DocumentCode :
1419317
Title :
Cavity element for resonant micro optical gyroscope
Author :
Ford, Carol ; Ramberg, Randy ; Johnson, Klein ; Bergulund, W. ; Ellerbusch, Benjamin ; Schermer, Ross ; Gopinath, Anand
Author_Institution :
Honeywell Inc., MN, USA
Volume :
15
Issue :
12
fYear :
2000
fDate :
12/1/2000 12:00:00 AM
Firstpage :
33
Lastpage :
36
Abstract :
Significant strides have been made towards a feasible resonant micro optic gyro (RMOG). Uniquely crucial components have been developed. Experimental measurements, when coupled with theoretical analysis predicts that 1 degree/hour performance can be achieved. Three critical elements required for the successful development have been demonstrated. A high quality trench waveguide has been designed, fabricated and demonstrated to have losses as little as 0.1 dB/cm. The waveguide has been demonstrated to have gain in the 4.0 dB/cm range. Finally, a waveguide laser has been fabricated and has shown nearly enough power to adequately drive an RMOG. Analysis of the measured performance predicts that a 1 degree/hour RMOG can be constructed. The small size and projected ruggedness of the RMOG will be advantageous in high G applications. Other applications, such as man portable guidance systems, where weight and size are critical, may also benefit from RMOG technology
Keywords :
gyroscopes; laser cavity resonators; micro-optics; optical planar waveguides; waveguide lasers; cavity element; control loops; high G applications; high quality trench waveguide; man portable guidance systems; planar waveguide; resonant micro optical gyroscope; ruggedness; small size; waveguide laser; Costs; Frequency; Gyroscopes; Laser beams; Optical interferometry; Optical pumping; Optical resonators; Optical ring resonators; Optical waveguides; Resonance;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0885-8985
Type :
jour
DOI :
10.1109/62.891978
Filename :
891978
Link To Document :
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