Interface configuration for rate sensor apparatus

• US 5,157,461 A
• Filed: 06/14/1990
• Issued: 10/20/1992
• Est. Priority Date: 06/14/1990
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Smiths Industries Aerospace & Defense Systems Incorporated (General Electric Company)
• Inventors: Page, Jerry L.
• Primary Examiner(s): Buczinski, Stephen C.
• Application Number:
  US07/544,144
• Time in Patent Office: 859 Days
• Field of Search: 356/350, 350/96.15, 350/96.2, 350/96.12, 350/96.21, 350/96.31, 350/96.342, 385/14, 385/15
• US Class Current: 356/462
• CPC Class Codes: G01C 19/72 with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers
• CPC Class Codes: G01C 19/721 Details
• CPC Class Codes: G01C 19/728 Assemblies for measuring along different axes, e.g. triads

Abstract

An optical rate sensor apparatus (300) measures rates of angular rotation along a plurality of orthogonal axes. The apparatus (300) comprises a passive ring Sagnac interferometric arrangement having a light source circuit (308) and a series of multi-turn fiber optic rings (302, 304, 306). An optics/modulator circuit (312) selectively switches optical waves emitted from the light source circuit (308) into gyroscope channels and transmits the signals through fiber optic rings as counter-propagating optical waves. The optics/modulator circuit (312) also recombines the optical waves after they emerge from the corresponding rings. The optics/modulator circuit (312) includes optical components integrated onto an integrated optics chip (IOC) consisting substantially of lithium niobate. Optical fibers (606, 608) are coupled from the rings (302, 304, 306) to the integrated optics chip. To reduce bias error effects of reflections, the interface (610) between the optical fibers and the integrated optics chip is angled in the plane of the interferometer. Also, the angled interface (610) creates a path length difference greater than the coherence length of the reflections traversing the IOC optical paths between the interface (610) and circuitry which recombines optical waves on the IOC paths.

Claims

1. A rate sensor for use in inertial reference systems to detect angular rotations and measure magnitudes and directional sense of the rates of angular rotations, said rate sensor comprising:

optical source means for generating an incoming optical source wave signal having a predetermined wave length;

at least one gyroscope channel comprising;

an optical fiber ring;

optics circuit means for splitting said source wave signal into a pair of counter-propagating optical waves, and for recombining said counter-propagating optical waves into an outgoing wave signal wherein resultant fringe patterns are representative of the relative phases of said counter-propagating waves; and

optical path means for interconnecting said optical source means, said optics circuit means, and said optical fiber ring so as to apply said incoming optical source wave signal to said optics circuit means, to apply said counter-propagating optical waves through said optical fiber ring and to apply said counter-propagating optical waves emerging from said optical fiber ring back to said optics circuit means;

detection circuit means connected to said gyroscope channel for generating an intensity signal indicative at least in part of said resultant fringe patterns; and

signal processing means connected to said detection circuit means and responsive to said intensity signal for generating output signals corresponding at least in part to said rate of angular rotation;

characterized in that said optical path means further comprises;

first path means comprising at least in part a pair of first optical waveguides, each of said pair of first optical waveguides having substantially identical first indices of refraction and forming a first plane;

second path means comprising at least in part a pair of second optical waveguides, each of said pair of second optical waveguides having substantially identical second indices of refraction different from said first indices of refraction; and

said second pair of optical waveguides is coupled to said first pair of optical waveguides so that a boundary formed between said first and said second pairs of optical waveguides is angled within said first plane and relative to a plane passing transversely through longitudinal axes of each of said first pair of optical waveguides.

2. A rate sensor in accordance with claim 1 characterized in that the angle of said boundary relative to said transverse plane is such that reflection angles, of wave signals propagating in each of said pair of first optical waveguides toward said boundary and reflected in part from said boundary, are greater in value than acceptance angles of each of said pair of first optical waveguides.

3. A rate sensor in accordance with claim 2 or claim 1 characterized in that the angle of said boundary relative to said transverse plane is such as to create a path length difference between a path length of a first one of said pair of first optical waveguides and a path length of a second one of said pair of first optical waveguides, and said path length difference is greater than a coherence length of said counter-propagating optical waves.

4. A rate sensor in accordance with claim 3 characterized in that said optical source means comprises a broadband optical source having a sufficiently wide bandwidth so as to allow a physical realization of said path length difference without requiring any substantial increases in path lengths of either of said pair of first optical waveguides.

5. A rate sensor in accordance with claim 4 characterized in that said broadband optical source comprises a bandwidth in the range of 15 to 100 nanometers.

