• DocumentCode
    3386720
  • Title

    Ring laser gyro applications for tactical missiles: the Army TACMS solution

  • Author

    Curran, George L. ; Engelken, Daniel J.

  • Author_Institution
    Honeywell Mil. Avionics Div., Clearwater, FL, USA
  • fYear
    1990
  • fDate
    20-23 Mar 1990
  • Firstpage
    543
  • Lastpage
    548
  • Abstract
    The Honeywell H700-3A ring laser gyro missile guidance set (AN/DJW-51) provides navigation, guidance, autopilot, weapons dispensing, and communications functions for the US Army TACMS missile in a low-initial-cost and low-life-cycle-cost package. It is primarily the use of low-cost inertial sensors which make the use of a ring laser gyro navigation system feasible in the tactical missile market. The H700-3A ring laser gyro missile guidance set has proven to be a low-cost, high-accuracy guidance and navigation system for the deep-strike Army missile weapons system. This has been borne out by a highly successful test program of 26 missile flights. The components of the missile guidance set are described in detail
  • Keywords
    aerospace computer control; gyroscopes; inertial navigation; laser beam applications; missiles; ring lasers; AN/DJW-51; Army TACMS solution; Honeywell H700-3A ring laser gyro missile guidance set; autopilot; communications functions; guidance; navigation; tactical missiles; weapons dispensing; Accelerometers; Assembly; Laser applications; Mirrors; Missiles; Power supplies; Ring lasers; Temperature distribution; Temperature sensors; Voltage;
  • 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.1990.66226
  • Filename
    66226