• DocumentCode
    2837195
  • Title

    Notice of Retraction
    The Kinematics and Dynamics Design of Certain Follow-Up System

  • Author

    Zhiyong Qu ; Zhengmao Ye

  • Author_Institution
    Sch. of Mechatron. Eng., Harbin Inst. of Technol., Harbin, China
  • fYear
    2011
  • fDate
    17-18 July 2011
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    Notice of Retraction

    After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.

    We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.

    The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.

    Certain three freedom motion system for aerofoil fatigue experiment is presented. Multi-body theory is introduced to deduce the kinematics, where involve the stroke of cylinder and the aerofoil distortion. Dynamics is then done to calculate the force of cylinder for giving the correct element choice. These things can help designer to find effective structure and applied stylebook in the later studies.
  • Keywords
    aerodynamics; aerospace components; aerospace control; control system synthesis; fatigue; aerofoil fatigue experiment; cylinder stroke; follow-up system; multibody theory; three freedom motion system; Aerodynamics; Control systems; Fatigue; Force; Kinematics; Military aircraft;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Circuits, Communications and System (PACCS), 2011 Third Pacific-Asia Conference on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4577-0855-8
  • Type

    conf

  • DOI
    10.1109/PACCS.2011.5990201
  • Filename
    5990201