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    • 专利摘要:
    The present invention relates to an interferometric measuring device (100) comprising a light source (110) emitting a source signal and optical coupling means (121) receiving the source signal, directing a part thereof to a measurement channel ( 102) comprising a Sagnac ring interferometer (141) of natural frequency fp, outputting an output power output signal POUT biased in a first polarization direction, taking another portion of the source signal to a channel compensation device (103) producing a feedback power compensation signal PRET, and directing the output signal and the compensation signal to detection means. According to the invention, the compensation path comprises polarization rotation means (131) producing the compensation signal in a second cross polarization direction, and optical feedback means (132) redirecting a portion of the compensation signal to the measuring path; the detection means comprise a single detector (150) connected to the coupling means for receiving the output signal and the compensation signal; the device further comprises power balancing means (132) equalizing the output power and / or the return power supplied to the detector, and the compensation path has a length adjusted so that the output signal has, relative to to the compensation signal, a time delay τ equal to 1 / (2 * fp) at the detector.
    公开号:FR3017945A1
    申请号:FR1451543
    申请日:2014-02-26
    公开日:2015-08-28
    发明作者:Herve Lefevre；Frederic Guattari；Cedric Molucon；Stephane Chouvin
    申请人:iXBlue SAS；
    IPC主号:
    专利说明:

    [0001] TECHNICAL FIELD OF THE INVENTION The present invention relates to optical metrology by interferometric method. It relates more particularly to an interferometric measurement device for reducing the excess intensity noise of the light source used in this interferometric measurement device. The invention finds a particularly advantageous application in the production of a gyrometer comprising such an interferometric measuring device and in the production of a central attitude or inertial navigation using such a gyrometer. BACKGROUND ART US Pat. No. 5,331,404 discloses an interferometric measuring device comprising: a broad spectrum spontaneous emission light source emitting a source light signal; detection means delivering an electrical signal representative of the result of a measurement of said parameter to be measured, - processing and electrical control means processing said electrical signal to provide said measurement of said parameter to be measured, and - optical coupling means: receiving said source light signal, directing at least a part of said light signal source to a measurement channel comprising a measurement interferometer which comprises a phase modulator and a Sagnac ring, of natural frequency fp, responsive to said parameter to be measured, said interferometer receiving, as input, a luminous power input light signal PIN output and producing, at the output, a light output signal of read power output lightning machine For dependent on said physical parameter to be measured and proportional to said PIN input light power, said output light signal being polarized in a first polarization direction and modulated to a modulation frequency f, by said phase modulator, sampling another portion of said source light signal to a noise compensation path separate from said measurement path, said noise compensation path providing a compensation light signal having a return light power PRET, directing said output light signal and said light signal compensation to said detection means.
    [0002] In the following description, a light source is said to "spontaneous emission" when the spectrum of this source comprises a continuum of wavelengths. Examples of such a source include: the sun, a radiant heat source, a super-luminescent diode semiconductor, also called super-radiant, or a super-fluorescent source amplifying fiber.
    [0003] These super-luminescent, super-radiating or super-fluorescent sources are in fact spontaneous emission sources whose spontaneous emission is amplified by a stimulated emission which retains the spectral characteristics of the spontaneous emission of origin. The general term for this type of source is ASE (for "Amplified by stimulated emission Spontaneous Emission"). Unlike an ASE source, a laser source is not a spontaneous emission light source, its emission spectrum does not include a continuum of wavelengths. A light source shall also be considered to have a wide spectrum when the ratio between the full width at half maximum or FWHM (for "Full Width at Half Maximum") of its continuous spectrum and its average wavelength is greater than 10-7. For example, an erbium doped fiber light source (chemical symbol Er) filtered by means of a Bragg filter typically has a pseudo-Gaussian spectrum centered around a wavelength of 1530 nm to 1560 nm and having a full mid-height width (FWHM) of about 5 to 20 nanometers (nm); this light source is therefore a wide source, the ratio between its full width at half height and its average wavelength being equal to approximately 3 to 12 x 10-3. A wide-spectrum spontaneous emission light source emits a light signal whose light output is subject to different sources of noise.
    [0004] First of all, Bph photonic noise is known as "shot noise" and is the theoretical limit of any light source. Photonic noise is a white noise whose value is directly related to the light output of the light source. More precisely, the photonic noise varies, in absolute terms, as the square root of the luminous power and therefore, in relative terms, as the inverse of the square root of the luminous power. For example, a light signal at 1550 nm of 30 microwatt (1.1W) of power has a relative photonic noise Bph of 10-7 / Hz1 / 2 in standard deviation, that is to say 10-14 / Hz in noise power, ie -140 decibels / Hz (-140 dB / Hz).
    [0005] For a light signal of power 300 μW, thus ten times higher, the relative photonic noise Bph is -150 dB / Hz, or 10 dB / Hz below in noise power, or a factor 10 in noise power and a factor square root of 10 (101/2 ge 3.16) in standard deviation. Also known is excess relative noise ("excess Relative lntensity Noise" in English, or "excess RIN" or simply "RIN"), which is also a white noise but for frequencies less than one-tenth of the full width at mid-height of the optical frequency spectrum, FWHM (f), ie 0.1 to 0.3 terahertz (THz) for a FWHM (in wavelength) of 7 to 20 nm around a wavelength 1550 nm.