6. A rate sensor in accordance with claim 1 characterized in that each of said first indices of refraction is greater in value than each of said second indices of refraction.

7. A rate sensor in accordance with claim 1 characterized in that said pair of first optical waveguides is formed on an integrated optics chip.

8. A rate sensor in accordance with claim 7 characterized in that said integrated optics chip includes a single integrated chip comprising a crystal of z-cut, x-propagating lithium niobate.

9. A rate sensor in accordance with claim 7 characterized in that said integrated optics chip includes a single integrated chip comprising a crystal of x-cut, y-propagating lithium niobate.

10. A rate sensor in accordance with claim 8 or claim 9 characterized in that said first waveguides are formed on a surface of said crystal by a relatively thin film of titanium indiffused into said crystal at a relatively high temperature.

11. A rate sensor in accordance with claim 1 characterized in that said pair of second optical waveguides is formed of optical fiber materials.

12. A rate sensor in accordance with claim 1 characterized in that:

said first path means is optically interconnected between said optics circuit means and said boundary; and

said second path means is optically interconnected between said first path means and said optical fiber ring.

13. A rate sensor in accordance with claim 12 characterized in that said optics circuit means comprises splitting means for splitting said source wave signal into a pair of counter-propagating optical waves, said splitting means having a pair of optical paths emerging from one side thereof, and each of said pair of first optical waveguides is optically interconnected to a corresponding one of each said optical paths emerging from said splitting means.

14. A rate sensor in accordance with claim 13 characterized in that said splitting means is a Y-coupler.

15. A rate sensor in accordance with claim 3 characterized in that:

said first one of said pair of first optical waveguides and said second one of said pair of first optical waveguides are substantially parallel to each other and positioned substantially within a first plane; and

each of said pair of second optical waveguides are substantially parallel to each other and angled relative to said pair of said first optical waveguides within said first plane.

16. A rate sensor for use in inertial reference systems to detect angular rotations and measure magnitudes and directional sense of the rates of angular rotation, said rate sensor comprising:

optical source means for generating an incoming optical source wave signal having a predetermined nominal wavelength;

at least one gyroscope channel comprising;

a passive ring path having first and second ends;

splitting means for splitting said source wave signal into a pair of counter-propagating optical waves;

optical path means for applying said counter-propagating optical waves through said associated ring path, wherein said counter-propagating optical waves emerge therefrom with a relative Sagnac phase shift indicative of the rate of angular rotation of said ring path; and

combining means for recombining said counter-propagating waves into an outgoing optical wave signal, wherein the resultant low order fringe pattern is representative of the relative phases of said counter-propagating waves;

detection circuit means connected to said gyroscope channel for generating an intensity signal indicative of said resulting low order fringe pattern; and

signal processing means connected to said detection circuit means and responsive to said intensity signal for generating output signals corresponding to said rates of angular rotation;

characterized in that said optical path means comprises;

a first optical waveguide coupled to an optical path emerging from said splitting means, and having a first path length;

a second optical waveguide coupled to another optical path emerging from said splitting means, said second optical waveguide being substantially parallel to said first optical waveguide and having a second path length, and forming a first plane with said first optical waveguide;

a third optical waveguide coupled between said first optical waveguide and said first end of said passive ring path;

a fourth optical waveguide coupled between said second optical waveguide and said second end of said passive ring path, and positioned substantially parallel to said third optical waveguide; and

a boundary formed by interfaces between said first and third optical waveguides, and between said second and fourth optical waveguides, is angled within said first plane relative to a plane passing transversely through longitudinal axes of said first optical waveguide and said second optical waveguide.

17. A rate sensor in accordance with claim 16 characterized in that said first path length and said second path length have a difference therebetween greater than a coherence length of said incoming source wave signal.

18. A rate sensor in accordance with claim 17 characterized in that said optical source means comprises a broadband optical source having a sufficiently wide bandwidth so as to allow a physical realization of said difference without requiring any substantial increases in path lengths of either said first optical waveguide or said second optical waveguide.

19. A rate sensor in accordance with claim 16 or claim 17 characterized in that said boundary is angled relative to said first plane at an angle greater than an acceptance angle of each of said first and second optical waveguides.

20. A rate sensor in accordance with claim 19 characterized in that each of said first and said second optical waveguides is formed on a monolithic integrated optics chip.

21. A rate sensor in accordance with claim 20 characterized in that each of said third and said fourth optical waveguides is formed of optical fiber materials.