellation developed by Indian Space Research Organization (ISRO), India. IRNSS provides two services, with the standard positioning service open for civilian use, and for authorized users (including the military) with an assured absolute positional accuracy. IRNSS is designed to cover all the parts of India and also extending beyond the Indian borders. The coverage area of IRNSS with routes of satellites means and includes area covering entire Pakistan, Afghanistan, most of China and Middle East along with Indian Ocean. IRNSS downlink signals have two bands: S1 band and L5 Band. Presently Indian users are dependent on the civil GPS signals with a positional accuracy of 5 m. IRNSS system is intended to provide an absolute position accuracy of better than 10 m throughout Indian landmass better than 20 m over the Indian Ocean and approximately in a region of 1,500 km around India. There are 15 ground stations across the country responsible for operating and/or monitoring the IRNSS seven satellite constellation. A comparative analysis of IRNSS and GPS navigational satellites shows that the IRNSS consists of sufficient number of satellites for regional navigation system and it can also exhibit better performance. The main parameters selected for our study are orbital characteristics, position accuracy and positional error including Circular Error Probable (CEP), Altitude variation, Geometric Dilution of Precision (GDOP) with respect to Number of Satellites (NSAT), variations in Carrier to Noise (C/N0) ratio and scintillation effect of both GPS and IRNSS satellite systems. Our analysis showed that IRNSS systems shall be used as stand-alone system.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>Погрешность позиционирования</kwd><kwd>круговое вероятное отклонение</kwd><kwd>среднеквадратическая погрешность определения дальности</kwd><kwd>фактор геометрического снижения точности</kwd><kwd>отношение сигнал/шум</kwd><kwd>ионосферная задержка.</kwd></kwd-group><kwd-group xml:lang="en"><kwd>Positional error</kwd><kwd>circular error probable</kwd><kwd>distance root mean squared</kwd><kwd>geometrical dilution of precision</kwd><kwd>carrier to noise ratio</kwd><kwd>iono delay</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">Indian Regional Navigation Satellite System Signal In Space ICD for Standard Positioning Service. Version 1.0, ISROIRNSS-ICD-SPS-1.0. 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