Cavity element for Resonant Micro Optical Gyroscope

Carol Ford; Randy Ramberg; Klein Johnson; William Berglund; Benjamin Ellerbusch; Ross Schermer; Anand Gopinath

doi:10.1109/62.891978

Cavity element for Resonant Micro Optical Gyroscope

Carol Ford, Randy Ramberg, Klein Johnson, William Berglund, Benjamin Ellerbusch, Ross Schermer, Anand Gopinath

Electrical and Computer Engineering

Research output: Contribution to journal › Article › peer-review

24 Scopus citations

Abstract

The results of the work conducted in the field of inertial-based altitude and navigation control systems were reported. A Resonant Micro Optic Gyro (RMOG) was predicted to achieve one degree/hour performance. A high quality waveguide was developed and had small loss of 0.1 dB/cm and gain in the range of 4.0 dB/cm. A waveguide laser powerful enough to drive an RMOG was fabricated.

Original language	English (US)
Pages (from-to)	33-36
Number of pages	4
Journal	IEEE Aerospace and Electronic Systems Magazine
Volume	15
Issue number	12
DOIs	https://doi.org/10.1109/62.891978
State	Published - Dec 2000

Bibliographical note

Funding Information:
' Work sponsored by DARPA Ultra Photonic contract.

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10.1109/62.891978

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abstract = "The results of the work conducted in the field of inertial-based altitude and navigation control systems were reported. A Resonant Micro Optic Gyro (RMOG) was predicted to achieve one degree/hour performance. A high quality waveguide was developed and had small loss of 0.1 dB/cm and gain in the range of 4.0 dB/cm. A waveguide laser powerful enough to drive an RMOG was fabricated.",

author = "Carol Ford and Randy Ramberg and Klein Johnson and William Berglund and Benjamin Ellerbusch and Ross Schermer and Anand Gopinath",

note = "Funding Information: ' Work sponsored by DARPA Ultra Photonic contract.",

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AU - Ford, Carol

AU - Ramberg, Randy

AU - Johnson, Klein

AU - Berglund, William

AU - Ellerbusch, Benjamin

AU - Schermer, Ross

AU - Gopinath, Anand

N1 - Funding Information: ' Work sponsored by DARPA Ultra Photonic contract.

PY - 2000/12

Y1 - 2000/12

N2 - The results of the work conducted in the field of inertial-based altitude and navigation control systems were reported. A Resonant Micro Optic Gyro (RMOG) was predicted to achieve one degree/hour performance. A high quality waveguide was developed and had small loss of 0.1 dB/cm and gain in the range of 4.0 dB/cm. A waveguide laser powerful enough to drive an RMOG was fabricated.

AB - The results of the work conducted in the field of inertial-based altitude and navigation control systems were reported. A Resonant Micro Optic Gyro (RMOG) was predicted to achieve one degree/hour performance. A high quality waveguide was developed and had small loss of 0.1 dB/cm and gain in the range of 4.0 dB/cm. A waveguide laser powerful enough to drive an RMOG was fabricated.

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ER -

Cavity element for Resonant Micro Optical Gyroscope

Abstract

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