CA2258628A1 - A three-axis fiber optic gyroscope - Google Patents
A three-axis fiber optic gyroscope Download PDFInfo
- Publication number
- CA2258628A1 CA2258628A1 CA002258628A CA2258628A CA2258628A1 CA 2258628 A1 CA2258628 A1 CA 2258628A1 CA 002258628 A CA002258628 A CA 002258628A CA 2258628 A CA2258628 A CA 2258628A CA 2258628 A1 CA2258628 A1 CA 2258628A1
- Authority
- CA
- Canada
- Prior art keywords
- port
- coupler
- fiber optic
- junction
- depolarizer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
Classifications
-
- 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
- G01C19/728—Assemblies for measuring along different axes, e.g. triads
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Optics & Photonics (AREA)
- Electromagnetism (AREA)
- Power Engineering (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Gyroscopes (AREA)
Abstract
A gyroscope having three fiber optic loops for sensing rates of rotation in three axes orthogonal to one another. The gyroscope has one or two detectors and one source that is shared among the three fiber optic sensing loop subsystems with a special multicoupler configuration. Also, portions of the rotation rate signal processing electronics, whether an open or closed loop configuration, are shared among the three sensing loops. The gyroscope may be a single mode optical fiber depolarized configuration or a polarization maintaining optical fiber configuration.
Description
CA 022~8628 1998-12-16 2 1 PCT/USg7/11412 A THREE-AXIS FIBER OPTIC GYROSCOPE
BACKGROUND OF THE INVENTION
Typical inertial me~u.~;.,lent units have three g~,osco))es. A fiber optic inertial measurement system involves at least three fiber optic gyroscopes. Separate gyroscopes for each of the three axes involves a duplication of optical and electronic circuits.
SUMMARY OF THE INVENTION
The present invention is a three-axis fiber optic gyroscope that is a~plu~l;ate for an inertial measurement unit. The gyroscope measures rates of rotation for each of the three orthogonal axes. The three-axis fiber optic gyroscope of the present invention uses fewer optical and electronic components while still efficiently delivering sufficient optical power from a source through each gyroscope to the detector. A single source, one or two detectors, one preamplifier and two directional couplers are used outside the three interferometers. In contrast, the same task performed by the standard approach in the art uses three single axis gyros that require three sources, three detectors, three preamplifiers and three directional couplers. The electronics for the gyroscopes may be open loop or closed loop. Serrodyne, digital phase step and dual ramp electronics are options for a closed loop configuration. The interferometer or gyroscope for each axis of a three axis system can deliver nearly the same amount of power to the detector as a single axis configuration.
Figure 1 shows the optical configuration for the three axis gyroscope having onepolarization mz,i.ll~;-,ing coupler and four Y junctions.
Figure 2 shows the optical configuration for the three axis gyroscope having onenon-polarization m ~int~ining coupler and four Y junctions.
Figure 3a shows a three axis gyroscope having two polarization m~int~ining couplers and three Y junctions.
Figure 3b reveals a three axis gyroscope having two polarization m ~in~ining couplers, and three couplers at the sensing loops.
Figure 4a shows a three axis gyroscope having two non-polarization m ~int~ining 3 0 couplers and three Y junctions.
Figure 4b reveals a three axis gyroscope having two non-polarization m~ inil~g couplers, and three couplers at the sensing loops.
CA 022~8628 1998-12-16 Figure 5 shows an example of closed loop serrodyne electronics.
Figure 6 shows an example of dual ramp closed loop electronics.
Figure 7 shows the dual ramp closed loop electronics having a demodulator for each axis.
Figure 8 reveals an optical configuration for the three axis gyroscope having one non-polarization m~ g coupler and four Y junctions, and being without depolarizers at the sensing loops.
Figure 9 reveals a three axis gyroscope having two polarization m~ ,g couplers and three Y junctions, and being without depolarizers at the sensing loops.
Figure I shows a configuration 10 for a three axis fiber optic gyroscope (FOG) having one polarization m~int~ining (PM) fiber coupler 12 and an integrated optical circuit (IOC) 14 with four Y junctions 32, 34, 36 and SS. Coupler 12 is a coupler fabricated from PM fiber Light source 16 emits broad band light having a middle 1 5 wavelength of 0.83 microns. Light source 16 may be at some other wavelength. The light enters coupler 12 via fiber or port 18 and the light goes through coupler 12 wherein about half the light goes out on port or fiber 20 and the other half the light goes out on port or fiber 22, under the assumption that there is no light loss in coupler 12.
In this embodiment, coupler 12 is designed for 0.83 micron light. Fiber 20 is 2 0 connected to pigtail 13 of waveguide 28 via splice 11, of integrated optical circuit (IOC) 14 with aligned axes at splice 11 and connection 30. IOC 14 may be a proton exchange or titanium indiffused lithium niobate device. Also, IOC 14 may be fabricated from other materials such as silicon, tantalum, polymers and so on. The proton exchange device has polarizing waveguides 28, 38, 40, 46, 47, 53, 56, and 57. If IOC 14 is a 2 5 titanium indiffused device, then the IOC has a conductive sheath on it and over the waveguides thereby causing the respective waveguides to be pol~ri7ing.
The light is split 50/50 at Y junction 32 such that one half of the light to junction 32 goes to junction 34 and the other half of the light as a result of the split by junction 32 goes to junction 36. This ratio of light is with the assumption that there is little or no 3 0 loss of light at the junctions or in the waveguides of IOC 14. The other half of the light that enters junction 36 is split in half such that light propagates down light waveguides 38 and 40. Light in waveguide 38 propagates through connection 64, depolarizer 41 CA 022~8628 1998-12-16 and through loop 42 and on back through depolarizer 43, connection 64 and down waveguide 40. Light passing through waveguide 40 is subject to modulation by modulator 44. Light propag~in~ toward loop 42 down waveguide 40 goes through depolarizer 43 and through the loop 42 and back out of loop 42 and through depolarizer 41 and down through waveguide 38 0f IOC 14. The ~ g beams of light are combined from waveguides 38 and 40 at Y junction 36 and move towards junction 32.
Depolarizers 41 and 43 may be constructed in various ways. For in~t~nce~ in depolarizer 41, a PM fiber 154 is ~tt~checl to IOC 14 at point 64, with its birefringent axes aligned with the birefringent axes of waveguide 38. Fiber 154 may be a pigtail of 1 0 IOC 14. Another PM fiber 156 is spliced to fiber 154, with the birefringent axes of fibers 154 and 156 aligned at about 45 degrees relative to each other, at connection point 155. Fiber 156 is spliced to single mode non-polarization m;~ t;~ ;r.g fiber of coil 42 at connection 157. Fiber 156 is typically more than twice the length as fiber 154.
On the other hand, depolarizer 41 may have only one PM fiber 154 which has birefringent axes aligned at about 45 degrees relative to the axes of waveguide 38, at pigtail 64. Fiber 154 is then spliced to coil 42 at connection point 157. The beat length of fiber 154 is more than twice the beat length of waveguide 38. Splice 155 and fiber 156 are not needed in this depolarizer configuration.
Depolarizer 43 may be used in conjunction with depolarizer 41 or it may be 2 0 absent, thereby resulting in only one depolarizer 41 for coil 42. However, both depolarizers 41 and 43 result in better FOG perforrnance.
If depolarizer 43 is to be used it has the same structure as depolarizer 41 except that the length of fiber 158 is slightly different in length than that of fiber 154 and that the length of fiber 159 is more than four times the length of fiber 158, although fiber 2 5 159 may be more than twice the length of fiber 156.
ln the depolarizer 41 configuration having just the one PM fiber 154 with axes aligned with waveguide 38 axes, a similarly structured depolarizer 43 may or not be incorporated. If depolarizer 43 is incorporated, then the structure of the depolarizer may be that of two PM fibers 158 and 159, with fiber 159 having more than twice the beat 3 0 length of fiber 154 in the depolarizer configuration where fiber 154 axes are aligned at 45 degrees relative to waveguide axes at connection point 64. Depolarizer 43, inconjunction with either depolarizer 41 configuration, may have only fiber 158 which has CA 022~8628 1998-12-16 its birefringent axes aligned at 45 degrees relative to the axes of waveguide 40 at pigtail ~ 64. Fiber 158 in the latter structure, without splice 155 and fiber 159, has a beat length that is more than twice the beat length of waveguide 40, or it may have more than four times the beat length of waveguide 40 if depolarizer 41 has the same kind of ~ c as the latter depolarizer 43.
Depolarizers 48 and 49 have similar structure combinations as depolarizers 41 and 43, respectively. Likewise depolarizers 58 and 59 have similar structure combinations as depolarizers 41 and 43, respectively. The structures of depolarizers noted here are applicable to all figures having depolarizers 41, 43, 48, 49, 56 and 59.
1 0 A light from junction 34 is split and light beams propagate down waveguides 46 and 47 on through connection 64 and depolarizers 48 and 49, respectively, and counterpropagate through loop 45 and return through depolarizers 49 and 48, and connection 64 respectively. A light that passes either way through waveguide 47 is subject to modulation by modulator 50. The returning light beams from loop 45 via 1 5 waveguides 46 and 47 are combined at junction 34 and the resultant light goes on to junction 32 which is combined with light from junction 36. The combined light goes down waveguide 28, through connection 30 and into fiber or port 20 of coupler 12.
The other portion of the light from source 16 in coupler 12 goes through fiber or port 22 on to waveguide 53 of IOC 14 via splice 15, pigtail 17 and connection 54 with aligned axes at splice 15 and connection 54. Light going through waveguide 53 is split at Y junction 55 into wherein half the light goes down waveguide 56 and the other half the light from waveguide 53 goes through waveguide 57. The light goes through depolarizers 58 and 59 from waveguides 56 and 57, respectively. The light waves or beams counterpropagate through loop 60 and retD through depolarizers 59 and 58 and go through waveguides 57 and 56, respectively, to be combined at Y junction 55. Light prop~g~tin~ through waveguide 57 may be modulated by modulator 61. The combined light from junction 55 propagates down waveguide 53, through connection 54 and into port or fiber 22 of coupler 12. About half the light from port 20 goes into port or fiber 62 and half the light from port 22 is combined with the light from port 20 and goes 3 0 down port 62 into detector 63.
The light from port 62 constitutes interferences of pairs of beams of loops 42, 45 and 60. Detector 63 electrically converts the light beams and their respective CA 022~8628 1998-12-16 interferences into electrical signals which are deciphered into rate of rotationinformation of loops 42, 45 and 60. IOC 14 is designed for 0.83 micron wavelength of source light. The depolarizers which may be made of PM fiber are aligned respectively to waveguides of IOC 14 at a 45 degree angle (+/- 2 degrees) between the polarization axes of each PM fiber and the re~ecli~e waveguide of IOC 14. The resultant depolarizers are designed for 0.83 micron of light.
The fiber for coils 42, 45 and 60 is single mode fiber, that is, it is non-polarization maintaining fiber, and is de~igned for a wavelength of 1.3 microns of light.
The depolarizers 48, 49, 41, 43, 58 and 59 are spliced to the single mode fiber of the 1 0 respective loops.
Figure 2 shows a configuration 90 for a three axis fiber optic gyroscope (FOG) having one single-mode fiber coupler 12 and an integrated optical circuit (IOC) 14 with three Y junctions 34, 36, 55. Coupler 12 is a coupler fabricated from single mode non-polarization m~int~ining (SM) fiber. Light source 16, which is a laser diode, emits 1 5 broad band light having a middle wavelength of 0.83 microns. Light source 16 may instead be a fiber optic light source of another wavelength.
There may be a polarization m~ g (PM) fiber 94 spliced onto port 18 of coupler 12 at point 95. PM fiber 94 axes are aligned at 45 degrees relative to the source 16 PM pigtail 96 axes at splice 97. lnstead, fiber 94 may be aligned at 45 degrees at 2 0 source 16 itself relative to the axis of the polarized light. The combination of fibers 94 and 96~ and splice 97 is not required but is desired for use with SM coupler 12. The fiber 94 and 96 and splice 97 combination is not used with a non-polarized fiber light source, which emits non-polarized light, as source 16.
