Classifications

• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
  • G02B6/10—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type
  • G02B6/12—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type of the integrated circuit kind
  • G02B6/122—Basic optical elements, e.g. light-guiding paths
  • G02B6/125—Bends, branchings or intersections
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
  • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
  • G01C19/58—Turn-sensitive devices without moving masses
  • G01C19/64—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
  • G01C19/72—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers
  • G01C19/725—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers using nxn optical couplers, e.g. 3x3 couplers
• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
  • G02B6/24—Coupling light guides
  • G02B6/26—Optical coupling means
  • G02B6/28—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals
  • G02B6/2804—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals forming multipart couplers without wavelength selective elements, e.g. "T" couplers, star couplers
• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
  • G02B6/24—Coupling light guides
  • G02B6/26—Optical coupling means
  • G02B6/28—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals
  • G02B6/2804—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals forming multipart couplers without wavelength selective elements, e.g. "T" couplers, star couplers
  • G02B2006/2865—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals forming multipart couplers without wavelength selective elements, e.g. "T" couplers, star couplers couplers of the 3x3 type

Definitions

• This invention relates generally to Sagnac effect rotation sensors and particularly to fiber optic rotation sensors that guide counterpropagating light waves in a sensing loop to measure rotations about a sensing axis perpendicular to the plane of the sensing loop. Still more particularly, this invention relates to fiber optic rotation sensors that use 3x3 couplers to supply optical signals to the sensing loop and to guide the optical output signals from the sensing loop to electrical apparatus that processes the optical output signals to determine the rotation rate.
• Fiber optic rotation sensors are well-known in the art. Previous fiber optic rotation sensors included evanescent field couplers to couple light between two lengths of optical fiber. Subsequently, fiber optic rotation sensors using 3x3 coupler were developed. The primary advantage of using a 3x3 coupler in a fiber optic rotation sensor is the ease with which such devices are interfaced with electronics.
• United States Patents 4,440,498 and 4,479,715 to Sheem disclose two fiber optic rotation sensors that include 3x3 couplers.
• United States Patent 4,440,498 is directed to a fiber optic rotation sensor that includes a fiber optic sensing loop and an input fiber.
• a 3x3 fiber optic coupler divides light between the input fiber and the two legs of the fiber optic sensing loop.
• United States Patent 4,479,715 discloses a Sagnac effect rotation sensor in which the ends of a fiber optic sensing loop are coupled to a pair of optical waveguides.
• Light is input to a central input waveguide that is between the optical waveguides that are coupled to the ends of the sensing loop fiber.
• the three optical waveguides are arranged to form a 3x3 optical coupler.
• the input light is coupled from the central input waveguide to the optical waveguides that are connected to the optical fiber coil to produce the counterpropagating waves in the fiber optic sensing loop.
• the waves traverse the sensing coil and combine in the coupler.
• the combined waves are detected, and the resulting electrical signals are processed to determine the rotation rate.
• Poisel et al. discloses an optical fiber gyroscope that uses a 3x3 coupler to couple optical signals into and out of a fiber optic sensing loop.
• Poisel et al. discloses a photodetector arranged to detect the light that has been input the 3x3 coupler that is not coupled into the fiber optic sensing loop. The electrical signal resulting from detecting this light is used in signal processing circuitry to make adjustments for variations in the input light intensity.
• Such fiber optic rotation sensors may be operated in phase quadrature, which provides maximum sensitivity at zero rotation rate.
• previous fiber optic rotation sensors that include 3x3 optical couplers are sensitive to temperature changes.
• the coupling ratios of the 3x3 fiber optic couplers are temperature-sensitive such that bias errors of 1000° per hour are typically observed. Errors of such magnitude are unacceptable for most applications of rotation sensors.
• the present invention is an improved fiber optic rotation sensor using 3x3 couplers with optimized coupling ratios.
• the coupling ratios are selected to prevent changes in the amount of light coupled into the two counterpropagating waves caused by temperature changes and other mechanical factors.
• the selected coupling ratios also maximize the optical power output that is delivered to the rate photodetectors.
• a fiber optic rotation sensor comprises a 3x3 optical coupler that includes first, second and third optical waveguides arranged to have an interaction length in which light couples between the first, second and third optical waveguides, the first, second and third optical waveguides being formed such that the fractions of light coupled from any one of the first, second and third optical waveguides to the other two optical waveguides are constant, independent of thermally- induced changes in the interaction length.
• An optical signal source is arranged to provide an input optical signal to the first optical waveguide such that portions of the input optical signal are coupled from the first optical waveguide into the second and third optical waveguides.
• the optical fiber in which the sensing loop is formed has ends that are coupled to the second and third optical waveguides to receive optical signals that form counterpropagating optical waves in the sensing loop and to combine the counterpropagating optical waves after they have traversed the sensing loop.
