NASA NTRS · 19910034955
Fiber optic gyroscope using an eight-component LiNbO3 integrated optic circuit
Abstract
A LiNbO3 integrated optic circuit (IOC) containing eight optical functions has been successfully incorporated into an interferometric fiber optic gyroscope. The IOC has the minimum configuration optical functions (a phase modulator, a polarizer, and two beam splitters) and Jet Propulsion Laboratory's novel beat detection circuit (a phase modulator, two optical taps, and a beam splitter) which provides a means of directly reading angular position and rotation rate. The optical subsystem consisting of the fiber-pigtailed IOC and a sensing coil of 945 meters of polarization-maintaining fiber has a loss of 18.7dB, which includes 9dB due to the architecture and unpolarized source. A random walk coefficient was measured using an edge-emitting LED as the source.
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Minford, W. J., Stone, F. T., Youmans, B. R., Bartman, R. K.. 1990-01-01. Fiber optic gyroscope using an eight-component LiNbO3 integrated optic circuit. https://ntrs.nasa.gov/citations/19910034955
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