Fiber optic Sagnac interferometer with spatial filter

Optics: measuring and testing – By light interference – Rotation rate

Reexamination Certificate

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Reexamination Certificate

active

06563587

ABSTRACT:

BACKGROUND
1. Field of the Invention
The present invention relates to apparatus for measurement of rotation rate. More particularly, the invention pertains to improved fiber optic Sagnac interferometers.
2. Description of the Prior Art
Fiber optic Sagnac interferometers, especially those for determining rotational speed (fiber gyroscopes) are currently often constructed in a reciprocal minimum configuration. This optical architecture is known from the literature and may be described below briefly with the aid of FIG.
3
.
A light source
1
(e.g. a superluminescent LED (SLD)) is connected to a coupler
3
through an optical fiber
2
. In the reverse direction (i.e., the direction opposite to the light irradiated by the source
1
), a light-sensitive detector
5
(also known as a receiver) is connected to the coupler
3
through an optical fiber
4
.
Irradiated light reaches a beamsplitter
8
through a spatial filter
6
and a polarizer and polarization filter
7
. The beamsplitter splits the incoming light approximately in half so that the optical fiber
9
, connected at the two outputs of the beamsplitter
8
and preferably wound to form a coil, is penetrated by two counterrotating component light waves. After traversing the optical fiber
9
, the component light waves are reunited in the beamsplitter
8
, then traverse the polarization filter
7
, the spatial filter
6
, the coupler
3
and the optical fiber
4
to the receiver
5
. A phase modulator
10
in the light path of the optical fiber
9
wound to form the coil insures a suitable operating point of the interferometer via an electronic control system (not shown).
Mathematical models for describing the sensor signal received at the receiver
5
have been devised by many scientists and authors. The signal errors that result from physical inadequacies have been described by error models (See, for example, Canadian patent 1,276,274.) Such error models distinguish amplitude and intensity errors of fiber gyroscopes for the optical arrangements described briefly above. Amplitude errors result from interference from waves that are orthogonally polarized upstream of the polarization filter
7
and transferred by cross coupling to the same polarization direction. Intensity errors result from interference from waves originally of the same polarization and rotated to the polarization direction by cross coupling.
An important parameter in the mathematical description of the amplitude error is the polarization ratio of the light upstream of the polarization filter, the polarizes. The larger the component to be suppressed by the polarizes, the greater the amplitude error. If the amplitude error becomes the dominant error component, the technical task is to reduce the latter.
In the prior art, it is known, for example, to use light sources that emit light with a large polarization factor. Using polarization-maintaining fibers, such polarized light can be directed to the polarizes so that the component of false polarization is small. If no polarization-maintaining fiber is employed, the light is generally completely depolarized to avoid a situation in which inadvertent rotation of the polarization direction can result in only a very small component of the light passing the downstream polarizes.
A substantial cost factor of the first-mentioned solution is that of the production of the coupler
3
(at the light source
1
) and the light receiver
5
from polarization-maintaining fiber as fiber couplers of polarization-maintaining fiber are substantially more expensive than those of simple monomode fiber. In the latter case, depolarization of the light generates a large component of false polarization upstream of the polarization filter
7
that unfortunately amplifies the amplitude error.
SUMMARY AND OBJECTS OF THE INVENTION
It is therefore an object of the invention to reduce amplitude error substantially as the dominant error component in a fiber optic Sagnac interferometer.
It is a further object of this invention to achieve the above object without couplers of polarization-maintaining fiber.
The present invention achieves the preceding and other objects by providing an improvement in a fiber optic Sagnac interferometer of the type having a light source connected through an optical fiber to an input of an optical directional coupler. At least one output of the coupler is connected via a spatial filter and a polarization filter to a beamsplitter that splits the light transmitted by the polarization filter into two component beams. The component beams are irradiated into the two ends of an optical fiber. The beamsplitter reunites the component light beams returning after traversing the optical fiber through the other end of the optical fiber. The reunited component light beams are applied in reverse direction through the polarization filter, the spatial filter and the directional coupler to a light-sensitive receiver connected to the coupler. The improvement provided by the invention comprises the spatial filter being of polarizing monomode fiber.
The foregoing features of the invention are described in the detailed description that follows. Such description is accompanied by a set of drawing figures in which numerals, corresponding to those of the written description, identify the features of the invention with like numerals referring to like features throughout both the written description and the drawing figures.


REFERENCES:
patent: 4480915 (1984-11-01), Arditty et al.
patent: 4875775 (1989-10-01), Michal et al.
patent: 4944591 (1990-07-01), McMichael
patent: 5137360 (1992-08-01), Ferrar
patent: 5141316 (1992-08-01), Lefevre et al.
patent: 5331404 (1994-07-01), Moeller et al.
patent: 5365337 (1994-11-01), Page et al.
patent: 5377283 (1994-12-01), Blake et al.
patent: 3446663 (1986-07-01), None
patent: 4223740 (1994-01-01), None
patent: 0474389 (1992-03-01), None
Article: “Polarization and Depolarization in the Fiber-Optic Gyroscope” by R. Ulrich,Selected Papers on Fiber Optic Gyroscopes(SPIE Milestone Series, vol. MS 8) (Jan. 1, 1982).
Article: “Progress in Optical Fiber Gyroscopes Using Integrated Optics” by H.Lefevre, J. Bettini, S. Vatoux and M. Papuchon,Selected Papers on Fiber Optic Gyroscopes(SPIE Milestones Series, vol. MS 8) (Jan. 13, 1985).

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