    [0006] The relative noise of excess intensity BRIN is, in noise power, approximately equal to the inverse of the full width at half height of the optical frequency spectrum FWHM (f) of the broad-spectrum light signal, ie ie BRIN = 1 / FWHM (f). Indeed, it is known that the excess intensity noise comes from the power beats between all the different frequency components of the continuous broad spectrum of the light signal which interfere with each other, these components having between them different frequencies and a phase random. The spectrum of the relative noise of excess intensity is therefore the result of an autocorrelation law: it starts at the zero frequency and has a width substantially equal to the width of the optical spectrum of the light source which is in turn contrast centered around a very high frequency, about 200 THz for a wavelength of 1550 nm. Thus, the same light signal of 30 1..1W of power which would present a full width at half-height in optical frequency FWHM (f) of 1THz, thus of 1012Hz, would, at low frequency, have a relative intensity noise in excess BRIN of 10-12 / Hz or -120 dB / Hz, in power of noise, and thus 20 dB / Hz above the relative photonic noise power Bph of -140 dB / Hz. Such a broad-spectrum spontaneous emission signal has a relative noise of excess intensity which is the dominant source of noise and which should be compensated or even eliminated. The interferometric measurement device of US Pat. No. 5,331,404 uses for this purpose detection means which comprise two distinct optical radiation detectors measuring, the one the output light signal produced by the measurement interferometer which is tainted by the noise RIN of the light source, and the other the noise compensation light signal tainted by the same sound RIN. It is then expected that the processing and electrical control means process the electrical signals delivered by each of the detectors, in order to subtract the noise RIN from the electrical measurement signal with the noise RIN of the compensation signal, so that the measurement of the parameter is more precise. However, the interferometric measurement device of US Pat. No. 5,331,404 proves difficult to implement because of the additional electronic processing chain necessary for the subtraction of the RIN noise.
    [0007] OBJECT OF THE INVENTION In order to overcome the above-mentioned drawback of the state of the art, the present invention proposes an interferometric measurement device making it possible to compensate for, or even eliminate, optically and simply, the noise of excess intensity. staining the output light signal produced by the interferometer. For this purpose, the invention relates to an interferometric measuring device as described in the introduction. According to the invention, said interferometric measurement device is such that: said noise compensation channel RIN comprises: polarization rotation means adapted to produce said compensation light signal in a second direction of polarization crossed with said first direction of polarization, and - means of optical loopback of said compensation channel on said measurement channel, said loopback means receiving said compensation light signal flowing on said compensating channel and redirecting at least part of said compensation light signal to said channel measuring means, - said detection means comprise a single optical radiation detector connected to said optical coupling means, said optical coupling means receiving said power output light signal For and said power compensation light signal PRET, which flow on said measuring path, to route them to said detector - power balancing means adapted to correct said FRET return light power or said output power for routing towards said detector are provided in such a way that said return light power PRET is substantially equal to said power. luminous output For at said detector, and - said compensation path has a length such that said output light signal has at the detector a time delay i with respect to said compensation light signal substantially equal to 1 / (2 * fp ).
    [0008] The device according to the invention makes it possible to reduce or even eliminate the effect of excess intensity noise of the light source on the measurement of the parameter to be measured by means of the measurement interferometer, and this by using a single detector of optical radiation. In addition, the realization of such an interferometric measuring device, in particular of its processing and electrical control means, is easier because it uses only one light radiation detector and a single processing chain. electronic. Thanks to the configuration of the compensation channel with its polarization rotation means and its optical loopback means, it is possible to reinject, on the measurement channel, the RIN noise compensation light signal which carries the same noise. intensity in excess of the output light signal, these two light signals then being conveyed to the single detector of the detection means thanks in particular to the optical coupling means. Since the output light signal and the compensation light signal are polarized in two directions of polarization orthogonal to each other, these two signals can not interfere with each other, so that the electrical signal delivered by the optical radiation detector is directly proportional to the sum of the output light power For and the return light power READY. The length of the compensating channel being adjusted so that the output light signal has at the detector a time delay i relative to the compensation light signal substantially equal to 1 / (2 * fp), and the return light power PRET being substantially equal to said output light power. For said detector by the power balancing means, the excess intensity noise at the characteristic frequencies equal to an odd multiple of the natural frequency fp (ie fp, 3 * fp, 5 * fp, etc ...) of the measurement interferometer is reduced or eliminated if ti = 1 / (2 * fp) and if For = READY on the detector.
    [0009] As explained in "The Fiber-Optic Gyroscope" (H. Lefèvre, Artech House, 1993), the output light signal, which carries the information on the parameter to be measured, is advantageously modulated at a frequency of modulation f, which is precisely an odd multiple of the natural frequency fp of the Sagnac ring interferometer (ie f, = (2k + 1) * fp, where k is a natural integer).
    [0010] Thus, thanks to the interferometric measuring device according to the invention, it is advantageously possible to overcome the effect of the excess intensity noise coming from the light source in order to make an accurate measurement of the parameter to be measured. In other words, using the interferometric measuring device according to the invention, a light intensity (ie power) delay line is obtained which makes it possible to subtract optically for all the odd multiple frequencies of the frequency the measurement interferometer itself, of the measurement signal, a reference signal having at these frequencies the same noise of excess intensity. The powers of the measurement and reference signals are summed on the detector, but at the odd multiples of the natural frequency, this summation is equivalent to a subtraction, because the noises at these frequencies are in phase opposition. Advantageously, the time delay ti between the output light signal and the compensation light signal is between 0.9 / (2 * fp) and 1.1 / (2 * fp), preferably between 0.99 / (2 * fp) and 1.01 / (2 * fp). Preferably, this time delay i is greater than 1 / (2 * fp).
