• DocumentCode
    3384572
  • Title

    The next frontier for strapdown RLG inertial systems. Precision navigation

  • Author

    Upton, Robert W., Jr. ; Miller, William G.

  • Author_Institution
    Honeywell Mil. Avionics Div., Clearwater, FL, USA
  • fYear
    1990
  • fDate
    20-23 Mar 1990
  • Firstpage
    537
  • Lastpage
    542
  • Abstract
    Honeywell research and development projects directed at improvements in the design, building, and testing of RLG (ring laser gyro) strapdown systems are reviewed. Some of the performance standards being set with current hardware are discussed, as are a number of the known error sources existing in these systems along with candidate solutions, the analysis and test results upon which precision navigation performance projections are based, and plans to demonstrate the feasibility of a precision pure strapdown RLG system. Based upon current performance, reasonable projections and analysis, and laboratory test data, it is anticipated that strapdown RLG systems can deliver performance consistent with the precision requirements of SNU 84-3 (0.2 nm/h after a precision-extended time-alignment) while retaining the major advantages that the pure strapdown mechanization offers
  • Keywords
    gyroscopes; inertial navigation; laser beam applications; nonelectric sensing devices; ring lasers; Honeywell; SNU 84-3; accelerometers; error sources; inertial sensors; military systems; strapdown RLG inertial systems; Aerospace electronics; Aerospace engineering; Aircraft navigation; Application software; Design engineering; Inertial navigation; Military aircraft; Military standards; Performance analysis; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Position Location and Navigation Symposium, 1990. Record. The 1990's - A Decade of Excellence in the Navigation Sciences. IEEE PLANS '90., IEEE
  • Conference_Location
    Las Vegas, NV
  • Type

    conf

  • DOI
    10.1109/PLANS.1990.66225
  • Filename
    66225