There is a need for low cost, high performance gyroscopes for navigation systems, precision point systems, and guidance systems. Passive optical resonator gyroscopes, such as resonator fiber optic gyroscopes, are a type of gyroscope that is a promising contender for a next generation navigation grade gyroscope. Passive optical resonator gyroscopes have the potential to provide a solution that has high resolution at a low cost. Passive optical resonator gyroscopes are gyroscopes that use the Sagnac effect to measure resonance frequency shifts due to inertial rotation in a resonator, where the resonator does not contain a gain medium that leads to laser light generation inside the resonator. However, passive optical resonant gyroscopes generally include multiple laser sources outside the resonator and complicated locking schematics, or optical frequency shifters, which significantly increase production cost. If a solid core optical fiber resonator is used, which may allow for a high sensitivity in measuring rotation rate, the laser light intensity within the fiber resonator coil may generate Brillouin scattering within the fiber resonator coil of the gyroscope, where the Brillouin scattering degrades the performance of the gyroscope. Further the optical fiber used to fabricate a fiber resonator coil can be relatively bulky, expensive to make and wind, requires relatively expensive coupling optics, and can experience performance variations due to environmental factors.
Systems and methods for an optical frequency comb stimulated Brillouin scattering gyroscope with a rigid optical waveguide resonator are provided. In one embodiment, a system comprises: a light source that produces an optical frequency comb comprising a multiple-frequency light field; a rigid optical waveguide resonator coupled to the light source, wherein a recirculating optical frequency comb produced from the optical frequency comb propagates in a first direction around the rigid optical waveguide resonator and generates within the rigid optical waveguide a SBS light field comprising at least one SBS frequency component, and wherein one or more optical frequency components of the recirculating optical frequency comb are locked on resonance peaks of the rigid optical waveguide resonator; and an optical mixer configured to produce an optical beat signal that varies as a function of a frequency difference between the stimulated Brillouin scattering light field and the recirculating optical frequency comb.
Understanding that the drawings depict only exemplary embodiments and are not therefore to be considered limiting in scope, the exemplary embodiments will be described with additional specificity and detail through the use of the accompanying drawings, in which:
In accordance with common practice, the various described features are not drawn to scale but are drawn to emphasize specific features relevant to the exemplary embodiments.
In the following detailed description, reference is made to the accompanying drawings that form a part hereof, and in which is shown by way of illustration specific illustrative embodiments. However, it is to be understood that other embodiments may be utilized and that logical, mechanical, and electrical changes may be made. Furthermore, the method presented in the drawing figures and the specification is not to be construed as limiting the order in which the individual steps may be performed. The following detailed description is, therefore, not to be taken in a limiting sense.
Embodiments of the present disclosure provide for resonator optical gyroscopes where the resonator comprises a rigid waveguide such as a lithographically fabricated waveguide formed on a rigid substrate. The systems and methods described herein further provide a low cost, high performance gyroscope using a single laser source that produces an optical frequency comb. The optical frequency comb propagates around the optical waveguide resonator with at least one frequency component having a sufficient amplitude to produce stimulated Brillouin scattering (SBS) that counter-propagates around the optical waveguide resonator in the direction opposite to the optical frequency comb. Both the optical frequency comb, and the stimulated Brillouin scattering are constrained to match the resonance frequencies of the optical waveguide resonators associated with their particular direction of propagation. The optical frequency comb is locked to the resonances in the first direction (for example, the clockwise, CW, direction), for example, through servo electronics that control the laser light source. The generated SBS light frequencies are automatically on resonance in the second direction (for example, the counter-clockwise, CCW, direction) because lasers by their nature only output light at frequencies which resonate internally. The differences of the resonance frequencies in the two opposite directions contain information about the rotation rate of the gyro. The combination of using the optical frequency comb and an SBS light field intentionally generated in the rigid optical waveguide resonator can significantly reduce the cost of a navigation grade resonator optical gyroscope as compared to systems requiring two light sources. In particular, one or more embodiments of the gyroscope described herein, utilize a beat frequency signal derived from the optical frequency comb and SBS light to detect rotation rate.