    [0011] Advantageously, the P / P ratio. RET. OUT between the return light power READY and the output light power For is between 0.8 and 1.2, preferably between 0.95 and 1.05. Furthermore, other advantageous and non-limiting features of the interferometric measuring device according to the invention are the following: said interferometric measuring device further comprises a linear polarizer placed downstream of said light source for polarizing said source light signal according to said first direction of polarization; wherein said optical coupling means comprises a first two by two four-port coupler; said optical coupling means comprise an optical circulator placed upstream of said first coupler, said optical circulator having three ports respectively connected to said light source, to one of said first coupler ports, and to said detector; said optical loopback means comprise a second four-port two by two coupler, said power balancing means also comprising said second coupler; said optical loopback means comprise a polarization splitter; said power balancing means comprise an optical attenuator for a light signal polarized along said second polarization direction so as to correct said return light power PRET- In the general case where the light source emits a non-polarized source light signal, the device interferometric measurement is designed for such a light source, and, on the one hand, said compensation channel comprises an optical isolator for blocking a polarized light signal in the second polarization direction propagating on said compensation path in the opposite direction of said compensation light signal, and secondly, said optical loopback means comprise a polarization splitter. In this case, other advantageous and non-limiting features of the interferometric measuring device according to the invention are the following: said optical coupling means comprise a first two-by-two coupler with four ports; said optical coupling means comprise an optical circulator placed upstream of said first coupler, said optical circulator having three ports respectively connected to said light source, to one of the ports of said first coupler, and to said detector, and said balancing means power devices comprise said first coupler; said optical coupling means further comprise a second four-port two by two coupler, and said power balancing means comprise said second coupler; said power balancing means comprise an optical attenuator for a light signal polarized along said second polarization direction so as to correct said return light power P RET - said power balancing means comprise said phase modulator and said processing means and electrical control controlling said phase modulator to correct said output light power For. The present invention finds a particularly advantageous application in the production of an optical fiber gyro having an interferometric measuring device for measuring the speed of rotation about an axis of rotation perpendicular to the plane of the SAGNAC ring of the measurement interferometer.
    [0012] Thus, the present invention also relates to a gyrometer comprising an interferometric measuring device according to the invention, the physical parameter to be measured being a component of the speed of rotation of said gyrometer about its axis of rotation, said axis of rotation being merged with the axis of revolution of the SAGNAC ring. The present invention also relates to a central attitude or inertial navigation comprising at least one such gyro.
    [0013] DETAILED DESCRIPTION OF AN EXEMPLARY EMBODIMENT The following description with reference to the accompanying drawings, given as non-limiting examples, will make it clear what the invention consists of and how it can be achieved.
    [0014] In the accompanying drawings: FIGS. 1 to 3 show schematic views respectively of a first, second and third embodiment of an interferometric measuring device according to the invention in which the device comprises a linear polarizer placed downstream of the light source; FIG. 4 represents a schematic view of a variant of the third embodiment of FIG. 3 in which the compensation channel comprises an optical attenuator; - Figures 5 to 7 show schematic views respectively of a fourth, fifth and sixth embodiment of an interferometric measuring device according to the invention designed for a non-polarized light source; FIG. 8 represents a schematic view of a seventh embodiment of an interferometric measurement device according to the invention. Figures 1 to 8 show diagrammatic views showing a device 100; 200; 300; 400 of interferometric measurement according to several embodiments of the invention and their variants. This device 100; 200; 300; 400 is here an optical fiber device which comprises different channels 101, 102, 103, 104 of circulation for the propagation of light signals in this device 100; 200; 300; 400, all these channels 101, 102, 103, 104 being formed of sections of optical fiber, for example silica optical fibers conventionally used in optical telecommunications. In these different embodiments, the device 100; 200; 300; 400 comprises a light source 110, a measurement interferometer 140 and a single optical radiation detector 150. The light source 110 is here a broad spectrum spontaneous emission light source. This is for example a light source ASE optical fiber doped with a rare earth, for example erbium such as those conventionally used in the field of optical telecommunications. This light source 110 may be filtered by means of a Bragg filter (not shown) so that it has a substantially Gaussian optical spectrum, which is centered around an average wavelength λ 0 of 1530 nm, that is 196 THz in frequency, and which has a full width at half height FWHM of 6.5 nm, or 833 GHz, expressed in frequency. This light source 110 is therefore a broad-spectrum light source since the ratio between its full width at half height FWHM and its average wavelength λ0 is equal to 4.2 × 10 -3, greater than 10-7.
    [0015] This light source 110 emits a source light signal S1,11; S1,11, S'1, ± on a source channel 101 of the device 100; 200; 300; 400 interferometric measurement. As mentioned above, the source channel 101 is formed of an optical fiber section, for example a polarization maintaining single mode fiber section when the source is polarized (the case of FIGS. 1 to 4) or an ordinary fiber section when the source is non-polarized (the case of Figures 5 to 8). This light signal source Sil; Sil, S'1, ± is tainted by a relative noise of excess intensity BRIN whose noise power spectral density is equal to 1 / FWHM or 1.2 x 10-12 / Hz, or -119 dB / Hz.
    [0016] The spectral density of photonic noise power is constant and independent of the frequency, the photonic noise being known to be a white noise. With an output power of 3011W, the relative photonic noise Bph would be equal to 10-7 / Hz1 / 2, ie -140 dB / Hz for the relative photonic noise power spectral density. Conversely, as mentioned above, it is known that the noise of excess intensity is not rigorously a white noise. Nevertheless, for the light source 110 which has a wide Gaussian full-width half-height optical spectrum FWHM = 6.5 nm around the average wavelength λ = 1530 nm, the spectral power density of the relative noise of Excess intensity can be considered constant below a frequency equal to one-tenth of the full width at half-full optical frequency FWHM (f) or 83 GHz.
