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<!DOCTYPE article PUBLIC "-//NLM//DTD JATS (Z39.96) Journal Publishing DTD v1.3 20210610//EN" "JATS-journalpublishing1-3.dtd">
<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">bsuir</journal-id><journal-title-group><journal-title xml:lang="ru">Доклады БГУИР</journal-title><trans-title-group xml:lang="en"><trans-title>Doklady BGUIR</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">1729-7648</issn><issn pub-type="epub">2708-0382</issn><publisher><publisher-name>БГУИР</publisher-name></publisher></journal-meta><article-meta><article-id custom-type="elpub" pub-id-type="custom">bsuir-323</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>АЛГОРИТМ МОДЕЛИРОВАНИЯ ТРАЕКТОРИИ ДВИЖЕНИЯ ВОЗДУШНОГО ОБЪЕКТА</article-title><trans-title-group xml:lang="en"><trans-title>ALGORITHM OF MODELING THE TRAJECTORY OF AN AERIAL OBJECT</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>Дятко</surname><given-names>А. А.</given-names></name><name name-style="western" xml:lang="en"><surname>Dyatko</surname><given-names>A. A.</given-names></name></name-alternatives><email xlink:type="simple">noemail@neicon.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Костромицкий</surname><given-names>С. М.</given-names></name><name name-style="western" xml:lang="en"><surname>Kostromitski</surname><given-names>S. M.</given-names></name></name-alternatives><email xlink:type="simple">noemail@neicon.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Шумский</surname><given-names>П. Н.</given-names></name><name name-style="western" xml:lang="en"><surname>Shumski</surname><given-names>P. N.</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>ОАО «КБ Радар» - управляющая компания холдинга «Системы радиолокации»</institution><country>Belarus</country></aff><pub-date pub-type="collection"><year>2014</year></pub-date><pub-date pub-type="epub"><day>03</day><month>06</month><year>2019</year></pub-date><volume>0</volume><issue>4</issue><fpage>41</fpage><lpage>47</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Дятко А.А., Костромицкий С.М., Шумский П.Н., 2019</copyright-statement><copyright-year>2019</copyright-year><copyright-holder xml:lang="ru">Дятко А.А., Костромицкий С.М., Шумский П.Н.</copyright-holder><copyright-holder xml:lang="en">Dyatko A.A., Kostromitski S.M., Shumski P.N.</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://doklady.bsuir.by/jour/article/view/323">https://doklady.bsuir.by/jour/article/view/323</self-uri><abstract><p>Приведен метод вычисления координат траектории полета летательного аппарата, заданной множеством своих опорных точек и значениями радиусов окружностей, по которым летательный аппарат должен выполнять вираж в случае изменения направления своего движения. Показано, что наиболее просто необходимые вычисления выполняются в специальной системе координат, положение которой в пространстве определяется тремя опорными точками траектории.</p></abstract><trans-abstract xml:lang="en"><p>The method of coordinates calculation of a flight trajectory of the aircraft, adjusted by the reference points and values of radiuses of circles on which the bend in case of change of a direction of the movement should carry out the aircraft is resulted. It is shown that it’s easier to carry out nessesary calculations in special system of the co-ordinates which position in space is defined by three reference points of a trajectory.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>траектория</kwd><kwd>вираж</kwd><kwd>система координат</kwd><kwd>аффинные преобразования</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">Остославский И.В. Динамика полета. М., 1969.</mixed-citation><mixed-citation xml:lang="en">Остославский И.В. Динамика полета. М., 1969.</mixed-citation></citation-alternatives></ref><ref id="cit2"><label>2</label><citation-alternatives><mixed-citation xml:lang="ru">Порев В.Н. Компьютерная графика. СПб, 2002.</mixed-citation><mixed-citation xml:lang="en">Порев В.Н. Компьютерная графика. СПб, 2002.</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>