The light enters coupler 12 via fiber or port 18 and the light goes through 2S coupler 12 wherein about half the light goes through port or fiber 20 and the other half the light goes through port or fiber 22, under the assumption that there is no light loss in coupler 12. Fiber coupler 12 is designed for 0.83 micron light. Fiber 20 at point 99 is spliced to a piece of PM fiber 98. PM fiber 98 is connected to a PM pigtail 24 at a 45 degree-axis aligned splice 26. Fiber 24 has a length that is at least twice the length of 3 0 fiber 98. Fiber pigtail 24 is attached to waveguide 28 at point 30 with aligned axes.
The depolarizer could instead include just PM fiber 24 having a 45 degree axis ~ignment with waveguide 28 at connection 30. The beat length of fiber 24 would be CA 022~8628 1998-12-16 WO 9~,~3~ 6 PCT/US97/11412 less than one-half of the beat length of waveguide 28. The light is split 50150 at Y
junction 32 such that one half of the light to junction 32 goes to junction 34 and the other half of the light as a result of the split by junction 32 goes to junction 36. The 50/50 ratio of light is based on the as~ .ylion that there is little or no loss of light at the 5 junction or in the waveguides of IOC 14. The light that enters junction 36 is split in half such that each half portion of the light propagates down light waveguides 38 and 40 respectively. Light in waveguide 38 propagates through connection 64, depolarizer 41 and through loop 42 and on back through depolarizer 43, connection 64 and down waveguide 40. Light passing through waveguide 40 is subject to modulation by 1 0 modulator 44.
Light prop;~g~ting toward loop 42 down waveguide 40 goes through depolarizer 43 and through loop 42 and back out of loop 42 and through depolarizer 41 and down through waveguide 38 of IOC 14. The returning beams of light are combined from waveguides 38 and 40, at Y junction 36 and moves towards junction 32.
1 5 A light from junction 34 is split and light beams propagate down waveguides 46 and 47 on through depolarizers 48 and 49, respectively, and counterpropagate through loop 45 and return through depolarizers 49 and 48, respectively. A light that passes either way through waveguide 47 is subject to modulation by modulator 50. The returning light from loop 45 via waveguides 46 and 47 is combined at junction 34 and 2 0 the resultant light goes on to junction 32 which is combined with light from junction 36.
The combined light goes down waveguide 28, through connection point 30 and through PM pigtail fiber 24, splice 26, PM fiber 98, and splice 99, respe~;lively, or alternatively just through 45 degree connection 30 and PM fiber 24, into fiber or port 20 of coupler 12.
2 5 The other portion of the light from source 16 goes through fiber or port 22 spliced at point 101 to a piece of PM fiber 102 which is at a 45 degree axis splice 51 connected to a PM pigtail or fiber 52. The length of fiber 52 is at least twice that of fiber 102. Fiber 52 is connected with aligned axes to waveguide 53 of IOC 14 at point 54. The depolarizer could instead include just PM fiber 52 having a 45 degree axis 3 0 alignrnent with waveguide 53 at cormection 54. The beat length of fiber 52 would be less than one-half of the beat length of waveguide 53. Light going through waveguide 53 is split at Y junction 55 into wherein halfthe light goes down waveguide 56 and the CA 022~8628 1998-12-16 other half the light from waveguide 53 goes through waveguide 57. The light goesthrough depolarizers 58 and 59 from waveguides 56 and 57, respectively. The light waves or beams cou~ opagate through loop 60 and return through depolarizers 59 and 58 and go through waveguides 57 and 56, les~e~ ely, to be combined at Y
5 junction 55. Light prop~ting through waveguide 57 may be mod~ tecl by modulator 61. The combined light from junction 55 propagates down waveguide 53, through point 54~ pigtail 52, splice 51, fiber 102, and splice 101, or alternatively just through 45 degree connection 54 and PM fiber 52, into port or fiber 22 of coupler 12. About half the light from port 20 goes into port or fiber 62 and half the light from port 22 is 1 0 combined with the light from port 20 and goes down port 62 on into detector 63. The light from port 62 constitutes interferences of pairs of beams of loops 42, 45 and 60.
Detector 63 electrically converts the light beams and their respective interferences into electrical signals which are deciphered into rate of rotation information of loops 42, 45 and 60.
IOC 14 is designed for 0.83 micron wavelength of source light. The depolarizers which may be made of PM fiber that is aligned respectively to waveguides of IOC 14 at a 45 degree angle (+/- 2 degrees) with respect to the polarization axis of the fiber of the depolarizer and the waveguide of IOC 14. The polarizers are designed for 0.83 micron of light. The fiber for coils 42, 45 and 60 is single mode fiber, that is, it 2 0 is non-polarization m~int~ining fiber, and is designed for a wavelength of 1.3 microns of light. Depolarizers 48, 49, 41, 43, 58 and 59 are of 0.83 micron PM fiber which is spliced to the single mode fiber of the respective loops and to IOC 14 at points 64 to the respective waveguides.
Configuration 100 of figure 3a involves an IOC 65 which may be split up into 2 5 three separate IOCs having junctions 34, 36 and 55, respectively, for each of the FOG
loops 45, 42 and 60. IOC 65 may have the same material and functional characteristics as IOC 14. IOC 14 and IOC 65 are preferred to have polarizing waveguides, although the waveguides may be polarization m~ i"ing or non polarization m~int~ining.
Configuration 100 uses two PM fiber optic couplers 66 and 67. IOC 65 has no Y junction splitter like Y junction 32 Of IOC 14 Of configuration 10. Source 16 is a laser diode and emits 0.83 micron broad band light which goes to coupler 66 via pigtail 91, splice 92 and port 68. Splice 92 is optional. To achieve equal detected optical CA 022~8628 1998-12-16 WO 98t00682 8 PCT/US97/11412 power from each of sensing coils 42, 45 and 60, the splitting ratio of first directional ~ coupler 66 is chosen al,lulu~l;ately. In the ideal case where each of directional couplers 66 and 67 are loss-less and each of the three coils 42, 45 and 60 are equally efficient, the splitting ratio of 33/67 at coupler 66 and S0/50 for coupler 67, produces or results in an 5 equal optical power from each sensor. If couplers 66 and 67 have losses, the light m:~king additional passes through the respective coupling region will suffer additional attenuation. Thus, the splitting ratio of coupler 66 needs to be di~le--t to compensate for this extra loss and still keep the power levels at detectors 69 and 93 the same for each of the three axes incorporating loops 42, 45 and 60. One example of this is the use 1 0 of a 30/70 instead of a 33/67 splitting ratio for coupler 66 to account for the loss occurred in couplers 66 and 67.
Light for the first loop 42 leaves source 16 and goes through port 68 of coupler66 and an approximately 70 percent portion of that light is split off into port 71 which goes to port 72 of coupler 67 via splice 73 with aligned axes. Fifty percent of the light 1 5 in port 72 goes to port 74 of coupler 67 and on through connection point 77, with aligned axes, into waveguide 78. The light goes through junction 36 through the colllpo~ of the gyroscope having loop 42.
The light returns after counterprop~g~ting through loop 42 back through waveguide 78, connection point 77, and on into port or fiber 74. How the light moves 2 0 through the components associated with loop 42 is described above with respect to configuration 10. Light coming back through port 74 of coupler 67 is split 50/50 and half that light goes to port 79 which is pigtailed to detector 69 thereby the light is being converted by detector 69 into electrical equivalents of the light signals. The light returns from loop 42 going through port 74 of coupler 67, and also the other portion of 2 5 the light goes through port or fiber 72 through aligned-axes splice 73 and port or fiber 71 of coupler 66. A portion of that light continues on through coupler 66 to port 81, and fiber 81 is either connected to detector 69 along with fiber 79, or to a second detector 93. to also be converted into representative electrical signals.
Light from source 16 for loop 45 goes through port 68 of coupler 66 which is portioned off at 70 percent to port 71. The light from port 71 goes through aligned-axes splice 73 and on through port 72 of coupler 67. Half of the light in port 72 goes to port 80 and on to IOC 65 at point 84. Point 84 is an aligned axis connection between port 80 CA 022~8628 1998-12-16 and waveguide 85, with or without splice 19 and pigtail 21. Similarly, light to or from ~ port 74 of coupler 67 and port 86 of coupler 66 may or may not go through splice 19 and pigtail 21. Light from point 84 goes through waveguide 85 on to be split by Y
junction 34. The light travels through the components associated with loop 45 as5 described above with respect to configuration 10. Light from junction 34, after countelprop~ting in loop 45, goes through waveguide 85, through point 84 on to port 80 of fiber optic coupler 67. A portion of the light in port 80 goes on to port 79 on to detector 69. The other portion of the light in port 80 goes through coupler 67 on to port 72 and through splice 73 and port 71. A portion of light in port 71 goes on to port 81 of 1 0 coupler 66 and to detector 69 or second detector 93. The received light at detector 69 or second detector 93 again is converted into electrical signals representative of the received optical signals.
The third axis rotation rate sensor incorporating loop 60, involves light from source 16 going through coupler 66 of which 30 percent goes on into port or fiber 86.
1 5 The light from port 86 goes on through point 54 to IOC 65, and continues on through waveguide 53. The propagation of light on into loop 60 is described above with respect to configuration 10. The light co~-tel~..,p~E;lting in loop 60 is combined at light junction 55 and returns through waveguide 53, point 54 and on into port 86 of coupler 66. 70 percent of the returning light in port 86 is coupled onto port 81 of coupler 66.
2 0 The light in port 81 goes on to detector 69 which converts the light into electrical signals representative of the optical signals in port 81.
Figure 3b shows a variation of configuration 100 in figure 3a. Y junctions 34, 36 and 55 are replaced with directional couplers 149, 14g and 150, respectively.Po}arizers 145, 146 and 147 are placed in optical fiber light paths between couplers 67 and 68, and couplers 148, 149 and 150, respectively. Electrooptic phase modulators 44, 50 and 61 are replaced with optical fiber piezoelectric phase modulators 151, 152 and 153, respectively. The IOC 65 waveguides functioning as light paths are replaced with optical fiber light paths.
Configuration 120 of figure 4a involves IOC 65 which may be split up into three 3 0 se~ ale IOCs for each of the FOG loops 42, 45 and 60. This configuration uses two single mode non-polarization m~int~ining (SM) fiber optic couplers 66 and 67. IOC 65 has no Y junction splitter like Y junction 32 of IOC 14 of configuration 90. Source 16 . .. , .. . . , . .. , ~ . , . .. . ~ , .... .
CA 022~8628 1998-12-16 WO 98/00682 10 PCTtUS97/11412 is a laser diode that emits 0.83 micron broad band light which goes to coupler 66 via port 68. Source 16 may be a fiber light source of another wavelength rather than that of a laser diode. Between source 16 and port 68 may be a piece of polarization m~int~ining (PM) fiber 103 connected to port 68 at connection 104 and to a PM pigtail 105 having polarization or birefringent axes aligned 45 degrees at splice 106. Tn~te~cl7 fiber 103 may be coupled directly to source 16 with its axes aligned at 45 degrees to the direction of polarization of the light from source 16. Fiber 103 and splice 106 are not necess:lry but p~ ed with a laser diode source. Fiber 103 and splice 106 are not used when source 16 is a fiber light source em~n~tin~ unpolarized light.
1 0 To achieve equal detected optical power from each of sensing coils 42, 45 and 60, the splitting ratio of first directional coupler 66 is chosen ~lol,liately. In the ideal case where each of directional couplers 66 and 67 are loss-less and each of the three coils 42, 45 and 60 are equally efficient, the splitting ratio of 33/67 at coupler 66 and 50/50 for coupler 67, produces or results in an equal optical power from each sensor. If 1 5 couplers 66 and 67 have losses, the light making additional passes through the respective coupling region will suffer additional attenuation. Thus. the splitting ratio of coupler 66 needs to be different to compensate for this extra loss and still keep the power at detector 69 the sarne for each of the three axes incorporating optical fiber loops 42, 45 and 60. One example of this is the use of a 30/70 instead of a 33/67 splitting 2 0 ratio for coupler 66 to account for the loss occurred in couplers 66 and 67.
