• DocumentCode
    2179071
  • Title

    New approach to coarse alignment

  • Author

    Schimelevich, Leonid ; Naor, R.

  • Author_Institution
    Israel Aircraft Ind. Ltd., Israel
  • fYear
    1996
  • fDate
    22-26 Apr 1996
  • Firstpage
    324
  • Lastpage
    327
  • Abstract
    Two different methods for coarse alignment are discussed. One of them (direct method) utilizes both accelerometers and gyros output for continuously tracking attitude estimation while the other (gyrocompassing) utilizes gyro outputs for continuously tracking attitude system and accelerometers for attitude estimation. The standard approach is gyrocompassing in spite of the fact that it is not always the most accurate. The rule for selecting an appropriate algorithm is obtained. Our approach is based on DCM instead of Euler angles estimation, a fact which allows us to solve the nonlinear problem
  • Keywords
    accelerometers; aircraft navigation; attitude control; gyroscopes; inertial navigation; matrix algebra; tracking; accelerometers; attitude control; attitude estimation; coarse alignment; direct method; gyrocompassing; gyros output; matrix algebra; tracking; Acceleration; Accelerometers; Aerospace industry; Aircraft; Azimuth; Earth; Gravity; Instruments; Least squares approximation; Sensor phenomena and characterization;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Position Location and Navigation Symposium, 1996., IEEE 1996
  • Conference_Location
    Atlanta, GA
  • Print_ISBN
    0-7803-3085-4
  • Type

    conf

  • DOI
    10.1109/PLANS.1996.509095
  • Filename
    509095