• DocumentCode
    1027430
  • Title

    An Improved Azimuth Indicating System for Aircraft

  • Author

    Lynch, E.E. ; Pfuntner, R.A.

  • Author_Institution
    General Electric Company, Lynn, Mass.
  • Volume
    65
  • Issue
    12
  • fYear
    1946
  • Firstpage
    806
  • Lastpage
    812
  • Abstract
    Because of the violent maneuvering possibilities in modern aircraft, the usefulness of azimuth indicators in avigation marine navigational applications. New problems in direction indicating instruments therefore have been introduced, such as the perplexing problem of obtaining indication after loops or rolls. Azimuth indicating systems now used in aircraft have indicating a completely satisfactory solution to such problems. This paper summarizes the progress from the direct reading compasses to monitored gyroscopes and concentrates on the unique problems in aircraft where space limitations, reliability, and operation at all altitudes are important. It indicates how azimuth indicators and auto pilot controls close to the ideal are obtainable by the use of special features including a novel ``nontumbling´´ mechanism and an electromagnetic type of gimbal adjusting device.
  • Keywords
    Acceleration; Aircraft navigation; Control systems; Gravity; Gyroscopes; Instruments; Turning; Voltage;
  • fLanguage
    English
  • Journal_Title
    American Institute of Electrical Engineers, Transactions of the
  • Publisher
    ieee
  • ISSN
    0096-3860
  • Type

    jour

  • DOI
    10.1109/T-AIEE.1946.5059252
  • Filename
    5059252