• DocumentCode
    1006134
  • Title

    The effect of gyro nonorthogonality error on gyrocompassing

  • Author

    Priel, B.

  • Author_Institution
    Israel Aircraft Ind., Yahud
  • Volume
    28
  • Issue
    3
  • fYear
    1992
  • fDate
    7/1/1992 12:00:00 AM
  • Firstpage
    890
  • Lastpage
    893
  • Abstract
    The effect of the gyro nonorthogonality on the two-step gyrocompassing process is analyzed. It is shown that the azimuth misalignment resulting from gyro nonorthogonality depends on the platform direction with respect to geographic frame. Gyrocompassing error is explicitly expressed in terms of gyro nonorthogonality and gyro parameters. A compensation scheme to eliminate the gyrocompassing error, which results from gyro nonorthogonality, is presented. This method can be used in cases where the gyro nonorthogonality error is beyond the standard requirements for high quality platforms. The main advantage is that it allows an increase in the tolerance of gyro nonorthogonality, and reduces the cost of inertial measurement unit manufacture
  • Keywords
    aircraft instrumentation; compensation; error correction; gyroscopes; inertial navigation; measurement errors; azimuth misalignment; compensation; gyro nonorthogonality error; gyrocompassing; inertial navigation; Accelerometers; Aircraft; Azimuth; Costs; Error correction; Manufacturing; Measurement standards; Measurement units; Navigation; Stability analysis;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.256312
  • Filename
    256312