• DocumentCode
    1945371
  • Title

    Flight test results of the Rockwell MIGITS

  • Author

    Shale, Richard ; Bader, John

  • Author_Institution
    Collins Avionics & Commun. Div., Rockwell Int., Anaheim, CA, USA
  • fYear
    1994
  • fDate
    11-15 Apr 1994
  • Firstpage
    306
  • Lastpage
    309
  • Abstract
    A new standard of lightweight, low cost, integrated GPS/INS products has been created with the introduction of Rockwell´s family of MIGITS (Miniature integrated GPS/INS Tactical System) products. This family takes full advantage of the precision pseudorange and pseudorange rate information available only from an embedded GPS receiver. This information is integrated with inertial data in a single Kalman filter in a synergistic manner which results in superior operation in high dynamic, antenna shading, and jamming environments. The Rockwell MIGITS has successfully demonstrated ability to tightly couple a tactical grade IMU with GPS to provide precise navigation operation in a dynamic environment. The integrated systems described in this paper build upon the lessons learned and the continued evolution of GPS. Continual refinements in research and development programs at Rockwell have led to this family of small integrated systems, resulting in what is believed to be the world´s smallest, integrated GPS/INS systems available today, the MIGITS. The MIGITS products are intended to satisfy the navigation requirements of a variety of applications including missiles, both fixed and rotary wing aircraft, UAV´s, munitions, targets and drones. This paper provides an introduction to the various MIGITS systems, followed by a description of the system testing performed thus far
  • Keywords
    aerospace testing; inertial navigation; radionavigation; satellite relay systems; GPS receiver; Kalman filter; Miniature integrated GPS/INS Tactical System; Rockwell MIGITS; UAV; aircraft; antenna shading; drones; dynamic environment; flight test results; inertial data; integrated GPS/INS products; integrated systems; jamming environments; missiles; munitions; precision pseudorange information; pseudorange rate information; system testing; targets; Aerospace electronics; Aircraft navigation; Communication standards; Costs; Global Positioning System; Jamming; Military equipment; Missiles; Research and development; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Position Location and Navigation Symposium, 1994., IEEE
  • Conference_Location
    Las Vegas, NV
  • Print_ISBN
    0-7803-1435-2
  • Type

    conf

  • DOI
    10.1109/PLANS.1994.303328
  • Filename
    303328