Light for the first loop 42 leaves source 16 and goes through pigtail 105, splice 106, fiber 103, splice 104, and port 68 of coupler 66. Approximately 70 percent portion of that light from port 68 is split off into port 71 which goes to port 72 of coupler 67 via splice 73. Fifty percent of the light in port 72 goes to port 74 of coupler 67 and on 2 5 through a piece of PM fiber 107 connected to port 74 at connection 108, and splice 75 which cormects PM fiber 107 to a PM pigtail fiber 76 with a 45 degree alignment of the axes of fibers 107 and 76. The length of fiber 76 is at least twice that of fiber 107.
Light goes through pigtail 76 on through connection point 77 into waveguide 78. The depolarizer could instead include just PM fiber 76 having a 45 degree axis alignrnent 3 0 with waveguide 78 at connection 77. The beat length of fiber 76 would be less than one-half of the beat length of waveguide 78. The light goes through junction 36 through the components of the gyroscope having loop 42. The light returns after CA 022~8628 1998-12-16 counterprop~g~tin~ through loop 42 back through waveguide 78, connection point 77, pigtail 76, splice 75, fiber 107 and splice 108, or alternatively just through 45 degree connection 77 and fiber 76, on into port or fiber 74. How the light moves through the components associated with loop 42 is described above with respect to configuration 90.
Light coming back through port 74 of coupler 67 is split 50/50 and half that light goes to port 79 which is pigtailed to detector 69 wherein the light is converted into electrical equivalents of the light signals. The light returns from loop 42 going through port 74 of coupler 67, and the other portion of the light goes through port or fiber 72 through splice 73 and port or fiber 71 of coupler 66. A portion of that light continues on 1 0 through coupler 66 to port 81 and to either a two-input (both port 81 and 79) detector 69 or a second detector 93 to be converted into representative electrical signals.
Light from source 16 for loop 45 goes through PM pigtail 105, 45 degree splice 106, PM fiber 103, splice 104, and port 68 of SM coupler 66 which is portioned off at 70 percent to port 71. The light from port 71 goes through splice 73 and on through 1 5 port 72 of coupler 67. Half of the light in port 72 goes to port 80, a piece of PM fiber 109 connected to port 80 at connection splice 110, and on through a 45 degree splice 82 through a PM pigtail 83 which is connected to IOC 65 at point 84. Splice 82 aligns the birefringent axes of PM fibers 83 and 109 at 45 degrees. The length of fiber 83 is at least twice that of fiber 109. The depolarizer could instead include just PM fiber 83 having a 45 degree axis ~lignment with waveguide 85 at connection 84. The beat length of fiber 83 would be less than one-half of the beat length of waveguide 85.
Light from connection 84 goes through waveguide 85 on to be split by Y
junction 34. The light travels through the components associated with loop 45 asdescribed above with respect to configuration 90. Light from junction 34, after 2 5 counterpropag~ting in loop 45, goes through waveguide 85, through connection point 84, pigtail fiber 83, splice 82, fiber 109, or alternatively just through 45 degree connection 84 and fiber 83, and through splice 110 on to port 80 of fiber optic coupler 67. A portion of the light in port 80 goes on to port 79 on to detector 69. The other portion of the light in port 80 goes through coupler 67 on to port 72 and through splice 3 0 73 and port 71. A portion of light in port 71 goes on to port 81 of coupler 66 and to either a two fiber input (port 79 and 81) detector 69 or a second detector 93. The CA 022~8628 1998-12-16 WO 98mo682 -12- PCT/US97/11412 received light at detector 69 and detector 93 is converted into electrical signals representative of the received optical signals.
The third axis rotation rate sensor inco,~ol~li"g loop 60, involves light from source 16 going through pigtail 105, splice 106, fiber 103, splice 104, port 68 and coupler 66 of which 30 percent goes on into port or fiber 86. A piece of PM fiber 111 is connected to port 86 at splice 112. Fiber 111 is cormected to PM pigtail 52 at splice 51 with axes of fiber 111 and pigtail 52 aligned with each other at 45 degrees. Fiber 52 has a length at least twice that of fiber 111. The light from port 86 goes on through splice 112, fiber 111, and splice 51. The depolarizer could instead include just PM fiber 52 1 0 having a 45 degree axis alignment with waveguide 53 at connection 54. The beat length of fiber 52 would be less than one-half of the beat length of waveguide 53.
Light coming through a 45 degree splice 51 on to pigtail 52 which is connected at connection 54 to IOC 65, continues on through waveguide 53. The propagation of light on into loop 60 is described above with respect to configuration 10. The light 1 5 counterpropag~ting in loop 60 is combined at waveguide junction 55 and returns through waveguide 53, connection point 54, pigtail 52, splice 51, fiber l l l, or alternatively just through 45 degree connection 54 and fiber 52, splice 112, and on into port 86 of coupler 66. 70 percent of the l~lulllhlg light in port 86 is coupled onto port 81 of coupler 66. The light in port 81 goes on to the second input of a two-input (ports 2 0 79 and 81) detector 69 or, alternatively, to a second detector 93 which converts the light into electrical signals representative of the optical signals in port 81.
Figure 4b shows a variation of configuration 120 in figure 4a. Y junctions 34, 36 and 55 are replaced with directional couplers 149, 148 and 150, respectively.Couplers 149, 148 and 150 are preferably PM couplers; although they could be SM
2 5 couplers resulting in a FOG having lower p~lrollllance capabilitites. Polarizers 145, 146 and 147 are placed in optical fiber light paths between couplers 67 and 66, source 16 and couplers 148, 149 and 150, respectively. Electrooptic phase modulators 44, 50 and 61 are replaced with optical fiber piezoelectric phase modulators 151, 152 and 153, l~e~ ely. The IOC 65 waveguides functioning as light paths are replaced with 3 0 optical fiber light paths.
Configurations 10, 90, 100 and 120 of figures 1, 2, 3 and 4, respectively, have a FOG procec~ing electronics 113. Processing electronics 113 outputs a rotation rate CA 022~8628 1998-12-16 WO 98/00682 ~3 PCT/US97/11412 signal to indicator 114. Proces~in~ e}ectronics 113 may be an open-loop or a closed-~ Ioop design. Figures 5 and 6 reveal two versions, serrodyne 115 and dual ramp 116, respectively, of closed-loop electronics 113. The output of detector 63 of figures 1 and 2 goes to an input of amplifier 117 which may be a one-input arnplifier instead of a two-input ~ itlg arnplifier. Outputs of detectors 69 and 93, in figures 3 and 4, go to the two inputs of :j--l-----it-g arnplifier 117 of figures 5 or 6. The outputs of detectors 69 and 93 may be connecte~l to each other and inputted into a one-input amplifier 117 instead, as shown in figure 7, for any of the two-clet~ctor configurations. The output amplifier 117 goes to analog-to-digital (A/D) converter 118, for connecting the analog electrical 1 0 signals representing the light signals from the respective loops 42, 45 and 60, which have a particular phase relationship representing a rate of rotation of the le~l,e~ e loop.
Outputs of A/D converter 11 ~ go to a digital synchronous demodulator 119 and a bias frequency generator and control logic 121 of a three-axis gyroscope digital processing application specified integrated circuit (ASIC) for a serrodyne circuit 115 and a dual 1 5 ramp circuit 116, respectively. An oscillator 122 provides a frequency reference signal to bias fre~uency generator and control logic 121, which in turn outputs a frequency signal to demodulator 119, and a bias modulation signal and an enable axis signal for serrodyne generators 123, 124 and 125 of ASIC 115, and for dual rarnp and bias generators 126, 127 and 128 of ASIC 116, for x, y and z axes, respectively.
In figure 5, each serrodyne generator 123, 124, 125 for the x-, y- and z-axes, respectively, has the output signal, which is a processed detector 69, 93, signal that is multiplexed for each axis generator from demodulator l l 9 going to an input of an axis accumulator 129 which outputs a signal to inputs of a serrodyne numerical control oscillator 130 and a rate clock numerical control oscillator 131. The outputs of2 5 oscillators 130 and 131 to inputs of counter 132 and logic circuit 133. Logic circuit 133 provides up-and-down clock signals and counter 132 provides a rotation rate dependent digital phase nulling signal to a respective axis channel of a triple digital-to-analog converter (DAC) 134. Converter 134 outputs analog phase nulling signals to driver amplifiers 135, 136, 137 for x-, y- and z- axes, respectively. The serrodyne outputs from arnplifiers 135, 136 and 137 go to modulators 50, 44 and 61 of loops 45, 42 and 60, respectively, to null out the phase dirr~,rences of counterpropag~ting light beams of the loops, caused by the Sagnac effect due to rotation of the respective loops. The .. . .
CA 022~8628 1998-12-16 WO 98/00682 -14- PCTrUS97/11412 serrodyne outputs indicate the rotation rates and are input to a rotation rate indieator ~ and/orprocessor 114.
In figure 6, eaeh dual ramp and bias generator 126,127 and 128, of elosed-loop ASIC 116, has an axis aeeumulator 138 that reeeives a signal from demodulator 119, whieh is a proeessed deteetor 69, 93, signal that is multiplexed for eaeh axis generator, respeetively, and outputs a signal to a dual ramp aec.~ tQr 139 and a rate eloeknumerical eontrol oseillator 140. The output of dual ramp aeeumulator goes to an add-bias eireuit 141 and the output of oseillator 140 goes to logic circuit 142. Logic circuit 142 provides up-and-down cloek signals and add-bias eireuit 141 provides dual ramp digital phase nulling signals to a respective axis channel of triple digital-to-analog eonverter 134. DAC 134 outputs dual ramp analog phase nulling signals to drive arnplifiers 135,136,137 for x-, y-, and z-axes, respectively. The dual ramp outputs from amplifiers 135,136 and 137 go to modulators 50, 44 and 61 of loops 45, 42 and 60, respectively, to null out the phase differences of eount~ op~g~ting light beams of the loops, caused by the Sagnac effect due to rotation of the respective loops. The dual ramp outputs indicate the rotation rates and are input to a rotation rate indicator and/or processor 1 14.
Figure 7 differs from figure 6, besides having a one-input amplifier 117, has three digital synchronous demodulators 1 19, that is, one demodulator 1 19 providing a 2 0 processed detector 69,93, output signal for each dual ramp and bias generator 126,127, 128, of x-, y- and z-axes, respectively. Since each generator has its own demodulator 1 19, the processed detector signals to the generators are not multiplexed. The eonfiguration of figure 7 is applicable to the serrodyne generator configuration of figure S, also.
2 ~ Figure 8 shows a configuration 170 that is similar to configuration 90 of figure 2, exeept that depolarizers 48,49,41,43,58 and 59, and sensing coils 45,42 and 60 are absent. Sensing coils 161,162 and 163 are constructed from polarization m;~ it~gfiber. Figure 9 shows a configuration 180 that is similar to configuration 100 of figure 3a, except that depolarizers 48,49,41,43,58 and S9, and sensing coils 45,42 and 60 are absent. Sensing coils 161,162 and 163 are constructed from polarization ;nil~g fiber. Polarization ~ ing sensing coils 161,162 and 163, witout depolarizers in the coils, may similarly be implemented in configurations 10, 100 and ~ 120 of figures 1, 3b, 4a and 4b.
Other variants of the invention, other than the embo~iment.c disclosed here, maybe implemented.
BACKGROUND OF THE INVENTION
Typical inertial me~u.~;.,lent units have three g~,osco))es. A fiber optic inertial measurement system involves at least three fiber optic gyroscopes. Separate gyroscopes for each of the three axes involves a duplication of optical and electronic circuits.
SUMMARY OF THE INVENTION
The present invention is a three-axis fiber optic gyroscope that is a~plu~l;ate for an inertial measurement unit. The gyroscope measures rates of rotation for each of the three orthogonal axes. The three-axis fiber optic gyroscope of the present invention uses fewer optical and electronic components while still efficiently delivering sufficient optical power from a source through each gyroscope to the detector. A single source, one or two detectors, one preamplifier and two directional couplers are used outside the three interferometers. In contrast, the same task performed by the standard approach in the art uses three single axis gyros that require three sources, three detectors, three preamplifiers and three directional couplers. The electronics for the gyroscopes may be open loop or closed loop. Serrodyne, digital phase step and dual ramp electronics are options for a closed loop configuration. The interferometer or gyroscope for each axis of a three axis system can deliver nearly the same amount of power to the detector as a single axis configuration.
