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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">novtexmech</journal-id><journal-title-group><journal-title xml:lang="ru">Мехатроника, автоматизация, управление</journal-title><trans-title-group xml:lang="en"><trans-title>Mekhatronika, Avtomatizatsiya, Upravlenie</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">1684-6427</issn><issn pub-type="epub">2619-1253</issn><publisher><publisher-name>Commercial Publisher «New Technologies»</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.17587/mau.18.637-641</article-id><article-id custom-type="elpub" pub-id-type="custom">novtexmech-481</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>УПРАВЛЕНИЕ ТЕХНИЧЕСКИМИ ОБЪЕКТАМИ И ТЕХНОЛОГИЧЕСКИМИ ПРОЦЕССАМИ</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="en"><subject>CONTROL IN AEROSPACE SYSTEMS</subject></subj-group></article-categories><title-group><article-title>Стохастическое управление внешней подвеской пожарного вертолета</article-title><trans-title-group xml:lang="en"><trans-title>Stochastic Control of the External Sling of a Fire Helicopter</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>Рачков</surname><given-names>М. Ю.</given-names></name><name name-style="western" xml:lang="en"><surname>Rachkov</surname><given-names>M. Yu.</given-names></name></name-alternatives><email xlink:type="simple">noemail@neicon.ru</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru"><institution>Московский политехнический университет</institution><country>Россия</country></aff><aff xml:lang="en"><institution>Moscow Polytechnic University</institution><country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2017</year></pub-date><pub-date pub-type="epub"><day>28</day><month>08</month><year>2018</year></pub-date><volume>18</volume><issue>9</issue><fpage>637</fpage><lpage>641</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Commercial Publisher «New Technologies», 2018</copyright-statement><copyright-year>2018</copyright-year><copyright-holder xml:lang="ru">Commercial Publisher «New Technologies»</copyright-holder><copyright-holder xml:lang="en">Commercial Publisher «New Technologies»</copyright-holder><license xlink:href="https://mech.novtex.ru/jour/about/submissions#copyrightNotice" xlink:type="simple"><license-p>https://mech.novtex.ru/jour/about/submissions#copyrightNotice</license-p></license></permissions><self-uri xlink:href="https://mech.novtex.ru/jour/article/view/481">https://mech.novtex.ru/jour/article/view/481</self-uri><abstract><p>Описывается моделирование движения вертолета с водосливным устройством на внешней подвеске для тушения пожаров. Синтезирована система оптимального стохастического управления с минимизацией колебаний подвески и энергии для его реализации. Проведен анализ влияния изменений параметров системы на управляющий сигнал в зависимости от длины подвески и интенсивности стохастических возмущений с помощью компьютерного моделирования.</p></abstract><trans-abstract xml:lang="en"><p>The paper describes the motion modeling of a fire helicopter with an external sling and a spillway device. The mathematical model of the fire helicopter with an external sling takes into account the effect of the stochastic disturbances for the sling caused by the rotor vibrations, gusts of wind and convection flows in the fire zone. The stochastic optimal control is synthesized with minimal sling oscillations and control power for its implementation. The solution is obtained due to dynamic programming. The resulting optimal control does not depend on the mass of a spillway device, but it is a function of a sling length. Thus, because of the changing sling length during motion, the length should be measured together with the sling deviation angle and the intensity of the stochastic disturbances. The temporal evolution of the system solution is done for various disturbance intensities. The computer calculation results are presented as a function of the suspension length and the intensity of the stochastic disturbances. Analysis of the results shows that the sling length affects significantly the value of the control signal, especially at high levels of the disturbances. A structure of the helicopter stochastic control system is proposed. It makes it possible to control oscillation of the external sling within an acceptable range. The system includes an oscillation angle, a sensor of the stochastic disturbance intensity and the sling length sensor. Thus, the helicopter control can be obtained through changing the thrust magnitude of the main and tail helicopter rotors.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>компьютерное моделирование</kwd><kwd>оптимальное управление</kwd><kwd>стохастические возмущения</kwd><kwd>пожарный вертолет</kwd><kwd>computer modeling</kwd><kwd>optimal control</kwd><kwd>stochastic disturbance</kwd><kwd>fire helicopter</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">Kutay A. Т., Calise A. J., Idan M., Hovakimyan N. Experimental Results on Adaptive Output Feedback Control Using a Laboratory Model Helicopter // IEEE Trans. on control systems technology. 2005. Vol. 13, N. 11. P. 196-202.</mixed-citation><mixed-citation xml:lang="en">Kutay A. Т., Calise A. J., Idan M., Hovakimyan N. 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