Because the SBS light is frequency shifted by a Brillouin shift associated with the material used to fabricate the rigid optical waveguide resonator (for example, about 11 GHz in SiO2), the SBS light and the optical frequency comb do not necessarily overlap in frequency. When the optical frequency comb and the SBS light do not have overlapping frequency spectra in the gyro resonator, the optical frequency comb and the SBS light do not become frequency-locked on to one another when the CW wave backscatters into the CCW direction, or vice versa. Thus the gyroscope is able to avoid the well-known backscatter-induced lock-in effects that degrade gyroscope performance in conventional ring laser gyroscopes (RLGs) that are used in many navigation applications.
Laser light source 103 produces a multiple-frequency light field referred to herein as an optical frequency comb 104. In alternate embodiments, laser light source 103 may comprise a mode locked laser or a supercontinuum light source, and/or the optical frequency comb 104 may generated by laser light source 103 using optical parametric amplification, four wave mixing, electro-optic modulation, or other techniques. The optical frequency comb 104 comprises a plurality of optical frequency components at different optical frequencies, some of which can be locked at resonant frequencies of the optical waveguide resonator 102. For example, in some embodiments, the frequency components of the optical frequency comb from laser light source 103 may be locked to the resonance peaks of the resonator 102 through servo electronics 106.
The frequency spacing between two adjacent components of the optical frequency comb 104 is a function of, and directly related to, the free spectral range of the optical waveguide resonator 102. For example, this frequency spacing can be integer multiples or submultiples of the free spectral range of the optical waveguide resonator. In some embodiments, laser light source 103 is integrated into the same rigid substrate 101 as the optical waveguide resonator 102 and the multiple-frequency light field produced by laser light source 103 is also delivered to optical waveguide resonator 102 via a rigid waveguide 107 (such as a lithographically fabricated waveguide, for example) on the rigid substrate 101. That is, in such an embodiment, the entire optical path from the laser light source 103 to the optical waveguide resonator 102 is provided by rigid waveguide rather than including any lengths of optical fiber. One or all of laser light source 103, optical mixer 109, and rate output 108 may be formed on the same rigid substrate 101 as optical waveguide resonator 102 and interconnected as shown in
Light from the optical frequency comb 104 is incident on resonator 102, and all, or a portion of its energy is coupled into resonator 102. If the frequency spacing of spectral components the optical frequency comb 104 is an integer multiple of the free spectral range, then substantially all of the frequency components are coupled into resonator 102 with high efficiency. If the optical frequency comb 104 is a submultiple of the free spectral range only some of the frequency components are coupled into resonator 102 with high efficiency. The coupled light energy from optical frequency comb 104 that is coupled into the resonator recirculates many times around the resonator forming the recirculating optical frequency comb 104b, as a result of the resonance condition of the resonator. As the recirculating optical frequency comb 104b propagates within the optical waveguide resonator 102 in a first direction (a clockwise direction as shown in
As the recirculating optical frequency comb 304a propagates around optical waveguide resonator 102, the multiple optical frequency components 305 of that light field each generate an associated stimulated SBS optical frequency component 307 to form the counter-propagating SBS light field 302a within the waveguide resonator (i.e., that propagates through the rigid waveguide resonator in a direction that is opposite to the direction of propagation for optical frequency comb 304a). Each SBS optical frequency component 307 is frequency shifted from its associated optical frequency component 305 of the comb 304a (i.e., the optical frequency component 305 of comb 304a that generated the SBS optical frequency component 307) by the Brillouin shift. That is, in this example, the SBS multiple-frequency light field 302a will be similar to the multiple frequency light field of recirculating optical frequency comb 304a, except the SBS multiple-frequency light field 302a is frequency-shifted by the Brillouin shift. As mentioned above, the amount of Brillouin shift is dependent on the material through which the light fields are propagating. It should be appreciated that in some implementations where the recirculating optical frequency comb 304a has optical frequency components 305 of varying amplitude, some of those optical frequency components may be of sufficient power to generate an associated SBS optical frequency component 307 in the SBS light field 302a, while others are not. Accordingly, in some implementations, the SBS light field 302a will comprise fewer optical frequency components 307 than the recirculating optical frequency comb 304a.
