article · 2003
Sagnac interferometer design for differential rotation measurement
Cited by 0Abstract and details only
Abstract
We have demonstrated a differential setup of two fiberoptic gyroscopes in series for measuring the difference in rotation between two parallel axes. The sensor is insensitive to global rotations affecting the two axis equally. The system can be used in structural monitoring of large sized objects such as ships and airplanes. The application at hand is a direct measurement of the torsion vibrations in ships. The idea is to put a Sagnac interferometer in each end of the ship with axis parallel to the alongside axis. This can be done using two independent gyroscopes, but the system developed here reduces the two independent gyroscopes to one interferometer.
Cite this paper
Vines, L., & Wang, G. (2003). Sagnac interferometer design for differential rotation measurement. https://doi.org/10.1109/ofs.2002.1000640
Vines, L., and G. Wang. “Sagnac interferometer design for differential rotation measurement.” vol. 1, 2003, pp. 395–98, https://doi.org/10.1109/ofs.2002.1000640.
Vines, L., and G. Wang. 2003. “Sagnac interferometer design for differential rotation measurement.” https://doi.org/10.1109/ofs.2002.1000640.
Vines, L. and Wang, G. (2003) ‘Sagnac interferometer design for differential rotation measurement’. Available at: https://doi.org/10.1109/ofs.2002.1000640.
@article{vines2003sagnac,
title = {{Sagnac interferometer design for differential rotation measurement}},
author = {Vines, L. and Wang, G.},
volume = {1},
pages = {395--398},
year = {2003},
doi = {10.1109/ofs.2002.1000640}
}Made from the index record. Check names, capitalisation and page numbers against the paper. Need another style? AI for Research has over 10,000.