DocumentCode
2185105
Title
Remote fiber optic gyroscopes for a broad range of applications
Author
Bowser, Mark ; Hammond, James ; Perlmutter, Michael ; Reynolds, Christopher
Author_Institution
Fibersense Technol. Corp., Norwood, MA, USA
fYear
1996
fDate
22-26 Apr 1996
Firstpage
553
Lastpage
558
Abstract
Fibersense Technology Corporation has completed the development of a new type of Fiber Optic Gyroscope (FOG) configuration in which the sensing element-the fiber coil-is separated from all other gyro elements. This configuration allows fiber coils to be located on the device of interest, without requiring any electrical connections to the rest of the gyro or system. A production version of this configuration, now being manufactured for a missile application, uses a sensing coil 1.3 inches in diameter and 0.3 inches thick. Without data compensation this FOG is capable of a dynamic range in excess of 10,000°/sec, an angle random walk of less than 0.03°/√h, and a bias stability over temperature and day-to-day of less than 2°/h. This FOG requires only ±5 volts to operate its low cost, all-digital signal processing electronics which produce a digital output proportional to rotation rate. Variations of this configuration, capable of 0.01°/h bias stability, have also been developed and demonstrated
Keywords
fibre optic sensors; gyroscopes; military avionics; missiles; optical information processing; remote sensing; signal processing equipment; 0.3 in; 1.3 in; 5 V; Fibersense Technology Corporation; angle random walk; bias stability; fiber coil; low-cost all-digital signal processing electronics; missile; remote fiber optic gyroscopes; Coils; Dynamic range; Gyroscopes; Manufacturing; Missiles; Optical fiber devices; Optical fibers; Production; Stability; Temperature distribution;
fLanguage
English
Publisher
ieee
Conference_Titel
Position Location and Navigation Symposium, 1996., IEEE 1996
Conference_Location
Atlanta, GA
Print_ISBN
0-7803-3085-4
Type
conf
DOI
10.1109/PLANS.1996.509127
Filename
509127
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