    [0017] Thus, for a frequency band between 0 and 100 MHz, for example, the relative power density of the excess intensity intensity BRIN is much greater than the relative photonic noise power density, the difference being as large as 21 dB / Hz. The measurement interferometer 140 of the device 100; 200; 300; 400 of interferometric measurement in the different embodiments of the invention here comprises a ring 141 of SAGNAC optical fiber and a modulator 143 phase. The measurement interferometer 140 is intended to measure a physical parameter, to which the ring 141 of Sagnac is sensitive. Here, this physical parameter to be measured is the s2R component of the rotational speed of the measurement interferometer 2, along an axis of rotation (not shown) perpendicular to the plane of the SAGNAC ring. This device 100; 200; 300; 400 interferometric measurement can enter into the realization of a gyrometer, here a fiber optic gyroscope, which can itself be part of a central attitude or inertial navigation. The physical parameter s2R to be measured then corresponds here to a component of the speed of rotation of the gyrometer around its axis of rotation, that being, for example, coinciding with the axis of the SAGNAC ring. In a known manner (see in particular H. Lefèvre, "The Fiber-Optic Gyroscope", Artech House, 1993), the ring 141 of SAGNAC comprises a coil of optical fiber, preferably monomode and polarization conservation.
    [0018] This optical fiber coil here has a length of 1 kilometer so that the ring 141 of SAGNAC has a natural frequency fp = 103.45 kHz. Advantageously, and as shown only in FIG. 1, the measurement interferometer 140 comprises a multifunction optical circuit 142 comprising an electro-optical substrate 146, an integrated optical junction 144 in the shape of a Y, also called a "Y junction". An integrated polarizer 145 disposed on the base of the Y junction 144, and two pairs of modulation electrodes 143 each placed on a branch 144A, 144B of the Y junction 144, these modulation electrodes 143 forming said modulator of the measurement interferometer 140.
    [0019] Indeed, when modulation voltages are applied across each of these two pairs of modulation electrodes 143, a modulated electric field appears in the electro-optical substrate 146 of the optical circuit 142 which will modulate the optical phase of the light signals. through the optical circuit 142. The measurement interferometer 140: receives as input an input light signal, represented here by a double arrow and referenced by the reference sign Sul (see FIGS. 1 to 8), and produces an output light output signal, also represented by a double arrow and referenced by the reference sign SouT1 (see Figures 1 to 8). The different light signals can flow on the different channels 101, 102, 103, 104 of the device 100; 200; 300; 400 according to different propagation directions. Also, for the sake of clarity, it has been indicated in the drawings, for each light signal, the direction of propagation of the light signal considered on a channel 101, 102, 103, 104 by means of a small arrow substantially parallel to said channel 101 , 102, 103, 104. Thus, in the drawings, the input light signal Sul propagates on the measurement channel 102 here from left to right and the output light signal is propagated on the measuring channel 102 from right to left. left. Preferably, this measurement path 102 is formed of a polarization-maintaining optical fiber section. The input light signal Sul has an input light power, denoted PIN, and the output light signal Sour1 has an output light power, denoted For. In conventional manner, the output light power For the output signal light Sour1 depends on the physical parameter s2R to be measured and is proportional to the input luminous power PIN of the input light signal Sul. The Souri output light signal is advantageously modulated at a modulation frequency f, thanks to the phase modulator 143 of the measurement interferometer 140. This modulation is made desirable in order to improve the signal-to-noise ratio of the measurement made by the In practice, the modulation of the output light signal Sour1 corresponds to a modulation of the output light power. Advantageously, it is known that the modulation frequency fm may be an odd multiple of the frequency. own of the SAGNAC ring 141 of the measurement interferometer 140. In the following, it will be considered that the modulation frequency fm of the output light signal Sour1 is equal to the natural frequency fp of the measurement interferometer 140, either: fm = fp = 103.45 kHz for a 1 km optical fiber coil. Furthermore, by passing through the optical circuit 142, the Souri output light signal produced by the measurement interferometer 140 is polarized linearly in a first polarization direction (see for example H. Lefèvre, "The Fiber-Optic Gyroscope", Artech House, 1993 - Appendix 3) thanks to the integrated polarizer 145 placed at the input / output of the optical circuit 142. In this description and the associated figures, this first polarization direction (referenced by the sign II) is here oriented in a parallel plane on the plane of the ring 141 of Sagnac.
    [0020] In practice, whatever the polarization direction of the input light signal SIN, II, the Souri output light signal will always be polarized according to this first polarization direction. It will be seen in the remainder of the description that this property of the phase modulator 142 can advantageously be used for the realization of the device 100; 200; 300; 400 of interferometric measurement according to the invention. The spontaneous emission light source 110 of the device 100, 200, 300, 400 is, in general, a source which is not a priori polarized, so that the source light signal emitted by the light source 110 is unpolarized. . It is known that the source light signal can then be decomposed into any two components having orthogonal polarization states: for example two rectilinear cross components, that is to say perpendicular to each other or two circular components, one circular right and the other left circular. To aid understanding, as shown in FIGS. 5 to 8 for the fourth, fifth, sixth and seventh embodiments in which the light source 110 is unpolarized, the source light signal S1, S'1, ± is decomposed into a parallel component Si whose linear polarization is aligned according to the first direction of polarization (here called "parallel" direction), and a perpendicular component S'1, whose linear polarization is aligned in a second direction of polarization ( here said "perpendicular" direction) which is crossed, that is to say perpendicular to the first direction of polarization. In the remainder of the description, it will be possible, for these particular embodiments, to assimilate the source light signal to its two components Sil, S'1, ± of linear polarization. It will be seen moreover that, for these particular embodiments, the parallel component S1 of the source light signal is the component which is used in the measurement interferometer 140, whereas the perpendicular component S'1, ± of the source light signal is not exploited by the measurement interferometer 140. Conversely, in the first, second and third embodiments shown in Figures 1 to 4, the source light signal is polarized.