In the embodiment shown in
The optical mixer 109 mixes the SBS light field 105 including the at least one frequency of light and the multiple-frequency light field from the optical frequency comb 104 or from a portion of the recirculating optical frequency comb 104b to create the beat frequency signal 110 containing at least one beat frequency. The beat frequency signal 110 comprises a signal component having a frequency or frequencies that are a function of the difference between the optical frequency components of the optical frequency comb 104, or a portion of the recirculating optical frequency comb 104b, and the SBS light field 105. The optical mixer 109 then provides the beat frequency signal 110 to the rate output 108. In one case, the beat frequency signal 110 contains multiple beat frequencies of multiple FSRs plus the frequency shift due to rotation rate. In a second case, the optical frequency comb portion 104 or the portion of the recirculating optical frequency comb 104b is filtered such that said portion only contains one frequency component of the original optical frequency comb 104, and only one SBS frequency is selectively generated. In this case, the beat frequency signal 110 contains a single, selected beat note of zero FSRs plus the frequency shift due to rotation rate, or it contains a single beat note of a frequency of an integer number of FSRs plus the rotation rate. In this case where said portion contains only one frequency, the optical frequency comb (OFC) helps to down convert the large offset beat signal to just the rotation-induced frequency shift, or to a frequency of small integer number of FSRs plus the rotation rate. Using OFC to down convert the 11 GHz beat signal to a very low beat frequency also service to increase the Signal-to-noise ratio (SNR). A highly stable OFC thus substantially removes the large SBS frequency offset from the measurement, making it easier to measure the small frequency shift due to rotation. In this way, the small frequency shift due to rotation is isolated for direct measurement, not mixed in with the large SBS frequency shift (which would add measurement errors in the indication of rotation-induced frequency shifts).The rate output 108 determines the rate of rotation for the gyroscope 100 based on the beat frequency 110.
By potentially using a single laser light source 103 to generate an optical frequency comb 104, laser resonator gyroscope 100 can offer both low cost and high resolution. Gyroscope 100 uses the both the optical frequency comb 104 and stimulated SBS light field 105 generated within the optical waveguide resonator 102 to obtain the rotation rate information. Also, because the stimulated SBS light field 105 is used to provide rate of rotation information, the gyroscope does not need to include mechanisms to suppress the stimulated Brillouin scattering. Thus, because of the simplified lock-in avoidance mechanism and the use of the stimulated SBS light field 105 to determine rate of rotation, the gyroscope can be produced at a reduced cost.
In addition to the components that correspond with components described in relation to system 100 in
A portion of the light coupled from optical frequency comb 204 is coupled into the resonator 202 to form recirculating optical frequency comb 204b. As the recirculating optical frequency comb 204b propagates within the optical waveguide resonator 202 in a first direction (a clockwise direction as shown in
When one or more optical frequency components of the recirculating optical frequency comb 204 and SBS multiple-frequency light field 205 overlap in their frequency spectra, and there can be optical backscatter from one direction into the other, the counter-propagating signals (204b, 205) in the gyroscope's resonator 202 can become locked onto one another. When counter-propagating signals become locked onto one another, the measured rotation rate becomes zero even when the actual value is not zero. The optical filter 220 limits the bandwidth of the optical frequency comb 204 so that it prevents signals that have similar frequencies from propagating within the optical waveguide resonator 202 in opposite directions. For example, where the Brillouin shift for the optical waveguide resonator is 11 GHz, the optical filter 220 attenuates an optical frequency comb 204 generated by a light source 203 such that frequencies of the SBS optical frequency components that are shifted 11 GHz do not overlap with the non-shifted optical frequency components of the optical frequency comb 204 and recirculating optical frequency comb 204b.
In at least one embodiment, system 200 also includes a free spectral range (FSR) control 212. Free spectral range control 212 may be formed on the same rigid substrate 201 as optical waveguide resonator 202 and interconnected as shown in
Further, in at least one implementation, one or more optional attenuators (shown at 214) optionally optically attenuate one or both of the SBS light field 205 and a portion of the recirculating optical frequency comb light field 204b prior to mixing by optical mixer 209. Attenuators 214 may be formed on the same rigid substrate 201 as optical waveguide resonator 202 and interconnected as shown in
In the embodiment shown in
The optical mixer 209 mixes the SBS light field 205 including the at least one frequency of light and the multiple-frequency light field from the optical frequency comb 204 or the recirculating optical frequency comb 204b to create at least one beat frequency signal 210. The beat frequency signal 210 comprises a signal component having a frequency that is a function of the difference between the optical frequency components of the optical frequency comb 204 or the recirculating optical frequency comb 204b, and the SBS light field 205. The optical mixer 209 then provides the beat frequency signal 210 to the rate output 208. The rate output 208 determines the rate of rotation for the gyroscope 200 based on the beat frequency 210.
