• DocumentCode
    1146293
  • Title

    Minitact gyroscope-the low cost alternative

  • Author

    Califano, Herbert T.

  • Author_Institution
    AlliedSignal Guidance & Control System, Teterboro, NJ, USA
  • Volume
    9
  • Issue
    8
  • fYear
    1994
  • Firstpage
    12
  • Lastpage
    16
  • Abstract
    The allure of the solid state optical gyros is being challenged by the invention of a new spinning mass device, providing superior low noise drift performance, high reliability at a very low cost. The Minitact is a unique two axis gyroscope advancing the technology of spinning mass devices to set new low cost standards. Minitact provides all the low noise performance benefits of tuned rotor gyroscopes without the vagaries of fixture suspension systems. The Minitact design integrates together the advantages of a spherical hydrodynamic gas bearing and a three axis permanent magnet DC commutated, motor and torquer, into miniature two aids gyroscope with a dynamic range of greater than 10/sup -7/. The design is described and performance data presented illustrating the capability of this low cost next generation rate gyroscope. The Minitact is the result of Integrated Product Development (IPD) and Design to Unit Production Cost (DTUPC) design processes and is expected to become the tactical performance benchmark.<>
  • Keywords
    gyroscopes; military equipment; navigation; permanent magnet motors; Design to Unit Production Cost; Integrated Product Development; Minitact gyroscope; cost; design; mechanical gyro; military equipment; navigation; noise drift performance; permanent magnet DC motor; reliability; spherical hydrodynamic gas bearing; spinning mass device; spinning mass devices; standards; tactical performance benchmark; tuned rotor gyroscopes; two axis gyroscope; Costs; Fixtures; Gyroscopes; Hydrodynamics; Magnetic levitation; Optical devices; Optical noise; Rotors; Solid state circuits; Spinning;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/62.311238
  • Filename
    311238