    [0021] This source light signal can be polarized either because the light source of the interferometric measuring device is intrinsically a polarized source, or by using an optical component for linearly polarizing the source light signal emitted by a non-polarized light source. In the first, second and third embodiments shown in FIGS. 1 to 4, here we are in the second case, and the device 100; 200 interferometric measurement comprises a linear polarizer 111 which is placed downstream of the light source 110 for biasing the source light signal in the first direction of polarization. In practice, the axis of the linear polarizer 111 can be aligned with this first polarization direction during a calibration operation of the light source 110. Thus, at the output of the linear polarizer 111, the source light signal has only one only rectilinear component, namely the parallel component Sil, to which we can assimilate the source light signal. To couple the light source 110 with the measurement interferometer 140, the device 100; 200; 300; 400 also comprises optical coupling means 120; 220; 320; 420 (see FIGS. 1 to 8). These optical coupling means 120; 220; 320; 420, whose various configurations will be described in detail in the following description, are connected to the light source 110 via the source channel 101 so as to receive the source light signal Sil; Si, S'1, ± emitted by the light source 110. The optical coupling means 120; 220; 320; 420 are also connected to the measurement interferometer 140 via the measurement path 102 so as to direct at least a portion of the source light signal Sil; Sil, S'1, ± received via the source channel 101 to the measurement channel 102.
    [0022] In the case where the source light signal S1 emitted by the light source 110 is polarized according to the first polarization direction by virtue of the linear polarizer 111 (in the case of the 1st, 2nd and 3rd embodiments, see FIGS. 1 to 4), the part of the source light signal S1 redirected to the measurement path 102 by the optical coupling means 120; 220 comprises a single component 521 rectilinear same polarization direction as the source light signal S1,11. In the case where the source light signal S1, S'1, ± emitted by the light source 110 is unpolarized (case of the 4th 5th heme and 7th embodiments, see FIGS. 5 to 8), the part of the source light signal Si, S'1, ± redirected to the measurement path 102 by the optical coupling means 320; 420 comprises two rectilinear components S21, S'2,1 whose polarization directions are respectively aligned with the directions of polarization of the rectilinear components Sil, S'1, ± of the source light signal, that is to say according to the first polarization direction and the second polarization direction. As shown in FIGS. 1 to 7, the optical coupling means 120; 220; 320; 420 are moreover connected to a third channel of said device 100; 200; 300; 400, said compensation path 103, separate from the measurement path 102 including the measurement interferometer 140, so as to take another part of the source light signal Sil; S1, ± to this compensation channel 103. In all the embodiments shown in Figures 1 to 8, this compensation channel 103 is preferably formed by a polarization-maintaining optical fiber section. In the case where the source light signal S1 emitted by the light source 110 is polarized according to the first polarization direction by virtue of the linear polarizer 111 (in the case of the 1st, 2nd and 3rd embodiments, see FIGS. 1 to 4), the part of the source light signal Sil taken to the compensation channel 103 by the optical coupling means 120; 220 comprises a single rectilinear component 53,11 of the same direction of polarization as the source light signal Sil. In the case where the source light signal S1, S'1, ± emitted by the light source 110 is unpolarized (case of the 4th 5th heme and 7th embodiments, see FIGS. 5 to 8), the part of the source light signal Si, S'1, ± taken to the compensation path 103 by the optical coupling means 320; 420 comprises two components S31, S'3, ± rectilinear whose directions of polarization are respectively aligned with the directions of polarization of the rectilinear components Sil, S'1, ± of the source light signal, that is to say according to the first polarization direction and the second polarization direction. From this other part S31; S31, S'3'L of the source light signal Sil; S ,, II S'i, ± taken and transmitted in the compensation path 103, it produces a compensation light signal Sp, ± having a return light power PRET- This compensating light signal SprL is then re-couple on the measurement path 102 by means of optical loopback of the compensating channel 103, the structure of which will be detailed below for the various embodiments of the invention and their variants.
