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
Link To Document :
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