Figure 1 shows the optical configuration for the three axis gyroscope having onepolarization mz,i.ll~;-,ing coupler and four Y junctions.
Figure 2 shows the optical configuration for the three axis gyroscope having onenon-polarization m ~int~ining coupler and four Y junctions.
Figure 3a shows a three axis gyroscope having two polarization m~int~ining couplers and three Y junctions.
Figure 3b reveals a three axis gyroscope having two polarization m ~in~ining couplers, and three couplers at the sensing loops.
Figure 4a shows a three axis gyroscope having two non-polarization m ~int~ining 3 0 couplers and three Y junctions.
Figure 4b reveals a three axis gyroscope having two non-polarization m~ inil~g couplers, and three couplers at the sensing loops.
CA 022~8628 1998-12-16 Figure 5 shows an example of closed loop serrodyne electronics.
Figure 6 shows an example of dual ramp closed loop electronics.
Figure 7 shows the dual ramp closed loop electronics having a demodulator for each axis.
Figure 8 reveals an optical configuration for the three axis gyroscope having one non-polarization m~ g coupler and four Y junctions, and being without depolarizers at the sensing loops.
Figure 9 reveals a three axis gyroscope having two polarization m~ ,g couplers and three Y junctions, and being without depolarizers at the sensing loops.
Figure I shows a configuration 10 for a three axis fiber optic gyroscope (FOG) having one polarization m~int~ining (PM) fiber coupler 12 and an integrated optical circuit (IOC) 14 with four Y junctions 32, 34, 36 and SS. Coupler 12 is a coupler fabricated from PM fiber Light source 16 emits broad band light having a middle 1 5 wavelength of 0.83 microns. Light source 16 may be at some other wavelength. The light enters coupler 12 via fiber or port 18 and the light goes through coupler 12 wherein about half the light goes out on port or fiber 20 and the other half the light goes out on port or fiber 22, under the assumption that there is no light loss in coupler 12.
In this embodiment, coupler 12 is designed for 0.83 micron light. Fiber 20 is 2 0 connected to pigtail 13 of waveguide 28 via splice 11, of integrated optical circuit (IOC) 14 with aligned axes at splice 11 and connection 30. IOC 14 may be a proton exchange or titanium indiffused lithium niobate device. Also, IOC 14 may be fabricated from other materials such as silicon, tantalum, polymers and so on. The proton exchange device has polarizing waveguides 28, 38, 40, 46, 47, 53, 56, and 57. If IOC 14 is a 2 5 titanium indiffused device, then the IOC has a conductive sheath on it and over the waveguides thereby causing the respective waveguides to be pol~ri7ing.
The light is split 50/50 at Y junction 32 such that one half of the light to junction 32 goes to junction 34 and the other half of the light as a result of the split by junction 32 goes to junction 36. This ratio of light is with the assumption that there is little or no 3 0 loss of light at the junctions or in the waveguides of IOC 14. The other half of the light that enters junction 36 is split in half such that light propagates down light waveguides 38 and 40. Light in waveguide 38 propagates through connection 64, depolarizer 41 CA 022~8628 1998-12-16 and through loop 42 and on back through depolarizer 43, connection 64 and down waveguide 40. Light passing through waveguide 40 is subject to modulation by modulator 44. Light propag~in~ toward loop 42 down waveguide 40 goes through depolarizer 43 and through the loop 42 and back out of loop 42 and through depolarizer 41 and down through waveguide 38 0f IOC 14. The ~ g beams of light are combined from waveguides 38 and 40 at Y junction 36 and move towards junction 32.
Depolarizers 41 and 43 may be constructed in various ways. For in~t~nce~ in depolarizer 41, a PM fiber 154 is ~tt~checl to IOC 14 at point 64, with its birefringent axes aligned with the birefringent axes of waveguide 38. Fiber 154 may be a pigtail of 1 0 IOC 14. Another PM fiber 156 is spliced to fiber 154, with the birefringent axes of fibers 154 and 156 aligned at about 45 degrees relative to each other, at connection point 155. Fiber 156 is spliced to single mode non-polarization m;~ t;~ ;r.g fiber of coil 42 at connection 157. Fiber 156 is typically more than twice the length as fiber 154.
On the other hand, depolarizer 41 may have only one PM fiber 154 which has birefringent axes aligned at about 45 degrees relative to the axes of waveguide 38, at pigtail 64. Fiber 154 is then spliced to coil 42 at connection point 157. The beat length of fiber 154 is more than twice the beat length of waveguide 38. Splice 155 and fiber 156 are not needed in this depolarizer configuration.
Depolarizer 43 may be used in conjunction with depolarizer 41 or it may be 2 0 absent, thereby resulting in only one depolarizer 41 for coil 42. However, both depolarizers 41 and 43 result in better FOG perforrnance.
If depolarizer 43 is to be used it has the same structure as depolarizer 41 except that the length of fiber 158 is slightly different in length than that of fiber 154 and that the length of fiber 159 is more than four times the length of fiber 158, although fiber 2 5 159 may be more than twice the length of fiber 156.
ln the depolarizer 41 configuration having just the one PM fiber 154 with axes aligned with waveguide 38 axes, a similarly structured depolarizer 43 may or not be incorporated. If depolarizer 43 is incorporated, then the structure of the depolarizer may be that of two PM fibers 158 and 159, with fiber 159 having more than twice the beat 3 0 length of fiber 154 in the depolarizer configuration where fiber 154 axes are aligned at 45 degrees relative to waveguide axes at connection point 64. Depolarizer 43, inconjunction with either depolarizer 41 configuration, may have only fiber 158 which has CA 022~8628 1998-12-16 its birefringent axes aligned at 45 degrees relative to the axes of waveguide 40 at pigtail ~ 64. Fiber 158 in the latter structure, without splice 155 and fiber 159, has a beat length that is more than twice the beat length of waveguide 40, or it may have more than four times the beat length of waveguide 40 if depolarizer 41 has the same kind of ~ c as the latter depolarizer 43.
Depolarizers 48 and 49 have similar structure combinations as depolarizers 41 and 43, respectively. Likewise depolarizers 58 and 59 have similar structure combinations as depolarizers 41 and 43, respectively. The structures of depolarizers noted here are applicable to all figures having depolarizers 41, 43, 48, 49, 56 and 59.
1 0 A light from junction 34 is split and light beams propagate down waveguides 46 and 47 on through connection 64 and depolarizers 48 and 49, respectively, and counterpropagate through loop 45 and return through depolarizers 49 and 48, and connection 64 respectively. A light that passes either way through waveguide 47 is subject to modulation by modulator 50. The returning light beams from loop 45 via 1 5 waveguides 46 and 47 are combined at junction 34 and the resultant light goes on to junction 32 which is combined with light from junction 36. The combined light goes down waveguide 28, through connection 30 and into fiber or port 20 of coupler 12.
The other portion of the light from source 16 in coupler 12 goes through fiber or port 22 on to waveguide 53 of IOC 14 via splice 15, pigtail 17 and connection 54 with aligned axes at splice 15 and connection 54. Light going through waveguide 53 is split at Y junction 55 into wherein half the light goes down waveguide 56 and the other half the light from waveguide 53 goes through waveguide 57. The light goes through depolarizers 58 and 59 from waveguides 56 and 57, respectively. The light waves or beams counterpropagate through loop 60 and retD through depolarizers 59 and 58 and go through waveguides 57 and 56, respectively, to be combined at Y junction 55. Light prop~g~tin~ through waveguide 57 may be modulated by modulator 61. The combined light from junction 55 propagates down waveguide 53, through connection 54 and into port or fiber 22 of coupler 12. About half the light from port 20 goes into port or fiber 62 and half the light from port 22 is combined with the light from port 20 and goes 3 0 down port 62 into detector 63.
The light from port 62 constitutes interferences of pairs of beams of loops 42, 45 and 60. Detector 63 electrically converts the light beams and their respective CA 022~8628 1998-12-16 interferences into electrical signals which are deciphered into rate of rotationinformation of loops 42, 45 and 60. IOC 14 is designed for 0.83 micron wavelength of source light. The depolarizers which may be made of PM fiber are aligned respectively to waveguides of IOC 14 at a 45 degree angle (+/- 2 degrees) between the polarization axes of each PM fiber and the re~ecli~e waveguide of IOC 14. The resultant depolarizers are designed for 0.83 micron of light.
The fiber for coils 42, 45 and 60 is single mode fiber, that is, it is non-polarization maintaining fiber, and is de~igned for a wavelength of 1.3 microns of light.
The depolarizers 48, 49, 41, 43, 58 and 59 are spliced to the single mode fiber of the 1 0 respective loops.
Figure 2 shows a configuration 90 for a three axis fiber optic gyroscope (FOG) having one single-mode fiber coupler 12 and an integrated optical circuit (IOC) 14 with three Y junctions 34, 36, 55. Coupler 12 is a coupler fabricated from single mode non-polarization m~int~ining (SM) fiber. Light source 16, which is a laser diode, emits 1 5 broad band light having a middle wavelength of 0.83 microns. Light source 16 may instead be a fiber optic light source of another wavelength.
There may be a polarization m~ g (PM) fiber 94 spliced onto port 18 of coupler 12 at point 95. PM fiber 94 axes are aligned at 45 degrees relative to the source 16 PM pigtail 96 axes at splice 97. lnstead, fiber 94 may be aligned at 45 degrees at 2 0 source 16 itself relative to the axis of the polarized light. The combination of fibers 94 and 96~ and splice 97 is not required but is desired for use with SM coupler 12. The fiber 94 and 96 and splice 97 combination is not used with a non-polarized fiber light source, which emits non-polarized light, as source 16.
The light enters coupler 12 via fiber or port 18 and the light goes through 2S coupler 12 wherein about half the light goes through port or fiber 20 and the other half the light goes through port or fiber 22, under the assumption that there is no light loss in coupler 12. Fiber coupler 12 is designed for 0.83 micron light. Fiber 20 at point 99 is spliced to a piece of PM fiber 98. PM fiber 98 is connected to a PM pigtail 24 at a 45 degree-axis aligned splice 26. Fiber 24 has a length that is at least twice the length of 3 0 fiber 98. Fiber pigtail 24 is attached to waveguide 28 at point 30 with aligned axes.
The depolarizer could instead include just PM fiber 24 having a 45 degree axis ~ignment with waveguide 28 at connection 30. The beat length of fiber 24 would be CA 022~8628 1998-12-16 WO 9~,~3~ 6 PCT/US97/11412 less than one-half of the beat length of waveguide 28. The light is split 50150 at Y
junction 32 such that one half of the light to junction 32 goes to junction 34 and the other half of the light as a result of the split by junction 32 goes to junction 36. The 50/50 ratio of light is based on the as~ .ylion that there is little or no loss of light at the 5 junction or in the waveguides of IOC 14. The light that enters junction 36 is split in half such that each half portion of the light propagates down light waveguides 38 and 40 respectively. Light in waveguide 38 propagates through connection 64, depolarizer 41 and through loop 42 and on back through depolarizer 43, connection 64 and down waveguide 40. Light passing through waveguide 40 is subject to modulation by 1 0 modulator 44.
Light prop;~g~ting toward loop 42 down waveguide 40 goes through depolarizer 43 and through loop 42 and back out of loop 42 and through depolarizer 41 and down through waveguide 38 of IOC 14. The returning beams of light are combined from waveguides 38 and 40, at Y junction 36 and moves towards junction 32.
1 5 A light from junction 34 is split and light beams propagate down waveguides 46 and 47 on through depolarizers 48 and 49, respectively, and counterpropagate through loop 45 and return through depolarizers 49 and 48, respectively. A light that passes either way through waveguide 47 is subject to modulation by modulator 50. The returning light from loop 45 via waveguides 46 and 47 is combined at junction 34 and 2 0 the resultant light goes on to junction 32 which is combined with light from junction 36.
The combined light goes down waveguide 28, through connection point 30 and through PM pigtail fiber 24, splice 26, PM fiber 98, and splice 99, respe~;lively, or alternatively just through 45 degree connection 30 and PM fiber 24, into fiber or port 20 of coupler 12.
