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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-824</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>УПРАВЛЕНИЕ МОЩНОСТЬЮ ПСЕВДОСПУТНИКА ПРИ ЗАХОДЕ НА ПОСАДКУ ВОЗДУШНОГО СУДНА</article-title><trans-title-group xml:lang="en"><trans-title>POWER CONTROL OF PSEUDOLITES WHILE LANDING AN AIRCRAFT</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>Ерохин</surname><given-names>В. В.</given-names></name><name name-style="western" xml:lang="en"><surname>Erokhin</surname><given-names>V. V.</given-names></name></name-alternatives><bio xml:lang="ru"><p>кандидат технических наук, доцент, доцент кафедры АРЭО ИФ</p></bio><email xlink:type="simple">ww-erohin@mail.ru</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>28</day><month>11</month><year>2016</year></pub-date><volume>0</volume><issue>226</issue><fpage>54</fpage><lpage>61</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Ерохин В.В., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Ерохин В.В.</copyright-holder><copyright-holder xml:lang="en">Erokhin V.V.</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/824">https://avia.mstuca.ru/jour/article/view/824</self-uri><abstract><p>Исследовано влияние сигнала псевдоспутника (ПС) на качество функционирования ГЛОНАСС/GPS приемников спутниковой навигации и получено экспериментальное подтверждение проявлению эффекта «ближний-дальний» с помощью программно-аппаратного комплекса NI GPS Simulation Toolkit. Синтезирован алгоритм оптимального управления мощностью ПС на основе оценки времени задержки сигнала в линии передачи данных. Показано, что реализация предложенного алгоритма оптимального управления позволяет устранить проявление эффекта «ближний-дальний» и обеспечить одновременный прием сигналов навигационных спутников ГЛОНАСС/GPS и ПС.</p></abstract><trans-abstract xml:lang="en"><p>The effect of a pseudolite (PL) signal on quality of functioning of the GLONASS/GPS receivers of satellite navigation has been researched and experimental confirmation of near-far effect developing with the help of NI GPS Simulation Toolkit hardware and software has been obtained. An algorithm of an optimal power control has been obtained. PL based on the evaluation of the signal delay time in data transfer line has been synthesized. The analysis of the simulation results showed that the implementation of the proposed optimal control algorithm allows eliminating the effect “near-far” developing and ensuring simultaneous reception of signals of GLONASS/GPS satellite and PL.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>псевдоспутник</kwd><kwd>оптимальное управление мощностью</kwd><kwd>время задержки сигнала</kwd><kwd>УКВ линия передачи данных</kwd></kwd-group><kwd-group xml:lang="en"><kwd>pseudolite</kwd><kwd>optimal power control</kwd><kwd>delay time of the signal</kwd><kwd>VHF data line</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">Крыжановский Г.А. Концепция и системы CNS/ATM в гражданской авиации. М.: Академкнига, 2003</mixed-citation><mixed-citation xml:lang="en">Kryzhanovsky G.A. The concept and CNS/ATM systems in civil aviation. M.: ICC Scientific journal, 2003. 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