Here, laser light source (103, 203) produces a multiple-frequency light field having only a single component in recirculating optical frequency comb (shown at 303) that has an intensity (i.e., amplitude or power) large enough to generate stimulated Brillouin scattering (SBS) in resonator 202.
In certain embodiments, the components 305 of the multiple-frequency light field comprised of the recirculating optical frequency comb 304b may overlap with the frequency spectrum contained within the SBS light field 302b. The overlapping frequencies can cause a gyroscope to exhibit lock-in effects, or degrade the ability to precisely adjust lock the CW wave comb frequencies to the frequencies of the optical waveguide resonator as desired, which degrades the performance of the gyroscope. To avoid the problem of overlapping frequencies, the frequency components of the light field constituting the recirculating optical frequency comb 304 may be configured so that frequencies are greater than the frequency of the Brillouin light field 302b.
In certain embodiments, the frequencies of the multiple-frequency light field constituting the recirculating optical frequency comb 304c may overlap with the frequency of the SBS light field 302c. The overlapping frequencies, in the presence of optical backscatter, can cause a gyroscope to exhibit lock-in, or degrade the precision of the lock between frequencies of the frequency comb 304c and the resonator resonance frequencies which degrades the performance of the gyroscope. To avoid the overlapping frequencies, the multiple-frequency light field constituting the optical frequency comb emitted by the laser can be filtered by a pass band 306 (see for example, as applied by optical filter 220 in
Method 400 proceeds to 404 with mixing of a portion the recirculating optical frequency comb emanating from the rigid optical waveguide resonator in a first direction with the a portion of the SBS light field emanating from the rigid optical waveguide resonator in a first direction to produce at least one signal that is a function of a frequency difference between the recirculating optical frequency comb and the SBS light field. In one embodiment, mixing the portions of the recirculating optical frequency comb with the SBS light field is performed by a mixer formed on the same rigid substrate at the rigid optical waveguide resonator. That is, this resulting signal comprises a beat frequency signal derived from the recirculating optical frequency comb and SBS light that is a function of the rotation rate of the rigid waveguide resonator. As such, the method 400 may proceed to 406 with determining a rate of rotation based on the at least one signal. For example, as the gyroscope/rigid resonator rotates, the frequency difference between the SBS light field and the recirculating optical frequency comb changes in proportion to the rate of rotation. When these optical signals are mixed, a beat signal is produced having a beat frequency that is a function of the difference between the frequency of the SBS light field and the recirculating optical frequency comb. Since the nominal zero rotation rate beat signal is a known value (i.e., the difference between the frequency of the SBS light field and the recirculating optical frequency comb without the influence of Sagnac effect) differences between that nominal zero rotation rate beat signal and the output produced by mixing the optical signals at 404 can be used to determine the rate of rotation.
Example 1 includes a system comprising: a light source configured to produce an optical frequency comb comprising a multiple-frequency light field; a rigid optical waveguide resonator coupled to the light source, wherein a recirculating optical frequency comb produced from the optical frequency comb propagates in a first direction around the rigid optical waveguide resonator and generates within the rigid optical waveguide a stimulated Brillouin scattering (SBS) light field comprising at least one SBS frequency component, and wherein one or more optical frequency components of the recirculating optical frequency comb are locked on resonance peaks of the rigid optical waveguide resonator; and an optical mixer configured to produce an optical beat signal that varies as a function of a frequency difference between the stimulated Brillouin scattering light field and the recirculating optical frequency comb.
Example 2 includes the system of example 1, wherein the rigid optical waveguide resonator is fabricated on a rigid substrate.
Example 3 includes the system of example 2, wherein the rigid optical waveguide resonator is a lithographically fabricated waveguide formed on the rigid substrate.
Example 4 includes the system of any of examples 2-3, wherein the rigid optical waveguide resonator is formed on an optical grade crystal substrate.
Example 5 includes the system of any of examples 2-4, wherein one or both of the light source and the optical mixer are formed on the rigid substrate and interconnected with the rigid optical waveguide resonator by rigid waveguides.
Example 6 includes the system of any of examples 1-5, further comprising servo electronics configured lock the optical frequency comb to the resonance peaks of the rigid waveguide resonator based on feedback signals from processed resonator output that contains information about deviation of the plurality of component frequencies from resonance peaks in the first direction of the rigid optical waveguide resonator.
