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High Precision Photonic Crystal Fiber Optic Gyroscope for Space Application

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Abstract

A low-loss (~1.7dB/km) PM-PCF has been designed and fabricated, based on which a PCFOG having a bias stability of ~0.002°/h is developed. The PCFOG has a flight test in “Tianzhou-1” Cargo Spaceship.

© 2017 Optical Society of America

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