2 5 The other portion of the light from source 16 goes through fiber or port 22 spliced at point 101 to a piece of PM fiber 102 which is at a 45 degree axis splice 51 connected to a PM pigtail or fiber 52. The length of fiber 52 is at least twice that of fiber 102. Fiber 52 is connected with aligned axes to waveguide 53 of IOC 14 at point 54. The depolarizer could instead include just PM fiber 52 having a 45 degree axis 3 0 alignrnent with waveguide 53 at cormection 54. The beat length of fiber 52 would be less than one-half of the beat length of waveguide 53. Light going through waveguide 53 is split at Y junction 55 into wherein halfthe light goes down waveguide 56 and the CA 022~8628 1998-12-16 other half the light from waveguide 53 goes through waveguide 57. The light goesthrough depolarizers 58 and 59 from waveguides 56 and 57, respectively. The light waves or beams cou~ opagate through loop 60 and return through depolarizers 59 and 58 and go through waveguides 57 and 56, les~e~ ely, to be combined at Y
5 junction 55. Light prop~ting through waveguide 57 may be mod~ tecl by modulator 61. The combined light from junction 55 propagates down waveguide 53, through point 54~ pigtail 52, splice 51, fiber 102, and splice 101, or alternatively just through 45 degree connection 54 and PM fiber 52, into port or fiber 22 of coupler 12. About half the light from port 20 goes into port or fiber 62 and half the light from port 22 is 1 0 combined with the light from port 20 and goes down port 62 on into detector 63. The light from port 62 constitutes interferences of pairs of beams of loops 42, 45 and 60.
Detector 63 electrically converts the light beams and their respective interferences into electrical signals which are deciphered into rate of rotation information of loops 42, 45 and 60.
IOC 14 is designed for 0.83 micron wavelength of source light. The depolarizers which may be made of PM fiber that is aligned respectively to waveguides of IOC 14 at a 45 degree angle (+/- 2 degrees) with respect to the polarization axis of the fiber of the depolarizer and the waveguide of IOC 14. The polarizers are designed for 0.83 micron of light. The fiber for coils 42, 45 and 60 is single mode fiber, that is, it 2 0 is non-polarization m~int~ining fiber, and is designed for a wavelength of 1.3 microns of light. Depolarizers 48, 49, 41, 43, 58 and 59 are of 0.83 micron PM fiber which is spliced to the single mode fiber of the respective loops and to IOC 14 at points 64 to the respective waveguides.
Configuration 100 of figure 3a involves an IOC 65 which may be split up into 2 5 three separate IOCs having junctions 34, 36 and 55, respectively, for each of the FOG
loops 45, 42 and 60. IOC 65 may have the same material and functional characteristics as IOC 14. IOC 14 and IOC 65 are preferred to have polarizing waveguides, although the waveguides may be polarization m~ i"ing or non polarization m~int~ining.
Configuration 100 uses two PM fiber optic couplers 66 and 67. IOC 65 has no Y junction splitter like Y junction 32 Of IOC 14 Of configuration 10. Source 16 is a laser diode and emits 0.83 micron broad band light which goes to coupler 66 via pigtail 91, splice 92 and port 68. Splice 92 is optional. To achieve equal detected optical CA 022~8628 1998-12-16 WO 98t00682 8 PCT/US97/11412 power from each of sensing coils 42, 45 and 60, the splitting ratio of first directional ~ coupler 66 is chosen al,lulu~l;ately. In the ideal case where each of directional couplers 66 and 67 are loss-less and each of the three coils 42, 45 and 60 are equally efficient, the splitting ratio of 33/67 at coupler 66 and S0/50 for coupler 67, produces or results in an 5 equal optical power from each sensor. If couplers 66 and 67 have losses, the light m:~king additional passes through the respective coupling region will suffer additional attenuation. Thus, the splitting ratio of coupler 66 needs to be di~le--t to compensate for this extra loss and still keep the power levels at detectors 69 and 93 the same for each of the three axes incorporating loops 42, 45 and 60. One example of this is the use 1 0 of a 30/70 instead of a 33/67 splitting ratio for coupler 66 to account for the loss occurred in couplers 66 and 67.
Light for the first loop 42 leaves source 16 and goes through port 68 of coupler66 and an approximately 70 percent portion of that light is split off into port 71 which goes to port 72 of coupler 67 via splice 73 with aligned axes. Fifty percent of the light 1 5 in port 72 goes to port 74 of coupler 67 and on through connection point 77, with aligned axes, into waveguide 78. The light goes through junction 36 through the colllpo~ of the gyroscope having loop 42.
The light returns after counterprop~g~ting through loop 42 back through waveguide 78, connection point 77, and on into port or fiber 74. How the light moves 2 0 through the components associated with loop 42 is described above with respect to configuration 10. Light coming back through port 74 of coupler 67 is split 50/50 and half that light goes to port 79 which is pigtailed to detector 69 thereby the light is being converted by detector 69 into electrical equivalents of the light signals. The light returns from loop 42 going through port 74 of coupler 67, and also the other portion of 2 5 the light goes through port or fiber 72 through aligned-axes splice 73 and port or fiber 71 of coupler 66. A portion of that light continues on through coupler 66 to port 81, and fiber 81 is either connected to detector 69 along with fiber 79, or to a second detector 93. to also be converted into representative electrical signals.
Light from source 16 for loop 45 goes through port 68 of coupler 66 which is portioned off at 70 percent to port 71. The light from port 71 goes through aligned-axes splice 73 and on through port 72 of coupler 67. Half of the light in port 72 goes to port 80 and on to IOC 65 at point 84. Point 84 is an aligned axis connection between port 80 CA 022~8628 1998-12-16 and waveguide 85, with or without splice 19 and pigtail 21. Similarly, light to or from ~ port 74 of coupler 67 and port 86 of coupler 66 may or may not go through splice 19 and pigtail 21. Light from point 84 goes through waveguide 85 on to be split by Y
junction 34. The light travels through the components associated with loop 45 as5 described above with respect to configuration 10. Light from junction 34, after countelprop~ting in loop 45, goes through waveguide 85, through point 84 on to port 80 of fiber optic coupler 67. A portion of the light in port 80 goes on to port 79 on to detector 69. The other portion of the light in port 80 goes through coupler 67 on to port 72 and through splice 73 and port 71. A portion of light in port 71 goes on to port 81 of 1 0 coupler 66 and to detector 69 or second detector 93. The received light at detector 69 or second detector 93 again is converted into electrical signals representative of the received optical signals.
The third axis rotation rate sensor incorporating loop 60, involves light from source 16 going through coupler 66 of which 30 percent goes on into port or fiber 86.
1 5 The light from port 86 goes on through point 54 to IOC 65, and continues on through waveguide 53. The propagation of light on into loop 60 is described above with respect to configuration 10. The light co~-tel~..,p~E;lting in loop 60 is combined at light junction 55 and returns through waveguide 53, point 54 and on into port 86 of coupler 66. 70 percent of the returning light in port 86 is coupled onto port 81 of coupler 66.
2 0 The light in port 81 goes on to detector 69 which converts the light into electrical signals representative of the optical signals in port 81.
Figure 3b shows a variation of configuration 100 in figure 3a. Y junctions 34, 36 and 55 are replaced with directional couplers 149, 14g and 150, respectively.Po}arizers 145, 146 and 147 are placed in optical fiber light paths between couplers 67 and 68, and couplers 148, 149 and 150, respectively. Electrooptic phase modulators 44, 50 and 61 are replaced with optical fiber piezoelectric phase modulators 151, 152 and 153, respectively. The IOC 65 waveguides functioning as light paths are replaced with optical fiber light paths.
Configuration 120 of figure 4a involves IOC 65 which may be split up into three 3 0 se~ ale IOCs for each of the FOG loops 42, 45 and 60. This configuration uses two single mode non-polarization m~int~ining (SM) fiber optic couplers 66 and 67. IOC 65 has no Y junction splitter like Y junction 32 of IOC 14 of configuration 90. Source 16 . .. , .. . . , . .. , ~ . , . .. . ~ , .... .
CA 022~8628 1998-12-16 WO 98/00682 10 PCTtUS97/11412 is a laser diode that emits 0.83 micron broad band light which goes to coupler 66 via port 68. Source 16 may be a fiber light source of another wavelength rather than that of a laser diode. Between source 16 and port 68 may be a piece of polarization m~int~ining (PM) fiber 103 connected to port 68 at connection 104 and to a PM pigtail 105 having polarization or birefringent axes aligned 45 degrees at splice 106. Tn~te~cl7 fiber 103 may be coupled directly to source 16 with its axes aligned at 45 degrees to the direction of polarization of the light from source 16. Fiber 103 and splice 106 are not necess:lry but p~ ed with a laser diode source. Fiber 103 and splice 106 are not used when source 16 is a fiber light source em~n~tin~ unpolarized light.
1 0 To achieve equal detected optical power from each of sensing coils 42, 45 and 60, the splitting ratio of first directional coupler 66 is chosen ~lol,liately. In the ideal case where each of directional couplers 66 and 67 are loss-less and each of the three coils 42, 45 and 60 are equally efficient, the splitting ratio of 33/67 at coupler 66 and 50/50 for coupler 67, produces or results in an equal optical power from each sensor. If 1 5 couplers 66 and 67 have losses, the light making additional passes through the respective coupling region will suffer additional attenuation. Thus. the splitting ratio of coupler 66 needs to be different to compensate for this extra loss and still keep the power at detector 69 the sarne for each of the three axes incorporating optical fiber loops 42, 45 and 60. One example of this is the use of a 30/70 instead of a 33/67 splitting 2 0 ratio for coupler 66 to account for the loss occurred in couplers 66 and 67.
Light for the first loop 42 leaves source 16 and goes through pigtail 105, splice 106, fiber 103, splice 104, and port 68 of coupler 66. Approximately 70 percent portion of that light from port 68 is split off into port 71 which goes to port 72 of coupler 67 via splice 73. Fifty percent of the light in port 72 goes to port 74 of coupler 67 and on 2 5 through a piece of PM fiber 107 connected to port 74 at connection 108, and splice 75 which cormects PM fiber 107 to a PM pigtail fiber 76 with a 45 degree alignment of the axes of fibers 107 and 76. The length of fiber 76 is at least twice that of fiber 107.
Light goes through pigtail 76 on through connection point 77 into waveguide 78. The depolarizer could instead include just PM fiber 76 having a 45 degree axis alignrnent 3 0 with waveguide 78 at connection 77. The beat length of fiber 76 would be less than one-half of the beat length of waveguide 78. The light goes through junction 36 through the components of the gyroscope having loop 42. The light returns after CA 022~8628 1998-12-16 counterprop~g~tin~ through loop 42 back through waveguide 78, connection point 77, pigtail 76, splice 75, fiber 107 and splice 108, or alternatively just through 45 degree connection 77 and fiber 76, on into port or fiber 74. How the light moves through the components associated with loop 42 is described above with respect to configuration 90.
Light coming back through port 74 of coupler 67 is split 50/50 and half that light goes to port 79 which is pigtailed to detector 69 wherein the light is converted into electrical equivalents of the light signals. The light returns from loop 42 going through port 74 of coupler 67, and the other portion of the light goes through port or fiber 72 through splice 73 and port or fiber 71 of coupler 66. A portion of that light continues on 1 0 through coupler 66 to port 81 and to either a two-input (both port 81 and 79) detector 69 or a second detector 93 to be converted into representative electrical signals.
Light from source 16 for loop 45 goes through PM pigtail 105, 45 degree splice 106, PM fiber 103, splice 104, and port 68 of SM coupler 66 which is portioned off at 70 percent to port 71. The light from port 71 goes through splice 73 and on through 1 5 port 72 of coupler 67. Half of the light in port 72 goes to port 80, a piece of PM fiber 109 connected to port 80 at connection splice 110, and on through a 45 degree splice 82 through a PM pigtail 83 which is connected to IOC 65 at point 84. Splice 82 aligns the birefringent axes of PM fibers 83 and 109 at 45 degrees. The length of fiber 83 is at least twice that of fiber 109. The depolarizer could instead include just PM fiber 83 having a 45 degree axis ~lignment with waveguide 85 at connection 84. The beat length of fiber 83 would be less than one-half of the beat length of waveguide 85.
