• DocumentCode
    858156
  • Title

    Nongyroscopic inertial reference

  • Author

    Klein, J.J.

  • Author_Institution
    Lockheed Aircraft Corp., Sunnyvale, CA, USA
  • Volume
    4
  • Issue
    2
  • fYear
    1959
  • fDate
    11/1/1959 12:00:00 AM
  • Firstpage
    182
  • Lastpage
    191
  • Abstract
    The space stabilizing capability of a servo controlled nonrotating inertial mass is analyzed and its drift rate performance compared with a high precision gyroscope. The results indicate that the nongyroscopic inertial reference and guidance system exceeds the performance of gyroscopic systems by several orders of magnitude. It is shown that a servo system materially contributes to the drift accuracy in the nongyroscopic system but not in the gyroscopic system. The navigation errors of the discussed scheme are directly proportional to the accelerometer errors and, therefore, are inherently smaller than in an equivalent gyroscopic system.
  • Keywords
    Accelerometers; Containers; Glass; Gyroscopes; Missiles; Navigation; Servomechanisms; Torque control; Weight control; Wheels;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IRE Transactions on
  • Publisher
    ieee
  • ISSN
    0096-199X
  • Type

    jour

  • DOI
    10.1109/TAC.1959.1104858
  • Filename
    1104858