Example 7 includes the system of example 6, wherein the feedback signal comprises information about deviation of the one or more optical frequency components of the recirculating optical frequency comb from resonance peaks in the first direction of the rigid optical waveguide resonator; and wherein one or more frequency components of the optical frequency comb have a frequency separation that tracks free spectral range drift of the rigid optical waveguide resonator.
Example 8 includes the system of any of examples 1-7, further comprising an optical filter configured to filter the multiple-frequency light field such that a first frequency range of the recirculating optical frequency comb does not overlap with a second frequency range of the stimulated Brillouin scattering light field.
Example 9 includes the system of example 8, wherein the rigid optical waveguide resonator is coupled to the optical filter such that the rigid optical waveguide resonator receives the multiple-frequency light field after the multiple-frequency light field is filtered.
Example 10 includes the system of any of examples 8-9, wherein the rigid optical waveguide resonator is fabricated on a rigid substrate; and wherein at least one of the light source, the optical mixer, and the optical filter are formed on the rigid substrate and interconnected with the rigid optical waveguide resonator by rigid waveguides.
Example 11 includes the system of any of examples 1-10, wherein the optical mixer receives both the recirculating optical frequency comb and the stimulated Brillouin scattering light field from the rigid optical waveguide resonator via rigid waveguides.
Example 12 includes the system of any of examples 1-11, wherein the optical mixer receives the optical frequency comb from the light source via a first rigid waveguide and the stimulated Brillouin scattering light field from the rigid optical waveguide resonator via a second rigid waveguide.
Example 13 includes the system of any of examples 1-12, further comprising at least one attenuator coupled to the optical mixer, the at least one attenuator configured to attenuate at least one of the recirculating optical frequency comb and the stimulated Brillouin scattering light field prior to the optical mixer.
Example 14 includes the system of any of examples 1-13, further comprising a comb spacing control coupled between the rigid optical waveguide resonator and the light source, the comb spacing control configured to adjust the frequency separation of the multiple-frequency light field to track the free spectral range of the optical waveguide resonator.
Example 15 includes the system of any of examples 1-14, wherein the stimulated Brillouin scattering (SBS) light field is generated by fewer than all of the one or more optical frequency components of the recirculating optical frequency comb.
Example 16 includes a method for measuring rotation, the method comprising: propagating a recirculating optical frequency comb through a rigid optical waveguide resonator in a first direction, wherein the recirculating optical frequency comb stimulates a stimulated Brillouin scattering (SBS) light field including at least one frequency component in a second direction counter to the first direction; mixing a portion the recirculating optical frequency comb emanating from the rigid optical waveguide resonator with the a portion of the SBS light field emanating from the rigid optical waveguide resonator to produce at least one signal that is a function of a frequency difference between the recirculating optical frequency comb and the SBS light field; and determining a rate of rotation based on the at least one signal.
Example 17 includes the method of example 16, further comprising: controlling a light source that produces the optical frequency comb such that a plurality of frequency components of the recirculating optical frequency comb are locked to resonance peaks of the rigid optical waveguide resonator and have a frequency separation that tracks free spectral range drift of the rigid optical waveguide resonator.
Example 18 includes the method of any of examples 16-17, further comprising: filtering the multiple-frequency light field such that a first frequency range of the recirculating optical frequency comb does not overlap with a second frequency range of the stimulated Brillouin scattering light field.
Example 19 includes the method of any of examples 16-18, wherein the rigid optical waveguide resonator is fabricated on a rigid substrate comprising an optical grade crystal.
Example 20 includes the method of example 19, wherein one or both of a light source that produces the optical frequency comb and an optical mixer that mixes the portion the recirculating optical frequency comb emanating from the rigid optical waveguide resonator with the portion of the SBS light field emanating from the rigid optical waveguide resonator r are formed on the rigid substrate and interconnected with the rigid optical waveguide resonator by rigid waveguides.
Although specific embodiments have been illustrated and described herein, it will be appreciated by those of ordinary skill in the art that any arrangement, which is calculated to achieve the same purpose, may be substituted for the specific embodiments shown. Therefore, it is manifestly intended that this invention be limited only by the claims and the equivalents thereof.
This application claims priority to and the benefit of U.S. Provisional Application 62/103,158 entitled “OPTICAL FREQUENCY COMB STIMULATED BRILLOUIN SCATTERING GYROSCOPE WITH RIGID OPTICAL WAVEGUIDE RESONATOR” filed on Jan. 14, 2015, which is herein incorporated by reference in its entirety.
Number | Date | Country | |
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62103158 | Jan 2015 | US |