• DocumentCode
    979868
  • Title

    Inertial-Guidance Limitations Imposed by Fluctuation Phenomena in Gyroscopes

  • Author

    Newton, George C., Jr.

  • Author_Institution
    Electronic Systems Lab., Dept. of Elec. Engrg., Massachtusetts Inistitute of Technology, Cambridge, Mass.
  • Volume
    48
  • Issue
    4
  • fYear
    1960
  • fDate
    4/1/1960 12:00:00 AM
  • Firstpage
    520
  • Lastpage
    527
  • Abstract
    Because of recent improvements, inertial guidance is becoming increasingly important to space and missile programs in connection with the navigation of mobile bases and the launching of vehicles. Gyroscopes are an important component of inertial systems. In order to see if much room remains for further improvement, the performance limitation imposed by thermal fluctuations in gyroscopes is examined. This is done because experience in electronics shows that thermal noise is the ultimate performance limitation in sensitive instruments such as radio receivers and galvanometers. It is found that a system limited only by thermal noise in its gyroscopes would have several orders of magnitude more precision than that indicated in published performance data. This must mean that other factors are limiting performance of gyroscopes, and investigation of several of these shows that bearing noise may be an important one. In conclusion, since gyroscopes do not yet come near to attaining the performance limits set by thermal noise, there may be much room left for their further improvement.
  • Keywords
    Acceleration; Aircraft navigation; Earth; Fluctuations; Gravity; Gyroscopes; Missiles; Space technology; Space vehicles; Underwater vehicles;
  • fLanguage
    English
  • Journal_Title
    Proceedings of the IRE
  • Publisher
    ieee
  • ISSN
    0096-8390
  • Type

    jour

  • DOI
    10.1109/JRPROC.1960.287401
  • Filename
    4066050