Light from connection 84 goes through waveguide 85 on to be split by Y
junction 34. The light travels through the components associated with loop 45 asdescribed above with respect to configuration 90. Light from junction 34, after 2 5 counterpropag~ting in loop 45, goes through waveguide 85, through connection point 84, pigtail fiber 83, splice 82, fiber 109, or alternatively just through 45 degree connection 84 and fiber 83, and through splice 110 on to port 80 of fiber optic coupler 67. A portion of the light in port 80 goes on to port 79 on to detector 69. The other portion of the light in port 80 goes through coupler 67 on to port 72 and through splice 3 0 73 and port 71. A portion of light in port 71 goes on to port 81 of coupler 66 and to either a two fiber input (port 79 and 81) detector 69 or a second detector 93. The CA 022~8628 1998-12-16 WO 98mo682 -12- PCT/US97/11412 received light at detector 69 and detector 93 is converted into electrical signals representative of the received optical signals.
The third axis rotation rate sensor inco,~ol~li"g loop 60, involves light from source 16 going through pigtail 105, splice 106, fiber 103, splice 104, port 68 and coupler 66 of which 30 percent goes on into port or fiber 86. A piece of PM fiber 111 is connected to port 86 at splice 112. Fiber 111 is cormected to PM pigtail 52 at splice 51 with axes of fiber 111 and pigtail 52 aligned with each other at 45 degrees. Fiber 52 has a length at least twice that of fiber 111. The light from port 86 goes on through splice 112, fiber 111, and splice 51. The depolarizer could instead include just PM fiber 52 1 0 having a 45 degree axis alignment with waveguide 53 at connection 54. The beat length of fiber 52 would be less than one-half of the beat length of waveguide 53.
Light coming through a 45 degree splice 51 on to pigtail 52 which is connected at connection 54 to IOC 65, continues on through waveguide 53. The propagation of light on into loop 60 is described above with respect to configuration 10. The light 1 5 counterpropag~ting in loop 60 is combined at waveguide junction 55 and returns through waveguide 53, connection point 54, pigtail 52, splice 51, fiber l l l, or alternatively just through 45 degree connection 54 and fiber 52, splice 112, and on into port 86 of coupler 66. 70 percent of the l~lulllhlg light in port 86 is coupled onto port 81 of coupler 66. The light in port 81 goes on to the second input of a two-input (ports 2 0 79 and 81) detector 69 or, alternatively, to a second detector 93 which converts the light into electrical signals representative of the optical signals in port 81.
Figure 4b shows a variation of configuration 120 in figure 4a. Y junctions 34, 36 and 55 are replaced with directional couplers 149, 148 and 150, respectively.Couplers 149, 148 and 150 are preferably PM couplers; although they could be SM
2 5 couplers resulting in a FOG having lower p~lrollllance capabilitites. Polarizers 145, 146 and 147 are placed in optical fiber light paths between couplers 67 and 66, source 16 and couplers 148, 149 and 150, respectively. Electrooptic phase modulators 44, 50 and 61 are replaced with optical fiber piezoelectric phase modulators 151, 152 and 153, l~e~ ely. The IOC 65 waveguides functioning as light paths are replaced with 3 0 optical fiber light paths.
Configurations 10, 90, 100 and 120 of figures 1, 2, 3 and 4, respectively, have a FOG procec~ing electronics 113. Processing electronics 113 outputs a rotation rate CA 022~8628 1998-12-16 WO 98/00682 ~3 PCT/US97/11412 signal to indicator 114. Proces~in~ e}ectronics 113 may be an open-loop or a closed-~ Ioop design. Figures 5 and 6 reveal two versions, serrodyne 115 and dual ramp 116, respectively, of closed-loop electronics 113. The output of detector 63 of figures 1 and 2 goes to an input of amplifier 117 which may be a one-input arnplifier instead of a two-input ~ itlg arnplifier. Outputs of detectors 69 and 93, in figures 3 and 4, go to the two inputs of :j--l-----it-g arnplifier 117 of figures 5 or 6. The outputs of detectors 69 and 93 may be connecte~l to each other and inputted into a one-input amplifier 117 instead, as shown in figure 7, for any of the two-clet~ctor configurations. The output amplifier 117 goes to analog-to-digital (A/D) converter 118, for connecting the analog electrical 1 0 signals representing the light signals from the respective loops 42, 45 and 60, which have a particular phase relationship representing a rate of rotation of the le~l,e~ e loop.
Outputs of A/D converter 11 ~ go to a digital synchronous demodulator 119 and a bias frequency generator and control logic 121 of a three-axis gyroscope digital processing application specified integrated circuit (ASIC) for a serrodyne circuit 115 and a dual 1 5 ramp circuit 116, respectively. An oscillator 122 provides a frequency reference signal to bias fre~uency generator and control logic 121, which in turn outputs a frequency signal to demodulator 119, and a bias modulation signal and an enable axis signal for serrodyne generators 123, 124 and 125 of ASIC 115, and for dual rarnp and bias generators 126, 127 and 128 of ASIC 116, for x, y and z axes, respectively.
In figure 5, each serrodyne generator 123, 124, 125 for the x-, y- and z-axes, respectively, has the output signal, which is a processed detector 69, 93, signal that is multiplexed for each axis generator from demodulator l l 9 going to an input of an axis accumulator 129 which outputs a signal to inputs of a serrodyne numerical control oscillator 130 and a rate clock numerical control oscillator 131. The outputs of2 5 oscillators 130 and 131 to inputs of counter 132 and logic circuit 133. Logic circuit 133 provides up-and-down clock signals and counter 132 provides a rotation rate dependent digital phase nulling signal to a respective axis channel of a triple digital-to-analog converter (DAC) 134. Converter 134 outputs analog phase nulling signals to driver amplifiers 135, 136, 137 for x-, y- and z- axes, respectively. The serrodyne outputs from arnplifiers 135, 136 and 137 go to modulators 50, 44 and 61 of loops 45, 42 and 60, respectively, to null out the phase dirr~,rences of counterpropag~ting light beams of the loops, caused by the Sagnac effect due to rotation of the respective loops. The .. . .
CA 022~8628 1998-12-16 WO 98/00682 -14- PCTrUS97/11412 serrodyne outputs indicate the rotation rates and are input to a rotation rate indieator ~ and/orprocessor 114.
In figure 6, eaeh dual ramp and bias generator 126,127 and 128, of elosed-loop ASIC 116, has an axis aeeumulator 138 that reeeives a signal from demodulator 119, whieh is a proeessed deteetor 69, 93, signal that is multiplexed for eaeh axis generator, respeetively, and outputs a signal to a dual ramp aec.~ tQr 139 and a rate eloeknumerical eontrol oseillator 140. The output of dual ramp aeeumulator goes to an add-bias eireuit 141 and the output of oseillator 140 goes to logic circuit 142. Logic circuit 142 provides up-and-down cloek signals and add-bias eireuit 141 provides dual ramp digital phase nulling signals to a respective axis channel of triple digital-to-analog eonverter 134. DAC 134 outputs dual ramp analog phase nulling signals to drive arnplifiers 135,136,137 for x-, y-, and z-axes, respectively. The dual ramp outputs from amplifiers 135,136 and 137 go to modulators 50, 44 and 61 of loops 45, 42 and 60, respectively, to null out the phase differences of eount~ op~g~ting light beams of the loops, caused by the Sagnac effect due to rotation of the respective loops. The dual ramp outputs indicate the rotation rates and are input to a rotation rate indicator and/or processor 1 14.
Figure 7 differs from figure 6, besides having a one-input amplifier 117, has three digital synchronous demodulators 1 19, that is, one demodulator 1 19 providing a 2 0 processed detector 69,93, output signal for each dual ramp and bias generator 126,127, 128, of x-, y- and z-axes, respectively. Since each generator has its own demodulator 1 19, the processed detector signals to the generators are not multiplexed. The eonfiguration of figure 7 is applicable to the serrodyne generator configuration of figure S, also.
2 ~ Figure 8 shows a configuration 170 that is similar to configuration 90 of figure 2, exeept that depolarizers 48,49,41,43,58 and 59, and sensing coils 45,42 and 60 are absent. Sensing coils 161,162 and 163 are constructed from polarization m;~ it~gfiber. Figure 9 shows a configuration 180 that is similar to configuration 100 of figure 3a, except that depolarizers 48,49,41,43,58 and S9, and sensing coils 45,42 and 60 are absent. Sensing coils 161,162 and 163 are constructed from polarization ;nil~g fiber. Polarization ~ ing sensing coils 161,162 and 163, witout depolarizers in the coils, may similarly be implemented in configurations 10, 100 and ~ 120 of figures 1, 3b, 4a and 4b.
Other variants of the invention, other than the embo~iment.c disclosed here, maybe implemented.
Claims (21)
1. A three-axis fiber optic gyroscope comprising:
a coupler (12) having first (18), second (62), third (20) and fourth (22) ports;
a source (16) connected to the first port (18) of said coupler;
a detector (63) connected to the second port (62) of said coupler;
a first Y junction (32) having a first port connected to the third port (20) of said coupler (12), and having second and third ports;
a second Y junction (34) having a first port connected to the second port of said first Y junction (32), and having second and third ports;
a third Y junction (36) having a first port connected to the third port of said first Y junction (32), and having second and third ports;
a fourth Y junction (55) having a first port connected to the fourth port (22) of said coupler (12), and having second and third ports;
a first sensing loop (45) having at least one depolarizer (48, 49), and having first and second ends connected to the second and third ports, respectively, of said second Y junction (34);
a second sensing loop (42) having at least one depolarizer (41, 43), and having first and second ends connected to the second and third ports, respectively, of said third Y junction (36);
a third sensing loop (60) having at least one depolarizer (58, 59), having first and second ends connected to the second and third ports, respectively, of said fourth Y junction (55).
a coupler (12) having first (18), second (62), third (20) and fourth (22) ports;
a source (16) connected to the first port (18) of said coupler;
a detector (63) connected to the second port (62) of said coupler;
a first Y junction (32) having a first port connected to the third port (20) of said coupler (12), and having second and third ports;
a second Y junction (34) having a first port connected to the second port of said first Y junction (32), and having second and third ports;
a third Y junction (36) having a first port connected to the third port of said first Y junction (32), and having second and third ports;
a fourth Y junction (55) having a first port connected to the fourth port (22) of said coupler (12), and having second and third ports;
a first sensing loop (45) having at least one depolarizer (48, 49), and having first and second ends connected to the second and third ports, respectively, of said second Y junction (34);
a second sensing loop (42) having at least one depolarizer (41, 43), and having first and second ends connected to the second and third ports, respectively, of said third Y junction (36);
a third sensing loop (60) having at least one depolarizer (58, 59), having first and second ends connected to the second and third ports, respectively, of said fourth Y junction (55).
2. A three-axis fiber optic gyroscope comprising:
a first coupler (66) having first (68), second (81), third (71) and fourth (86) ports;
a source (61) connected to the first port (68) of said first coupler (66);
a detector (93) connected to the second port (81) of said first coupler (66);
a second coupler (67) having a first port (72) connected to the third port (71) of said first coupler, a second port (79) connected to a second detector (69), and having third (80) and fourth ports (74);
a first Y junction (34) having a first port connected to the third port (80) of said second coupler (67), and having second and third ports;
a second Y junction (36) having a first port connected to the fourth port (74) of said second coupler (67), and having second and third ports;
a third Y junction (55) having a first port connected to the fourth port (80) of said first coupler (66), and having second and third ports;
a first sensing loop (45) having first and second ends connected to the second and third ports, respectively, of said first Y junction (34);
a second sensing loop (42) having first and second ends connected to the second and third ports, respectively, of said second Y junction;
and a third sensing loop (60) having first and second ends connected to the second and third ports, respectively, of said third Y junction (55).
a first coupler (66) having first (68), second (81), third (71) and fourth (86) ports;
a source (61) connected to the first port (68) of said first coupler (66);
a detector (93) connected to the second port (81) of said first coupler (66);
a second coupler (67) having a first port (72) connected to the third port (71) of said first coupler, a second port (79) connected to a second detector (69), and having third (80) and fourth ports (74);
a first Y junction (34) having a first port connected to the third port (80) of said second coupler (67), and having second and third ports;
a second Y junction (36) having a first port connected to the fourth port (74) of said second coupler (67), and having second and third ports;
a third Y junction (55) having a first port connected to the fourth port (80) of said first coupler (66), and having second and third ports;
a first sensing loop (45) having first and second ends connected to the second and third ports, respectively, of said first Y junction (34);
a second sensing loop (42) having first and second ends connected to the second and third ports, respectively, of said second Y junction;
and a third sensing loop (60) having first and second ends connected to the second and third ports, respectively, of said third Y junction (55).