    [0023] In this way, the compensation light signal SR, ± and the output light signal Sour, 11 flow together in the same direction of propagation on the measurement path 102, towards the optical coupling means 120; 220; 320; 420 of the device 100; 200; 300; 400. These optical coupling means 120; 220; 320; 420, connected to a fourth channel of said device 100; 200; 300; 400, here called detection channel 104 then allow the output light signal Soull and the compensation light signal SR, ± to be directed together with detection means 150 placed at the end of the detection channel 104 (see FIGS. 8). In all the embodiments shown in FIGS. 1 to 8, this detection channel 104 is formed by a section of polarization-maintaining optical fiber or an ordinary monomode fiber. In both cases, the For and FRET powers maintain orthogonal polarizations. In a conventional manner, these detection means deliver an electrical signal 151 (see FIG. 1) which is representative of the result of the measurement of the physical parameter s2R to which the measurement interferometer 140 is sensitive. This electrical signal is then transmitted to means 160, which process it to provide, on the one hand, the measurement of the physical parameter s2R, and, on the other hand, to control the phase modulator 143 as a function of this measurement (see arrow between the means of processing and electrical control 160 and the modulator 143 in Figure 1). More precisely, the electrical processing and control means 160 operate, by demodulation, the modulated electrical signal 151 delivered by the detection means 150 in order to determine the s2R component of the rotational speed of the measurement interferometer 140. Without precautions particular, the electrical signal 151 delivered by the detection means 150 is noisy, because not only of the photonic noise, but especially of the excess intensity noise which are present in the output signal Souri coming out of the measurement interferometer 140, so that the measurement of the physical parameter s2R to be measured is not very precise. Thus, it is one of the objectives of the invention to propose an interferometric measuring device in which the effect of the relative intensity noise RIN of the light source 110 on the measurement of the physical parameter s2R to be measured is reduced. , if not eliminated. It is another object of the invention to provide such an interferometric measuring device that is easy to implement. For this purpose, according to the invention, it is provided that: the compensation path 103 comprises polarization rotation means 131; 231; 331; 431 for producing the compensation light signal Sp, i in the second polarization direction crossed with the first polarization direction, and optical loopback means 132; 134; 234; 334; 434 of the compensation path 103 on said measurement path 102, these optical loopback means 132; 134; 234; 334; 434 receiving the compensation light signal Sp, ± circulating on the compensation path 103 and redirecting at least a portion of the compensation light signal Sp i to the measurement path 102, the detection means 150 comprise a single optical radiation detector , for example here a semiconductor PIN photodiode, connected to the optical coupling means 120; 220; 320; 420 receiving the Sourl output light signal and the compensation light signal SR, i, which flow on the measurement path 102, to route them to said detector (150), the device 100; 200; 300; 400 further comprises power balancing means 132; 121, 133; 222; 223; 233, 321, 333; 321, 322; 422 correcting the output light power For and / or said return light FRET power directed to the detector 150 so that the return light power READY is substantially equal to the output light power For this detector 150, and - said compensation channel 103 has a length adjusted so that the output light signal Sour1 has at the detector 150 a time delay i relative to the compensation light signal SR, i substantially equal to 1 / (2 * fp). In order to better understand the advantages and the operation of such an interferometric measuring device, the first embodiment of the interferometric measurement device 100 according to the invention shown in FIG. 1 will now be described in detail. FIRST EMBODIMENT In FIG. this first embodiment, the optical coupling means 120 (see dashed lines in FIG. 1) comprise a first coupler 121 two by two (again denoted "2 x 2") with four ports 121A, 121B, 121C, 121D. This first coupler is conventionally characterized by its transmission coefficient, noted here T1, which is between 0 and 1 (T, = 0 corresponding to a transmission of 0% and 1 to a transmission of 100%), and its coupling coefficient , noted here Cl, which is between 0 and 1 (C, = 0 corresponding to a coupling of 0% and 1 coupling of 100%). In general, this type of coupler has very low losses, so that the transmission coefficient Ti and the coupling coefficient C1 are simply connected by the relation Cl = 1-T1. For example, a 2 × 2 coupler of the 50/50 type is a coupler such that Ti = 0.5 (50% of transmission) and Cl = 1-0.5 = 0.5 (50% of coupling). As shown in FIG. 1, the first coupler 121 is such that: the first port 121A, connected to the source channel 101, receives the source light signal Sil polarized in the first direction of polarization (parallel direction) - the second port 121 B, connected to the measurement path 102, transmits the portion 521 of the source light signal S1 to the measurement path 102, with a transmission factor equal to T1 .- the third port 121C, connected to the compensation path 103, torque the other part S31 of the source light signal Sil on the compensation channel 103 with a coupling factor equal to Cl, and the fourth port 121D, connected to the detection channel 104 couples the light output signal and the light signal of compensation SR, ± on the detection channel 103, with the same coupling factor equal to Cl. The other part S31 of the source light signal Sil coupled on the compensation channel 103 is, as the light source signal polarized selo n the first direction of polarization. Thanks to the polarization rotation means 131 disposed on the compensation path 103, the polarization direction is rotated by 90 ° so as to generate said compensation light signal SR, which is linearly polarized in the second cross polarization direction, 90 ° of the prerrière direction of polarization. Advantageously, the polarization rotation means comprise the optical fiber portion of the compensation channel 103 which is between the third port 121C of the first coupler 121, polarization-maintaining fiber portion of the optical fiber. in English or PM fiber) can be bent 90 ° between its two ends so as to obtain this rotation of the polarization. The compensation light signal Sp, ± then propagates along the compensation path 103 while maintaining its polarization until reaching the optical loopback means 132 of the compensation path 103 on the measurement path 102. These coupling means comprise in this first embodiment a second four-port two-by-two coupler 132, having a transmission coefficient T2 and a coupling coefficient O 2, defined in the same way as for the first coupler 131. Thanks to this second coupler 132, the compensation light signal SprL flowing on the compensating channel 103 is partially redirected to the measuring path 102, the coupled proportion depending on the coupling coefficient C2 of the second coupler 132. In the same way, the output light signal Soul1 coming from the measurement interferometer 140 and traveling on the measuring path 102 is transmitted by the second coupler 132 as a function of its drag coefficient. Transmission 12. The optical "loopback" of the compensation channel 103 on the measurement path 102 is here essential to the implementation of the invention. Thanks to it, it is possible to use detection means which comprise a single detector 150. Indeed, after passing through the second coupler 132, the output light signal Soull and the compensation light signal SprL propagate until at the second port 121B of the first coupler 121 which then carry these signals, by coupling on the detection channel 104 with a coupling coefficient equal to Cl up to the detector 150.
