Title :
Tightly coupled IFOG-based GGP implementation and field test results
Author :
Dahlen, Neal J. ; Caylor, Thomas L. ; Goldner, Eric L.
Author_Institution :
Litton Guidance & Control Syst., Woodland Hills, CA, USA
Abstract :
Four (4) meters SEP (spherical error probable) in an integrated GPS/inertial mode and 10 meters error growth after 5 minutes without GPS reception were achieved with an interferometric fibre optic gyro (IFOG)-based GPS guidance package (GGP) under harsh field conditions. The 295 cubic inch, 14 pound Phase 1 GGP systems were evaluated under controlled laboratory conditions and during van testing, as well as in a US Army Fire Support Team Vehicle (FISTV). During the FISTV Demonstration, the GGP significantly outperformed the Army´s currently used equipment. The results of these tests validated the tightly coupled GPS/inertial design approach with fiber optic sensors, and the system´s suitability for applications with demanding environmental requirements. Current development is focused on 0.8 nmi/hr inertial performance and miniaturization of the system to a 100 cubic inch, 7 pound package. The Phase 2 design provides capabilities of high dynamics and low jamming susceptibility, as well as adaptability to multiple military and commercial applications with a low cost production system
Keywords :
Global Positioning System; fibre optic sensors; gyroscopes; inertial navigation; light interferometers; military communication; military equipment; position control; testing; GPS guidance package; US Army Fire Support Team Vehicle; fiber optic sensors; field test; integrated GPS/inertial mode; interferometric fibre optic gyro; jamming susceptibility; miniaturization; Control systems; Fiber optics; Fires; Global Positioning System; Laboratories; Navigation; Optical interferometry; Packaging machines; System testing; Vehicles;
Conference_Titel :
Position Location and Navigation Symposium, 1996., IEEE 1996
Conference_Location :
Atlanta, GA
Print_ISBN :
0-7803-3085-4
DOI :
10.1109/PLANS.1996.509080