3. The three axis fiber optic gyroscope of claim 2 further comprising:
first, second and third sets of modulator electrodes (50, 44, 61) situated proximate to at least one port of said first, second and third Y
junctions (34, 36, 55), respectively.
first, second and third sets of modulator electrodes (50, 44, 61) situated proximate to at least one port of said first, second and third Y
junctions (34, 36, 55), respectively.
4. The three axis fiber optic gyroscope of claim 3, further comprising:
an at least one depolarizer (48, 49) connected between the first or second end of said first sensing loop and the second port of said first Y
junction (34);
an at least one depolarizer (41, 43) connected between the first or second end of said second sensing loop and the second port of said second Y junction (36);
an at least one depolarizer (58, 59) connected between the first or second end of said third sensing loop and the second port of said third Y
junction (55).
an at least one depolarizer (48, 49) connected between the first or second end of said first sensing loop and the second port of said first Y
junction (34);
an at least one depolarizer (41, 43) connected between the first or second end of said second sensing loop and the second port of said second Y junction (36);
an at least one depolarizer (58, 59) connected between the first or second end of said third sensing loop and the second port of said third Y
junction (55).
5. The three axis fiber optic gyroscope of claim 4 wherein:
said first Y junction (34) and first set of modulator electrodes (50) are formed on a first integrated optical circuit (65);
said second Y junction (36) and second set of modulator electrodes (44) are formed on a second integrated optical circuit (65); and said third Y junction (55) and third set of modulator electrodes (61) are formed on a third integrated optical circuit (65).
said first Y junction (34) and first set of modulator electrodes (50) are formed on a first integrated optical circuit (65);
said second Y junction (36) and second set of modulator electrodes (44) are formed on a second integrated optical circuit (65); and said third Y junction (55) and third set of modulator electrodes (61) are formed on a third integrated optical circuit (65).
6. The three axis fiber optic gyroscope of claim 4 wherein said first, second and third Y junctions and said first, second and third sets of modulator electrodes are formed on an integrated optical circuit.
7. The three axis fiber optic gyroscope of claim 6 further comprising:
an amplifier (117) having inputs connected to the first and second detectors;
an analog-to-digital converter (118) having an input connected to an output of said amplifier, and having an output;
a three axis gyroscope digital processing device (115) having an input connected to the output of said analog-to-digital converter;
a digital-to-analog converter (134) having an input connected to an output of said three axis gyroscope digital processing device, and having outputs connected to said first, second and third sets of modulator electrodes, respectively.
an amplifier (117) having inputs connected to the first and second detectors;
an analog-to-digital converter (118) having an input connected to an output of said amplifier, and having an output;
a three axis gyroscope digital processing device (115) having an input connected to the output of said analog-to-digital converter;
a digital-to-analog converter (134) having an input connected to an output of said three axis gyroscope digital processing device, and having outputs connected to said first, second and third sets of modulator electrodes, respectively.
8. The three axis fiber optic gyroscope of claim 7 wherein said three axis gyroscope digital processing device (115, 116) is a closed loop feedback system that nulls out phase differences of counterpropagating light in said first, second and third sensing loops, by signals sent from the output of said digital-to-analog converter to said first, second and third sets of modulator elements, respectively, the magnitude of the signals indicative of the rate of rotation of the respective sensing loops.
9. The three axis fiber optic gyroscope of claim 7 wherein said three axis gyroscope digital processing device (115) is a serrodyne closed loop feedback system.
10. The three axis fiber optic gyroscope of claim 7 wherein said three axis gyroscope digital processing system (116) is a dual ramp closed loop feedback system.
11. The three axis fiber optic gyroscope of claim 7 wherein said three axis gyroscope digital processing system is a digital phase step closed loop feedback system.
12. The three-axis fiber optic gyroscope of claim 4 further comprising:
a depolarizer (48) connected between the third port (80) of said second coupler (67) and the first port of said first Y junction;
a depolarizer (41) connected between the fourth port (74) of said second coupler (67) and the first port of said second Y junction; and a depolarizer (58) connected between the fourth port (80) of said first coupler (68) and the first port of said third Y junction.
a depolarizer (48) connected between the third port (80) of said second coupler (67) and the first port of said first Y junction;
a depolarizer (41) connected between the fourth port (74) of said second coupler (67) and the first port of said second Y junction; and a depolarizer (58) connected between the fourth port (80) of said first coupler (68) and the first port of said third Y junction.
13. The three-axis fiber optic gyroscope of claim 1 further comprising:
a depolarizer connected between the third port (20) of said coupler (12) and the first port of said first Y junction (32); and a depolarizer connected between the fourth port (22) of said coupler (12) and the first port of said fourth Y junction (55).
a depolarizer connected between the third port (20) of said coupler (12) and the first port of said first Y junction (32); and a depolarizer connected between the fourth port (22) of said coupler (12) and the first port of said fourth Y junction (55).
14. The three-axis fiber optic gyroscope of claim 13 wherein said first, second, third, and fourth junctions are polarizing junctions.
15. The three-axis fiber optic gyroscope of claim 12 wherein said first, second and third Y junctions are polarizing junctions.
16. The three-axis fiber optic gyroscope of claim 15 wherein said first, second and third sensing loops have non polarization maintaining fiber.
17. A three-axis fiber optic gyroscope comprising:
a first detector (69);
a second detector (93);
a light source (61);
a first coupler (60) having a first port (81) connected to said second detector (93), a second port (68) connected to said source (61), and third (71) and fourth (86) ports;
a second coupler (67) having a first port (79) connected to said first detector (69), a second port (72) connected to the third port (71) of said first coupler (66);
a first polarizer (146) connected to the third port (80) of said second coupler (67);
a second polarizer (145) connected to the fourth port (74) of said second coupler (68);
a third polarizer (147) connected to the fourth port (80) of said first coupler (66);
a third coupler (149) having a first port connected to said first polarizer (146), and having second (46) and third ports (47);
a fourth coupler (148) having a first port connected to said second polarizer (145), and having second (38) and third ports (40);
a fifth coupler (150) having a first port connected to said third polarizer (147), and having second (56) and third ports (57);
a first depolarizer (48) connected to the second port (46) of said third coupler (149);
a second depolarizer (41) connected to the second port (38) of said fourth coupler (148);
a third depolarizer (58) connected to the second port (56) of said fifth coupler (150);
a first non polarization maintaining fiber optic sensing loop (45) having a first end connected to said first depolarizer (48) and having a second end connected to the third port (47) of said third coupler (149);
a second non polarization maintaining fiber optic sensing loop (42) having a first end connected to said second depolarizer (41) and a second end connected to the third port (40) of said fourth coupler (148); and a third non polarization maintaining fiber optic sensing loop (60) having a first end connected to said third depolarizer (58) and a second end connected to the third port (57) of said fifth coupler (150).
a first detector (69);
a second detector (93);
a light source (61);
a first coupler (60) having a first port (81) connected to said second detector (93), a second port (68) connected to said source (61), and third (71) and fourth (86) ports;
a second coupler (67) having a first port (79) connected to said first detector (69), a second port (72) connected to the third port (71) of said first coupler (66);
a first polarizer (146) connected to the third port (80) of said second coupler (67);
a second polarizer (145) connected to the fourth port (74) of said second coupler (68);
a third polarizer (147) connected to the fourth port (80) of said first coupler (66);
a third coupler (149) having a first port connected to said first polarizer (146), and having second (46) and third ports (47);
a fourth coupler (148) having a first port connected to said second polarizer (145), and having second (38) and third ports (40);
a fifth coupler (150) having a first port connected to said third polarizer (147), and having second (56) and third ports (57);
a first depolarizer (48) connected to the second port (46) of said third coupler (149);
a second depolarizer (41) connected to the second port (38) of said fourth coupler (148);
a third depolarizer (58) connected to the second port (56) of said fifth coupler (150);
a first non polarization maintaining fiber optic sensing loop (45) having a first end connected to said first depolarizer (48) and having a second end connected to the third port (47) of said third coupler (149);
a second non polarization maintaining fiber optic sensing loop (42) having a first end connected to said second depolarizer (41) and a second end connected to the third port (40) of said fourth coupler (148); and a third non polarization maintaining fiber optic sensing loop (60) having a first end connected to said third depolarizer (58) and a second end connected to the third port (57) of said fifth coupler (150).
18. The three-axis fiber optic gyroscope of claim 17 further comprising:
a fourth depolarizer (49) connected between the third port (47) of said third coupler (149) and the second end of said first fiber optic sensing loop (45);
a fifth depolarizer (43) connected between the third port (40) of said fourth coupler (148) and the second end of said second fiber optic sensing loop (42); and a sixth depolarizer (59) connected between the third port (57) of said fifth coupler (150) and the second end of said third fiber optic sensing loop (60).
a fourth depolarizer (49) connected between the third port (47) of said third coupler (149) and the second end of said first fiber optic sensing loop (45);
a fifth depolarizer (43) connected between the third port (40) of said fourth coupler (148) and the second end of said second fiber optic sensing loop (42); and a sixth depolarizer (59) connected between the third port (57) of said fifth coupler (150) and the second end of said third fiber optic sensing loop (60).
19. The three-axis fiber optic gyroscope of claim 17 further comprising:
a fourth depolarizer connected between the third port (80) of said second coupler (67) and said first polarizer (146);
a fifth depolarizer connected between the fourth port (74) of said second coupler (67) and said second polarizer (145); and a sixth depolarizer connected between the fourth port (86) of said first coupler (66) and said third polarizer (147).
a fourth depolarizer connected between the third port (80) of said second coupler (67) and said first polarizer (146);
a fifth depolarizer connected between the fourth port (74) of said second coupler (67) and said second polarizer (145); and a sixth depolarizer connected between the fourth port (86) of said first coupler (66) and said third polarizer (147).
20. The three-axis fiber optic gyroscope of claim 19 further comprising:
a seventh depolarizer (49) connected between the third port (47) of said third coupler (149) and the second end of said first fiber optic sensing loop (45);
an eighth depolarizer (43) connected between the third port (40) of said fourth coupler (148) and the second end of said second fiber optic sensing loop (42); and a ninth depolarizer (59) connected between the third port (57) of said fifth coupler (150) and the second end of said third fiber optic sensing loop (60).
a seventh depolarizer (49) connected between the third port (47) of said third coupler (149) and the second end of said first fiber optic sensing loop (45);
an eighth depolarizer (43) connected between the third port (40) of said fourth coupler (148) and the second end of said second fiber optic sensing loop (42); and a ninth depolarizer (59) connected between the third port (57) of said fifth coupler (150) and the second end of said third fiber optic sensing loop (60).
