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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-137</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>Определение диапазона изменения выходных параметров подсистемы управления</article-title><trans-title-group xml:lang="en"><trans-title>DETERMINE THE RANGE OF VARIATION OF THE CONTROL SUBSYSTEM OUTPUT PARAMETERS</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>Бобрин</surname><given-names>М. А.</given-names></name><name name-style="western" xml:lang="en"><surname>Bobrin</surname><given-names>M. A.</given-names></name></name-alternatives><email xlink:type="simple">noemail@neicon.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>2015</year></pub-date><pub-date pub-type="epub"><day>07</day><month>11</month><year>2016</year></pub-date><issue>212</issue><fpage>133</fpage><lpage>136</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Бобрин М.А., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Бобрин М.А.</copyright-holder><copyright-holder xml:lang="en">Bobrin M.A.</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/137">https://avia.mstuca.ru/jour/article/view/137</self-uri><abstract><p>Для оценки эксплуатационного поля допуска выходных параметров функциональной подсистемы управления гидравлической системы при различных условиях работы и этапах полета приведены математические зависимости и представлены результаты, полученные в среде Mathcad в графической форме.</p></abstract><trans-abstract xml:lang="en"><p>For the evaluation of the tolerance of output parameters of the controls functional subsystem the hydraulic system under different operating conditions and phases of flight are given mathematical relationships and the results obtained in Mathcad are given in graphical form.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>гидравлическая система летательных аппаратов</kwd><kwd>контроль</kwd><kwd>система управления</kwd><kwd>диапазон изменения выходных параметров</kwd></kwd-group><kwd-group xml:lang="en"><kwd>hydraulic system of aircraft</kwd><kwd>control</kwd><kwd>control system</kwd><kwd>the range of output parameters</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">Гониодский В.И., Склянский Ф.И., Шумилов И.С. Привод рулевых поверхностей самолетов. М.: Машиностроение, 1974. 320 с.</mixed-citation><mixed-citation xml:lang="en">Goniodskiyj V.I., Sklyanskiyj F.I., Shumilov I.S. Privod rulevihkh poverkhnosteyj samoletov. M.: Mashinostroenie. 1974. 320 p. (In Russian).</mixed-citation></citation-alternatives></ref><ref id="cit2"><label>2</label><citation-alternatives><mixed-citation xml:lang="ru">Матвиенко А.М., Зверев И.И. Проектирование гидравлических систем летательных аппаратов. М.: Машиностроение, 1982. 296 с.</mixed-citation><mixed-citation xml:lang="en">Matvienko A.M., Zverev I.I. Proektirovanie gidravlicheskikh sistem letateljnihkh apparatov. M.: Mashinostroenie. 1982. 296 p. (In Russian).</mixed-citation></citation-alternatives></ref><ref id="cit3"><label>3</label><citation-alternatives><mixed-citation xml:lang="ru">Бобрин М.А., Клемина Л.Г., Козлов А.Н. Определение эксплуатационного диапазона изменения выходных параметров функциональных подсистем гидравлических систем летательных аппаратов // Научный Вестник МГТУ ГА. 2011. № 200. С. 16-19.</mixed-citation><mixed-citation xml:lang="en">Bobrin M.A., Klemina L.G., Kozlov A.N. Opredelenie jekspluatacionnogo diapazona izmenenija vyhodnyh parametrov funkcional'nyh podsistem gidravlicheskih sistem letatel'nyh apparatov. Nauchnihyj Vestnik MGTU GA. 2011. № 200. Pp. 16-19. (In Russian).</mixed-citation></citation-alternatives></ref></ref-list><fn-group><fn fn-type="conflict"><p>The authors declare that there are no conflicts of interest present.</p></fn></fn-group></back></article>
