• DocumentCode
    1145108
  • Title

    Development of a Low-Power Digital Inertial Reference Assembly

  • Author

    Bicking, R.E.

  • Author_Institution
    Honeywell Inc., Minneapolis, Minn.
  • Issue
    3
  • fYear
    1971
  • fDate
    5/1/1971 12:00:00 AM
  • Firstpage
    544
  • Lastpage
    549
  • Abstract
    Current and projected system requirements for inertial reference assemblies emphasize high accuracy, long life, and low power. An inertial reference assembly ( IRA) which embodies the aforementioned characteristics was developed recently. Pulse rebalanced gas-bearing gyroscopes were used to attain high accuracy and long life. Temperature compensation of gyroscope parameters (in lieu of temperature control) and dual voltage spinmotor operation helped achieve low-power operation. The latter two items represent an advancement in the state of the art and form the subject of this paper. These techniques were used in the construction of a three-axis IRA with an operating power less than 50 watts. It has achieved 0.1 percent scale factor accuracy over a 60°F range.
  • Keywords
    Assembly; Costs; Damping; Equations; Gyroscopes; Space vehicles; Temperature control; Temperature distribution; Temperature sensors; Thermal resistance;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1971.310297
  • Filename
    4103745