21. The three-axis fiber optic gyroscope of claim 20 further comprising:
a first modulator (152) connected within and near an end of said first fiber optic sensing loop (45);
a second modulator (151) connected within and near an end of said second fiber optic sensing loop (42); and a third modulator (153) connected within and near an end of said third fiber optic sensing loop (60).
a first modulator (152) connected within and near an end of said first fiber optic sensing loop (45);
a second modulator (151) connected within and near an end of said second fiber optic sensing loop (42); and a third modulator (153) connected within and near an end of said third fiber optic sensing loop (60).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/672,249 | 1996-06-28 | ||
| US08/672,249 US5854678A (en) | 1996-06-28 | 1996-06-28 | Three-axis fiber optic gyroscope having a single source and multi-coupler configuration |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2258628A1 true CA2258628A1 (en) | 1998-01-08 |
Family
ID=24697774
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002258628A Abandoned CA2258628A1 (en) | 1996-06-28 | 1997-06-26 | A three-axis fiber optic gyroscope |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US5854678A (en) |
| EP (1) | EP0907877B1 (en) |
| JP (1) | JP4117030B2 (en) |
| CA (1) | CA2258628A1 (en) |
| DE (1) | DE69725720T2 (en) |
| WO (1) | WO1998000682A2 (en) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ATE485492T1 (en) | 2000-11-28 | 2010-11-15 | Politecnico Di Bari | INTEGRATED OPTICAL ANGLE SPEED SENSOR |
| US6801319B2 (en) * | 2002-01-03 | 2004-10-05 | Honeywell International, Inc. | Symmetrical depolarized fiber optic gyroscope |
| US7190462B2 (en) * | 2003-03-27 | 2007-03-13 | Japan Aviation Electronics Industry Limited | Fiber optic gyroscope having optical integrated circuit, depolarizer and fiber optic coil |
| US7085441B1 (en) * | 2005-03-04 | 2006-08-01 | Northrop Grumman Corporation | Fiber-optic gyroscope with depolarizer using integrated optic waveguide |
| CN100362320C (en) * | 2005-04-08 | 2008-01-16 | 北京航空航天大学 | Light small triaxial integral fibre-optical gyrometer |
| US7713196B2 (en) | 2007-03-09 | 2010-05-11 | Nellcor Puritan Bennett Llc | Method for evaluating skin hydration and fluid compartmentalization |
| US8560059B2 (en) * | 2007-03-09 | 2013-10-15 | Covidien Lp | System and methods for optical sensing and drug delivery using microneedles |
| US20080291459A1 (en) * | 2007-05-22 | 2008-11-27 | Litton Systems, Inc. | Fiber optic gyroscope with integrated light source |
| WO2009103015A2 (en) * | 2008-02-14 | 2009-08-20 | Bergh Ralph A | An interferometer employing a multi-waveguide optical loop path and fiber optic rotation rate sensor employing same |
| CN101290227B (en) * | 2008-06-17 | 2010-12-29 | 北京航空航天大学 | Three axis optical fibre gyroscope inertia measurement unit integral structure |
| US7973938B2 (en) * | 2008-09-24 | 2011-07-05 | Honeywell International Inc. | Bias-reduced fiber optic gyroscope with polarizing fibers |
| US8351046B2 (en) * | 2008-09-29 | 2013-01-08 | The Boeing Company | Multiple nested interferometric fiber optic gyroscope system |
| CN101788297B (en) * | 2010-03-26 | 2011-10-12 | 中北大学 | Minisize embedded inertia measurement unit having anti-high overload performance |
| WO2011140534A2 (en) | 2010-05-07 | 2011-11-10 | Bergh Ralph A | Method and apparatus for multiplexing multiple sagnac interferometers with single input for source light |
| CN102305628B (en) * | 2011-05-20 | 2013-06-12 | 浙江大学 | Triaxial integrated all-optical-fiber inertial sensing system |
| FR2990751B1 (en) * | 2012-05-16 | 2015-07-17 | Ixblue | FIBER OPTIC INTERFEROMETRIC MEASUREMENT SYSTEM AND INERTIAL GUIDE OR NAVIGATION SYSTEM COMPRISING SUCH AN INTERFEROMETER MEASUREMENT SYSTEM |
| CN102937448B (en) * | 2012-10-26 | 2015-04-15 | 北京航空航天大学 | Method for removing impulse noises of fiber-optic gyroscope based on slope coefficient |
| US9568317B2 (en) * | 2013-01-31 | 2017-02-14 | Honeywell International Inc. | Fiber optic gyroscope mixed signal application specific integrated circuit |
| WO2018132659A1 (en) | 2017-01-13 | 2018-07-19 | The Charles Stark Draper Laboratory, Inc. | Fiber management assembly for multi-axis fiber optic gyroscope |
| CN110388910A (en) * | 2018-04-19 | 2019-10-29 | 上海亨通光电科技有限公司 | A kind of optical fibre gyro with light source self-checking function |
| CN110579204B (en) * | 2019-08-20 | 2021-05-28 | 北京航空航天大学 | Optical fiber coupler array for triaxial integrated optical fiber gyroscope |
| TWI765412B (en) | 2020-11-13 | 2022-05-21 | 國立中山大學 | Silicon photonic integrated circuit and fiber optic gyroscope apparatus |
| CN113932789B (en) * | 2021-10-13 | 2023-03-07 | 宁波圣荣电子科技有限公司 | Data transmission method and system for optical fiber gyroscope |
Family Cites Families (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4445780A (en) * | 1982-03-01 | 1984-05-01 | The United States Of America As Represented By The Secretary Of The Navy | Fiber optic rotation-sensing gyroscope with (3×2) coupler |
| US4479715A (en) * | 1982-03-09 | 1984-10-30 | Sheem Sang K | Optical rotation-sensing interferometer with (3×3)-(2×2) directional coupler |
| US4653917A (en) * | 1983-03-24 | 1987-03-31 | The United States Of America As Represented By The Secretary Of The Navy | Fiber optic gyroscope operating with unpolarized light source |
| JPH0715385B2 (en) * | 1983-06-03 | 1995-02-22 | 住友電気工業株式会社 | Fiber optic gyro |
| FR2605101B1 (en) * | 1986-10-14 | 1988-12-09 | Thomson Csf | THREE-AXIS FIBER OPTIC RING INTERFEROMETER |
| US4828389A (en) * | 1987-04-21 | 1989-05-09 | Smiths Industries | Integrated triad optical rate sensor apparatus |
| US4869592A (en) * | 1988-01-27 | 1989-09-26 | Bergh Ralph A | Method and apparatus for obtaining a digital measure of absolute rotation |
| EP0388499A1 (en) * | 1989-03-23 | 1990-09-26 | LITEF GmbH | Rotation rate sensor device using Sagnac interferometers for three spatial directions |
| US4953935A (en) * | 1989-03-27 | 1990-09-04 | United Technologies Corporation | Integrated optic star coupler |
| DE3912005A1 (en) * | 1989-04-12 | 1990-10-18 | Messerschmitt Boelkow Blohm | METHOD FOR EVALUATING SIGNALS FOR A FIBER GYRO |
| WO1990015967A1 (en) * | 1989-06-21 | 1990-12-27 | Teldix Gmbh | Fibre laser gyrometer |
| DE3926312A1 (en) * | 1989-08-09 | 1991-02-14 | Messerschmitt Boelkow Blohm | SAGNAC TYPE FIBER GYRO |
| DE3926313A1 (en) * | 1989-08-09 | 1991-02-14 | Messerschmitt Boelkow Blohm | SAGNAC TYPE FIBER GYRO |
| US5157461A (en) * | 1990-06-14 | 1992-10-20 | Smiths Industries Aerospace & Defense Systems Inc. | Interface configuration for rate sensor apparatus |
| US5146956A (en) * | 1990-08-09 | 1992-09-15 | Slocomb Industries, Inc. | Programmable controlled winder |
| CA2049382C (en) * | 1990-08-27 | 1996-06-04 | Yozo Nishiura | Fiber-optic gyroscope with fibre polarizers, depolarizers and coupling means |
| DE4037118C1 (en) * | 1990-11-22 | 1992-04-30 | Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De | |
| DE4108807C2 (en) * | 1991-03-18 | 1994-09-01 | Litef Gmbh | Multi-axis fiber optic rotation rate sensor arrangement |
| US5184195A (en) * | 1991-05-28 | 1993-02-02 | Litton Systems, Inc. | Triaxial fiber optic Sagnac interferometer with single source and detector |
| DE4120675A1 (en) * | 1991-06-22 | 1992-12-24 | Messerschmitt Boelkow Blohm | SAGNAC TYPE OPTICAL FIBER GYRO |
| JPH087072B2 (en) * | 1991-09-25 | 1996-01-29 | 日本航空電子工業株式会社 | Fiber optic gyro |
| DE4134312A1 (en) * | 1991-10-17 | 1993-04-22 | Deutsche Aerospace | FIBER OPTICAL GYPSY |
| US5293439A (en) * | 1991-11-12 | 1994-03-08 | Sumitomo Metal Mining Co., Ltd. | Integrated optical circuit for fiber-optics gyroscopes |
| US5260768A (en) * | 1991-11-25 | 1993-11-09 | Litton Systems, Inc. | Fiber optic gyro with low-birefringence and PM networks |
| US5189488A (en) * | 1991-11-25 | 1993-02-23 | Litton Systems, Inc. | Fiber optical gyroscope utilizing orthogonal sequences |
| US5491763A (en) * | 1992-04-03 | 1996-02-13 | Koninklijke Ptt Nederland N.V. | Optical hybrid with 3×3 coupling device |
| DE4301479A1 (en) * | 1993-01-21 | 1994-07-28 | Deutsche Aerospace | Method and device for correcting the measurement signals of a fiber gyroscope |
| US5486921A (en) * | 1994-04-05 | 1996-01-23 | Litton Systems, Inc. | Optimum coupler configuration for fiber optic rate gyroscope using [3×] coupler |
-
1996
- 1996-06-28 US US08/672,249 patent/US5854678A/en not_active Expired - Lifetime
-
1997
- 1997-06-26 CA CA002258628A patent/CA2258628A1/en not_active Abandoned
- 1997-06-26 EP EP97945179A patent/EP0907877B1/en not_active Expired - Lifetime
- 1997-06-26 DE DE69725720T patent/DE69725720T2/en not_active Expired - Lifetime
- 1997-06-26 WO PCT/US1997/011412 patent/WO1998000682A2/en active IP Right Grant
- 1997-06-26 JP JP50439298A patent/JP4117030B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| DE69725720T2 (en) | 2004-07-29 |
| WO1998000682A3 (en) | 1998-02-26 |
| WO1998000682A2 (en) | 1998-01-08 |
| EP0907877A2 (en) | 1999-04-14 |
| JP2000513812A (en) | 2000-10-17 |
| JP4117030B2 (en) | 2008-07-09 |
| US5854678A (en) | 1998-12-29 |
| EP0907877B1 (en) | 2003-10-22 |
| DE69725720D1 (en) | 2003-11-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP0907877B1 (en) | A three-axis fiber optic gyroscope | |
| JP2863009B2 (en) | Reduction of Kerr effect error of resonator optical fiber gyroscope | |
| JP4142120B2 (en) | Method for measuring rotational speed about several axes, and interferometric gyroscope using this measuring method | |
| Strandjord et al. | Resonator fiber optic gyro employing a polarization-rotating resonator | |
| JPH059769B2 (en) | ||
| JP2007501413A (en) | Sensing loop doubler for fiber optic gyroscope | |
| CN112710294B (en) | Low-optical-noise double-ring parallel resonant gyro system and method | |
| EP0563279B1 (en) | Fiber optic gyro | |
| US4479715A (en) | Optical rotation-sensing interferometer with (3×3)-(2×2) directional coupler | |
| US5223911A (en) | Single-polarization, integrated optical components for optical gyroscopes | |
| US4382681A (en) | Measurement of rotation rate using Sagnac effect | |
| EP0502196B1 (en) | Optical interference angular velocity meter | |
| EP0078931B1 (en) | Angular rate sensor | |
| US4420259A (en) | Double coupled dual input rate sensor | |
| US5170275A (en) | Optical mixing for heterodyne detection | |
| EP0416070B1 (en) | Single-polarization, integrated optical components for optical gyroscopes | |
| JPH0447214A (en) | Optical fiber gyroscope | |
| CN109099899B (en) | Passive bias optical gyroscope | |
| EP1212624A2 (en) | Fiber optic current sensor | |
| JPS61122516A (en) | Optical fiber gyroscope | |
| JP2002502021A (en) | Optical fiber Sagnac interferometer | |
| JPS6329211A (en) | Optical fiber rotary sensor | |
| Kelley et al. | Novel fiber-optic gyroscopes for KEW applications | |
| JPH05133757A (en) | Ring resonant gyroscope | |
| Hartl et al. | Low-cost passive fiber optic gyroscope |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| FZDE | Discontinued |