A Micro-Optical Transceiver for Interferometric Fiber Optic Gyroscope

2011 ◽  
Vol 483 ◽  
pp. 427-431
Author(s):  
Kun Bo Wang ◽  
Ying Jian Ma ◽  
Bo Zhang ◽  
Li Shuang Feng

The application of integrated optical components into a single module provides a method of increasing the level of integration with the real potential of reducing unit cost and raising the reliability. A new method was used to design a micro-optical transceiver module of an interferometric fiber optic gyroscope (IFOG) system. By using free-space optical coupling method, all optical parts except a phase modulator and the sensing coil were built in a single module to form the active configuration of the IFOG, including a SLD chip, a photoelectric detector, a beam splitter and a light source driving circuit. Very small optical elements were used in the micro-optical transceiver, and the driving circuit of the light source was optimized and integrated by using thick film integrated technology into the transceiver. Reducing the number of optical components makes size smaller and assembling-cost lower. A gyro test which was composed of the transceiver module connecting to a phase modulator and the polarization-mode (PM) fiber coil of 800 m in length was carried out. The bias stability of IFOG is about 0.63 degrees/hour. Experimental results show that this optical transceiver will dominate the entire low- and medium performance range of IFOG system.

2021 ◽  
Author(s):  
Xin Chen ◽  
Miao Yan ◽  
Jie Yu ◽  
Ruoxiang Tang

2020 ◽  
Vol 46 (10) ◽  
pp. 950-953
Author(s):  
E. V. Vostrikov ◽  
D. A. Pogorelaya ◽  
A. N. Nikitenko ◽  
A. S. Aleinik

2014 ◽  
Vol 5 (3) ◽  
pp. 993-1000
Author(s):  
P Nageswara Rao ◽  
S K Shrivastava

Single - axis missile fiber optic gyroscope requires a light source  with a band width> 10 nm and  output power  > 0.5 mW  .The commercial FOGs    weigh   200-250gms with  a physical size of 100mmX100mmX50mm..The type of light source for missile fiber optic gyroscope is selected by operating wavelength, wavelength stability with temperature, volume and physical size. Incase of space fiber gyroscopes,  the source should be insensitive to high energy radiation like proton and gamma radiations as well. Large bandwidth light source contributes to small bias drift by gyroscope. A small volume and light weight Single Pass Backward Signal Er3+  doped Super-fluorescent Fiber source was developed using only four commercially available components for use in  missile single axis fiber optic gyroscope .The bandwidth and output power of the source are 30. 507nm and1.318mW  respectively. We presented the experimental results along with non-flattened ASE spectrum. The packed super-fluorescent fiber  source   has   a  volume  of 100mm X 100mm X 25mm  and a weight of 150 grams which to our knowledge the  smallest  in volume and light in weight ever reported.


Author(s):  
Tien-Tsorng Shih ◽  
Chih-Wei Yu ◽  
Ren-Young Liu ◽  
Hao-Chi Chang ◽  
Oris Huang ◽  
...  

1996 ◽  
Author(s):  
Wolfgang Ecke ◽  
Klaus Hilpert ◽  
Andreas Holz ◽  
Rudolf Mueller ◽  
Michael Neukirch ◽  
...  

2019 ◽  
Vol 19 (19) ◽  
pp. 8733-8740 ◽  
Author(s):  
Daria A. Pogorelaya ◽  
Artem S. Aleynik ◽  
Alexander N. Nikitenko ◽  
Mikhail A. Smolovik ◽  
Vladimir E. Strigalev

Author(s):  
Dennis D. Earl ◽  
L. Curt Maxey ◽  
Jeff D. Muhs ◽  
Robert R. Thomas

We report on the performance of a new hybrid luminaire designed to blend light from a fiber optic solar source with electric fluorescent lamps. The luminaire design studied involves a commercially-available fluorescent luminaire that had been modified to include optical elements for efficiently dispersing a fiber optic solar light source. Quantitative measurements of the hybrid luminaire’s optical efficiency and spatial intensity distribution/deviations are discussed. The effects of static differences and dynamic fluctuations in spatial intensity distribution are qualitatively discussed and potential design improvements examined.


Author(s):  
Е.В. Востриков ◽  
Д.А. Погорелая ◽  
А.Н. Никитенко ◽  
А.С. Алейник

In this paper, the phase modulator optical phase drift reduction method is proposed and researched for LiNbO3 multi-functional integrated optical chip as a part of a fiber-optic gyroscope. This approach consists of applying a very high-frequency noise signal to a phase modulator in the range from 20 MHz to 100 MHz, which is outside of a fiber-optic gyroscope operating frequency range. The presented method showed that the increase in very high-frequency noise signal voltage up to around 1.7 half-wave voltages of the phase modulator allows decreasing optical phase drift by more than 4 times in the frequency range below 64.5 kHz.


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