High Precision Photonic Crystal Fiber Optic Gyroscope for Space Application

2017 Asia Communications and Photonics Conference (ACP) Pub Date : 2017-11-10 DOI:10.1364/ACPC.2017.SU1A.3

Xiaobin Xu, Ningfang Song, Zhihao Zhang, Wei Cai, Fuyu Gao

引用次数: 7

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.

查看原文本刊更多论文

空间应用的高精度光子晶体光纤陀螺仪

设计并制造了低损耗(~ 1.7dB/km)的PM-PCF，并在此基础上开发了偏置稳定性为~ 0.002°/h的PCFOG。PCFOG在“天舟-1”货运飞船上进行飞行试验。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

求助全文

约1分钟内获得全文求助全文

来源期刊

2017 Asia Communications and Photonics Conference (ACP)

自引率

0.00%

发文量