    [0024] Furthermore, in the device 100 according to the invention, the length of the compensation channel 103 is adjusted so that the output light signal Sour1 has, at the detector 150, a time delay i with respect to the compensation light signal. SprL. That is, according to the invention substantially equal to 1 / (2 * fp), fp thus being the natural frequency of the ring 141 of Sagnac.
    [0025] This time delay i corresponds to the difference in propagation time, between the light source 110 and the detector 150, between the light signal passed by the measurement interferometer 140 and the light signal passed through the compensation channel 103. We will now express, at any instant t, the output light power For and the FRET return light power arriving at the detector, as a function of the source light power P. It will first be noted that this source luminous power Ps fluctuates over time because of the excess intensity noise of the light source 110, so that the source light power Ps can be written in the following form: Ps (t) = <Ps> * [1 + B (t)], where the term <Pu> represents the average source light power and the term B (t) represents the relative intensity noise in excess of the light source 110, having a power spectral density or "noise power" BRIN (see introduction ). For the compensation light signal SR, ±, which is derived from the source light signal S1,11 coupled in the compensating channel 103 by the first coupler 131, then rotated by 90 °, then looped back on the measurement path 102 by the second coupler 132 and finally redirected to the detector 150 via the first coupler 131, it is possible to express the return light power PRET in the form: READY (t) = ar * Ps (t) * C1 * C2 * C1 = ar * <Ps> 1 1 + B (t)] * C12 * C2, the coefficient ar representing a generic term accounting for the different optical losses occurring on the optical path of the compensation light signal SR, ±. In the same manner, for the Souri output light signal, which is derived from the source light signal S1 coupled in the measurement path 102 by the first coupler 131, then passes into the measurement interferometer 140 to exit on the measurement path 102 and is finally redirected to the detector 150 via the first coupler 131, it is possible to express the output luminous power For in the form: For (t) = am * Ps (tt) * T1 * T22 * C1 = am * <Ps > * [1 + B (t- 'O] * T1 * T22 * C1, the coefficient am representing a generic term accounting not only for the different optical losses occurring on the optical path of the output light signal Sour, 11, but also , and especially of the response of the measurement interferometer 140, this response being able to vary as a function of the modulation depth at the bias slot, thus, since the output light signal Soul1 and the compensation light signal are respectively polarized. according to first and second direction These two signals are added in power without any interference effect at the detector 150, so that the detected light power PD (t) received by the detector 150 at the instant t is equal to the sum PRET (t) + PouT (t) of the return light power READY (t) and the output light power PouT (t), again: PD (t) = READY (t) + For t). This detected light power PD (t) can be written in the form: PD (t) = <PD> * [1 + BD (t)], where the term <PD> corresponds to the mean light power detected, free from noise, and where the term BD (t) corresponds to the noisy part of the detected light power PD (t), notably accounting for the noise RIN. Thus, to reduce the effect of the excess intensity relative noise (INR) of the light source 110, it is understood that the noise portion BD (t) must be as low as possible.
    [0026] Using the mathematical expressions given above for the output light power PouT (t) and the luminous power return READY (t), the noisy part BD (t) can be expressed as: BD (t) = ar * <Ps> * B (t) * C12 * C2 + am * <Ps> * B (t- t) * T1 * T22 * C1, ie = <Ps> * C1 * [ar * (1 -T,) * (1 -T2) * B (t) + am * T1 * T22 * B (t- t)], with Cl = 1-T1 and 02 = 1 -T2. At this stage, for the sake of understanding, it will be considered for example that the optical losses for the compensating light signal are negligible, that is to say that the coefficient ar can be approximated to 1. In this case, if one considers for example that the coefficient a, is typically equal to 0.01, corresponding to -20 dB of losses in the measurement interferometer 140 because of the coupling losses of the modulator 141, the ring 141 of Sagnac and the modulation depth of the modulator 141, then we can calculate that if Ti = 0.5 (ie C, = 1-T1 = 0.5 or 50%) and T2 = 0.99 (ie 02 = 1-T2 = 0, 01, ie 1%), then the output light power PouT and the return light power READY are substantially equal at the level of the detector 150, so that the noisy part BD (t) detected is equal to: BD (t) (1 / 400) * <Ps> * [B (t) + B (tT)]. In general, it will be understood that it is possible to equalize the return light power READ with the output light power PouT at the detector 150 by suitably adjusting the transmission coefficients T1, 12, respectively the coupling coefficients C1, C2 the first coupler 131 and the second coupler 132 of the device 100. In other words, the first coupler 131 and the second coupler 132 form here the power balancing means correcting the output light power PouT and the return light power. READY routed to the detector 150. As according to the invention, the length of the compensation channel 103 is adjusted so that the time delay ti between the output light signal Soull and the compensation light signal SR, ± is substantially equal to 1 / (2 * fp), the frequency spectrum of the noise power received by the detector 150 has a low value, or even zero if the light powers PRET, 'DOW- are perfectly equalized, for all the frequencies which are odd multiples of 1 / (2 * T), i.e., odd multiples of the natural frequency fp of the measurement interferometer 140 (i.e. fp, 3 * fp, 5 * fp, etc ...). In other words, by substantially equalizing the output light power PouT and the return light power READY and by adjusting the time delay between the output light signal and the cross polarization compensation light signal, it is possible to reduce or even to eliminate the effect of the excess intensity noise of the light source 110 on the measurement of the parameter 5-2R to be measured, the demodulation of the electrical signal 151 delivered by the detector 150 by means of processing and electrical control means 160 being precisely at the modulation frequency f, the phase modulator, which is an odd multiple of the natural frequency fp of the measurement interferometer 140. We will now describe the various other embodiments of a device 100; 200; 300; 400 of the invention shown in Figures 2 to 8 which operate according to the same principle. SECOND EMBODIMENT FIG. 2 shows, for example, a device 100 which differs from the first embodiment in that the optical loopback means here comprise a polarization separator 134 placed at the junction between the compensation channel 103 and the measuring path 102.
