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<!DOCTYPE ArticleSet PUBLIC "-//NLM//DTD PubMed 2.0//EN" "http://www.ncbi.nlm.nih.gov:80/entrez/query/static/PubMed.dtd"[]>
<ArticleSet>
  <Article>
    <Journal>
      <PublisherName>Science and Education Publishing</PublisherName>
      <JournalTitle>Journal of Automation and Control</JournalTitle>
      <Volume>2</Volume>
      <Issue>3</Issue>
      <PubDate PubStatus="epublish">
        <Year>2014</Year>
        <Month>11</Month>
        <Day>13</Day>
      </PubDate>
    </Journal>
    <ArticleTitle>Model of Stabilization of Helicopter in Hover Mode over a Given Point Object under Destabilizing Action of Weather Conditions</ArticleTitle>
    <FirstPage>86</FirstPage>
    <LastPage>90</LastPage>
    <Language>EN</Language>
    <AuthorList>
      <Author>
        <FirstName>Vasiliy</FirstName>
        <LastName>Kazak</LastName>
      </Author>
      <Author>
        <FirstName>Dmitry</FirstName>
        <LastName>Shevchuk</LastName>
      </Author>
      <Author>
        <FirstName>Nataliia</FirstName>
        <LastName>Tymoshenko</LastName>
        <Affiliation>National Aviation University, Kiev, Ukraine</Affiliation>
      </Author>
    </AuthorList>
    <ArticleIdList>
      <ArticleId IdType="pii">AUTOMATION2014234</ArticleId>
      <ArticleId IdType="doi">10.12691/automation-2-3-4</ArticleId>
    </ArticleIdList>
    <History>
      <PubDate PubStatus="received">
        <Year>2014</Year>
        <Month>10</Month>
        <Day>23</Day>
      </PubDate>
      <PubDate PubStatus="revised">
        <Year>2014</Year>
        <Month>11</Month>
        <Day>10</Day>
      </PubDate>
      <PubDate PubStatus="accepted">
        <Year>2014</Year>
        <Month>11</Month>
        <Day>13</Day>
      </PubDate>
    </History>
    <Abstract>The design problem of the high precision stabilizer for hovering of the helicopter about the point object as a part of the automatic control system (ACS) is considered. Here we substantiate method and models for hover mode of helicopter as well as measurements of parameters of this flight mode that requires smaller volume of calculation and preserves high speed and accuracy of stabilization. Also we investigate reduction of number of state vectors and volume of calculation via usage of extended Kalman filter (EKF) and standard sensors.</Abstract>
  </Article>
</ArticleSet>