• DocumentCode
    582370
  • Title

    On stability augmentation for camera optical axis based on attitude of air ship

  • Author

    Wei, Hu ; Hongmei, Zhang ; Gui, Liu

  • Author_Institution
    Dept. of Aerosp. Eng., Shenyang Aerosp. Univ., Shenyang, China
  • fYear
    2012
  • fDate
    25-27 July 2012
  • Firstpage
    4750
  • Lastpage
    4753
  • Abstract
    This paper introduces a technology of stability argumentation for camera optical axis based on attitude of air ship. The attitude relative to the inertial coordinate system could be obtained by compass on air ship, then calculates the deflection angle between the camera optical axis and the origin target field, at last, offsets the change of camera optical axis cased by the movement of air ship by adjusting the rotating platform on air ship in both yaw and pitch directions. The test on air ship shows that the method mentioned in this paper is simple and practical, and the method could effectively resolve the problem which the attitude change of air ship could influence the camera optical axis on ship by adjusting the platform on air ship. The method could make the camera optical axis exactly find back the original target field and could keep the camera optical axis stabilizing.
  • Keywords
    autonomous aerial vehicles; cameras; robot vision; stability; video signal processing; UAV systems; air ship attitude; camera optical axis; compass; deflection angle calculation; inertial coordinate system; pitch directions; rotating platform; stability augmentation; yaw directions; Attitude control; Cameras; Compass; Laser stability; Marine vehicles; Power system stability; Stability analysis; Air ship; Attitude; Camera optical axis; Stability augmentation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2012 31st Chinese
  • Conference_Location
    Hefei
  • ISSN
    1934-1768
  • Print_ISBN
    978-1-4673-2581-3
  • Type

    conf

  • Filename
    6390762