• DocumentCode
    3436439
  • Title

    Notice of Retraction
    Failure modes and effect analysis on the gyroscope of the INS on the spaceflight tracking ship

  • Author

    Feng Zhang ; Fan Zhang ; Yibin Ren

  • Author_Institution
    Maritime Tracking & Control Dept., China Satellite, Jiangyin, China
  • fYear
    2013
  • fDate
    15-18 July 2013
  • Firstpage
    388
  • Lastpage
    390
  • 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.

    In this paper, firstly, the structure of gyroscope is described, and then reliability analysis and modeling of gyroscope is carried out. Specific to one of the gyroscope failures, the failure tree model is built and analyzed. Finally, the failure type is counted up and the corresponding reason is analyzed.
  • Keywords
    fault trees; gyroscopes; inertial navigation; space vehicles; FMEA; INS; failure mode and effect analysis; failure tree model; gyroscope failures; gyroscope modeling; gyroscope structure; reliability analysis; spaceflight tracking ship; Gyroscopes; Integrated circuit reliability; Marine vehicles; Reliability engineering; Sealing materials; Wires; failure tree; failure type; gyroscope; reliability;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2013 International Conference on
  • Conference_Location
    Chengdu
  • Print_ISBN
    978-1-4799-1014-4
  • Type

    conf

  • DOI
    10.1109/QR2MSE.2013.6625608
  • Filename
    6625608