• the optical coupler is formed such that first, second and third optical waveguides being formed such that the optical splitting ratios between the first, second and third optical waveguides are 0.4108 : 0.1783 : 0.4108, so that when light intensity A 2 is input to the first optical waveguide, the optical intensity output by each of the second and third optical waveguides to the optical fiber to form the counterpropagating waves is 0.4108 A 2 and the optical intensity output by the first optical waveguide is 0.1783A 2 .
• FIG. 2 schematically illustrates a 3x3 coupler
• FIG. 3 illustrates the derivative with respect to coupling length of the intensity of the signal output by the fiber optic rotation sensor of FIG. 1.
• a fiber optic rotation sensor 10 includes a 3x3 optical coupler 12 and a length of optical fiber 13 arranged to form a fiber optic sensing coil 14.
• the optical coupler 12 includes optical waveguides
• the optical fiber 13 has ends 16 and 18.
• the fiber ends 16 and 18 are butt-coupled to ends 20 and 22 of the corresponding optical waveguides 1 and 2, respectively.
• a pair of output optical fibers 30 and 32 are connected to ends 34 and 36 of the optical waveguides 2 and 3, respectively.
• the output optical fiber 30 directs a light beam to first photodetector 38, which produces an electrical signal S ] that is indicative of the intensity of the optical signal transmitted thereto by the output optical fiber 30.
• the output optical fiber 32 directs a beam of light to a second photodetector 40. which produces an electrical signal S 2 that is indicative of the intensity of the optical signal transmitted thereto by the output optical fiber 32.
• the optical waveguide 1 is formed in the substrate 15 between the optical waveguides 2 and 3.
• the optical waveguides 1-3 are arranged to form the 3x3 coupler 12.
• the 3x3 coupler 12 is preferably an evanescent field coupler.
• An input optical fiber 46 has an end 48 that receives light from a light source 50.
• the other end 52 of the input optical fiber 46 is butt- coupled to an end 54 of the optical waveguide 1.
• An output optical fiber 56 has one end 58 butt-coupled to an end 60 of the central optical waveguide 3.
• the other end 62 of the output optical fiber 56 directs a beam of light to a third detector 64, which produces an electrical signal S 3 that is indicative of the intensity of the optical signal transmitted thereto by the output optical fiber 56.
• the 3x3 coupler 12 is preferably an evanescent field coupler that couples optical signals between the optical waveguide 1 and the optical waveguides 2 and 3. A portion of the light input to the 3x3 fiber optic coupler 12 remains in the optical waveguide 1.
• the 3x3 coupler has a coupling length L in which the evanescent fields of light waves guided by the waveguides 1-3 interact so that light couples between them.
• the intensity of light coupled between the waveguides 1-3 is a function of the coupling length L.
• the temperature of the coupler 12 fluctuates, the light intensity coupled between the waveguides 1- 3 also fluctuates.
• the three coupling ratios of the 3x3 optical coupler 12 are all equal to 1/3.
• the coupling ratios are all equal to 1/3, the light intensities output from the three optical waveguides 1-3 are equal.
• the present invention comprises a fiber optic rotation sensor using a 3x3 coupler that have coupling ratios selected to minimize the bias errors to the order of 10° to 100° per hour and which is insensitive to temperature changes. It has been found that there is a set of coupling ratios for which the fraction of light coupled into any selected one of the optical waveguides 1-3 remains constant as the coupling length L changes in response to temperature changes.
• the optimum configuration for the 3x3 optical coupler 12 is insensitive to temperature changes while providing a larger rate discriminant than has been obtained with previous designs.
• the 3x3 fiber optic coupler 20 may be described by the linear differential equations da.
• a ⁇ is the light amplitude in waveguide j; and k is the coupling ratio between any two of the three fibers 1-3.
• k 12 is the coupling ratio between waveguides 1 and 2; k 23 is the coupling ratio between waveguides 2 and 3, and k 1 is the coupling ratio between waveguides 3 and 1.
• the optical intensity in the optical waveguides 2 and 3 is the optical intensity input to the fiber optic sensing coil 14 at the ends 16 and 18 of the optical fiber 12. Therefore the input to the legs of the fiber optic i ⁇ I ⁇ 2 gyroscope are
• the angle ⁇ is the Sagnac phase shift angle between the beams caused by rotation of the sensing loop at angular velocity ⁇ about the sensing axis, which is perpendicular to the plane of the fiber optic sensing coil 14.
• the phase angle ⁇ and the angular velocity ⁇ are related by the Sagnac equation:
• the optical signals that have been output from the output of the fiber optic sensing coil are given by:
• the signal output of the fiber optic rotation sensor 10 may be written in terms of S,, S 2 and S 3 :
• the coupler 12 is insensitive to variations in coupling length that typically occur over time and temperature.
• the signals on the output legs are higher for this set of coupling ratios than for other coupling ratios.

Landscapes

• Physics & Mathematics (AREA)
• Optics & Photonics (AREA)
• Engineering & Computer Science (AREA)
• General Physics & Mathematics (AREA)
• Electromagnetism (AREA)
• Power Engineering (AREA)
• Radar, Positioning & Navigation (AREA)
• Remote Sensing (AREA)
• Microelectronics & Electronic Packaging (AREA)
• Gyroscopes (AREA)

Applications Claiming Priority (1)

Publications (1)

Family

ID=22250263

Family Applications (1)

Country Status (3)

Families Citing this family (2)

• 1995
  • 1995-12-08 EP EP95943772A patent/EP0808448A1/de not_active Ceased
  • 1995-12-08 JP JP9522002A patent/JPH11500830A/ja not_active Ceased
  • 1995-12-08 WO PCT/US1995/016178 patent/WO1997021981A1/en not_active Application Discontinuation

Non-Patent Citations (1)

Also Published As

Similar Documents

Legal Events