1 Ocak 2018 Konferans bildirisi Açık Erişim

Arberkli, Ferhat; Akbulut, Burak; Azgin, Kwanc; Tekinalp, Ozan

DataCite XML

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  <identifier identifierType="URL">https://aperta.ulakbim.gov.tr/record/32427</identifier>
  <creators>
    <creator>
      <creatorName>Arberkli, Ferhat</creatorName>
      <givenName>Ferhat</givenName>
      <familyName>Arberkli</familyName>
      <affiliation>Middle Tech Univ, Dept Mech Engn, TR-06800 Ankara, Turkey</affiliation>
    </creator>
    <creator>
      <creatorName>Akbulut, Burak</creatorName>
      <givenName>Burak</givenName>
      <familyName>Akbulut</familyName>
      <affiliation>Middle Tech Univ, Dept Aerosp Engn, TR-06800 Ankara, Turkey</affiliation>
    </creator>
    <creator>
      <creatorName>Azgin, Kwanc</creatorName>
      <givenName>Kwanc</givenName>
      <familyName>Azgin</familyName>
      <affiliation>Middle Tech Univ, Dept Mech Engn, TR-06800 Ankara, Turkey</affiliation>
    </creator>
    <creator>
      <creatorName>Tekinalp, Ozan</creatorName>
      <givenName>Ozan</givenName>
      <familyName>Tekinalp</familyName>
      <affiliation>Middle Tech Univ, Dept Aerosp Engn, TR-06800 Ankara, Turkey</affiliation>
    </creator>
  </creators>
  <titles>
    <title>Effects Of Rotor Geomery On The Performance Of Vibrating Mass Control Moment Gyrposcopes</title>
  </titles>
  <publisher>Aperta</publisher>
  <publicationYear>2018</publicationYear>
  <dates>
    <date dateType="Issued">2018-01-01</date>
  </dates>
  <resourceType resourceTypeGeneral="Text">Conference paper</resourceType>
  <alternateIdentifiers>
    <alternateIdentifier alternateIdentifierType="url">https://aperta.ulakbim.gov.tr/record/32427</alternateIdentifier>
  </alternateIdentifiers>
  <relatedIdentifiers>
    <relatedIdentifier relatedIdentifierType="DOI" relationType="IsVersionOf">10.81043/aperta.32426</relatedIdentifier>
    <relatedIdentifier relatedIdentifierType="DOI" relationType="IsIdenticalTo">10.81043/aperta.32427</relatedIdentifier>
  </relatedIdentifiers>
  <rightsList>
    <rights rightsURI="http://www.opendefinition.org/licenses/cc-by">Creative Commons Attribution</rights>
    <rights rightsURI="info:eu-repo/semantics/openAccess">Open Access</rights>
  </rightsList>
  <descriptions>
    <description descriptionType="Abstract">Elimination of unwanted oscillations on the satellite body that may be caused by the vibrating rotor control moment gyroscopes is addressed. It is mathematically shown that proper rotor inertia selection removes the unwanted oscillations on the output axis of the control moment gyroscope. Simulation results carried out using the ADAMS mechanical modeling and simulation software are given and discussed.</description>
  </descriptions>
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