DocumentCode
1112136
Title
Pointing grade fiber optic gyroscope
Author
Killian, Kevin M.
Author_Institution
AlliedSignal Guidance & Control Syst., Teterboro, NJ, USA
Volume
9
Issue
7
fYear
1994
fDate
7/1/1994 12:00:00 AM
Firstpage
6
Lastpage
10
Abstract
Fiber optic gyroscopes (FOG) are solid-state rotation sensors that are appropriate for a wide variety of applications. In addition to becoming competitive with ring laser gyroscopes on new programs, FOGs are being manufactured to replace spinning wheel gyro technology in existing programs. The FOG brings with it the advantages of long life, high reliability, input axis stability, and low acceleration sensitivity. The AlliedSignal pointing grade fiber gyroscope was designed to replace a high-performance mechanical gyroscope currently made by AlliedSignal. Detailed passive thermal design, gyro assembly techniques, methods for rejecting light source intensity noise, and light source wavelength control are critical features that have been developed to produce a FOG with low noise, stable bias, and a stable and linear scale factor. Results of performance tests and error models indicate that these gyros have a capability for random walk of 0.0002 degrees//spl ne/ hour and bias stability of 0.001 degrees/hour.<>
Keywords
aerospace instrumentation; attitude control; fibre optic sensors; gyroscopes; AlliedSignal; assembly; directional coupler; error models; light source intensity noise; light source wavelength control; low acceleration sensitivity; passive thermal design; performance tests; pointing grade fiber optic gyroscope; random walk; signal processing; solid-state rotation sensors; spacecraft attitude control; spinning wheel gyro technology; stability; Fiber lasers; Gyroscopes; Light sources; Manufacturing; Optical fiber sensors; Optical fibers; Optical sensors; Ring lasers; Solid state circuits; Stability;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems Magazine, IEEE
Publisher
ieee
ISSN
0885-8985
Type
jour
DOI
10.1109/62.295115
Filename
295115
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