• DocumentCode
    768963
  • Title

    An Automatic Gyro Mass-Unbalance Measuring Technique

  • Author

    Walker, F.L.

  • Author_Institution
    Inertial Navigation, Autonetics Division, North American Aviation, Inc., Downey, Calif.
  • Issue
    1
  • fYear
    1963
  • Firstpage
    36
  • Lastpage
    40
  • Abstract
    An inertial navigation system containing a versatile computer can be given the capability of automatically measuring its gyro mass unbalance. These measurements are accomplished in tests performed and monitored by the computer. Mass-unbalanced drifts induced by tilting the stable platform are detected by the system´s acceleration sensors. From the outputs of these sensors, the computer determines the mass-unbalance components using regression-analysis techniques that minimize errors of extraneous origin.
  • Keywords
    Acceleration; Computerized monitoring; Control systems; Equations; Inertial navigation; Military computing; Performance evaluation; Sensor systems; Test equipment; Testing;
  • fLanguage
    English
  • Journal_Title
    Military Electronics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0536-1559
  • Type

    jour

  • DOI
    10.1109/TME.1963.4323039
  • Filename
    4323039