    [0027] This polarization separator 134 functions here rather as a polarization combiner towards the measurement path 102: it transmits, on the one hand, the output light signal Sour1, polarized according to the first polarization direction and issuing from the measurement interferometer 140 , and it redirects, on the other hand, the compensation light signal SR, i, polarized in the second direction of polarization and coming from the compensation channel 103. This polarization separator 134 may for example be formed by a separator cube of polarization well known to those skilled in the art. Since this type of polarization separator 134 generally has substantially identical transmission and coupling coefficients, it is advantageous to use an optical attenuator 133 making it possible to lower the return light power READY of the compensation light signal SR, ±. Preferably, this optical attenuator 133 is placed on the compensation path 103 between the polarization rotation means 131 and the polarization separator 134. THIRD EMBODIMENT In a third embodiment shown in FIG. 3, the coupling means optical 220 comprise here, in addition to the first coupler 222, an optical circulator 221 placed upstream of this first coupler 222 which has three ports respectively connected to the light source 110, to one of the ports of said first coupler 222 and the detector 150 In this configuration, the power balancing means then comprise the first coupler 222 by which, by adjusting the transmission coefficient Ti and the coupling coefficient C1, it is possible to substantially equalize the output light power For and the return power READY at the detector 150. For example, by taking the numerical values of the example of the first embodiment for ar and am, then a transmission coefficient Ti is equal to 0.99 for the first coupler 222. VARIANT OF THE THIRD EMBODIMENT In a variant of the third embodiment shown in FIG. to use a first coupler 223 having Ti transmission and Cl coupling coefficients close to 0.5. In this case, it is then preferable to add an optical attenuator 233 on the compensation path 103 or on the measurement path 102 in order to correct the return light power READY of the compensation light signal. FOURTH, FIFTH, SIXTH AND SEVENTH EMBODIMENT In the fourth, fifth, sixth and seventh embodiments respectively shown in FIGS. 5 to 8, it has been seen that the light source 110 of the device 300; 400 interferometric measurement was unpolarized and emitted a source light signal that can decompose according to two components Sil, S'1, ± orthogonal. So that only the output signal Sourl polarized in the first polarization direction and the compensation light signal SR, ± biased in the second cross polarization direction reach the detector 150 of the device 300; 400, the compensation channel 103 comprises an optical isolator 332; 432 for the second polarization direction and the optical loopback means comprises a polarization splitter 334; 434. In order to understand the advantages of such a configuration when the light source 110 is not polarized, the path of the different light signals in the interferometric measurement device 300 for the fourth embodiment will be described in detail. FOURTH EMBODIMENT Thus, as shown in FIG. 5, the first coupler 321 of the optical coupling means 320 of the device, on the one hand, directs or transmits the source light signal Sil, S'irL to the measurement path 102 according to FIG. the two components S21, S'2,1 rectilinear, and, on the other hand, draws or couples the same luminous signal Sil, S'irL to the compensation path 103 according to the two components S31, S'3, ± rectilinear. Concerning the components 521 and S31, these flow in the device 300 in the same way as if the light source 110 was polarized according to the first polarization direction. In particular, it is these two components 521 and S31 which give rise respectively to the Sourl output light signal and to the compensation light signal. SR ±. Thus, for these two components 52, 11 and S31, everything happens as for the first three embodiments. In particular, the optical isolator 332 being oriented in the propagation direction of the compensation light signal SprL, it does not block it. For the other two components S'2, ± and S'3, ±, derived from the component S'1, ± of the source light signal polarized according to the second polarization direction, the behavior is different. On the one hand, the perpendicular component S'2'L propagating on the measurement path 102 is first coupled on the compensation path 103 by means of the polarization separator 334 so that this perpendicular component S'2, ± propagates on the compensation path 103 in a direction opposite to the compensation light signal Sp i. This perpendicular component S'2'L is then blocked by the optical isolator 332, so that it can not be redirected towards the detector thanks to the first coupler 321.
    [0028] On the other hand, the perpendicular component S'3'L propagating on the compensation path 103 is first rotated by means of polarization rotation means 331 so as to produce a parallel component S'31 propagating on the compensation channel 103 in the same direction as the compensation light signal Sp, i. Not being blocked by the optical isolator 332, this parallel component S'31 arrives on the polarization separator 334 which does not cross it on the measurement path 102 since its polarization direction is oriented in the first direction of polarization. Thus, this parallel component S'31 can not reach the detector 150. In other words, it can be said that: - for the parallel polarization direction light source signal S1, 11, the interferometric measurement device 300 operates as for the previously described devices (see FIGS. 1 to 4), and for the source light signal S'1, perpendicular direction of polarization direction, the interferometric measuring device 300 functions as a filter for this polarization, so that no light signal from this perpendicular component S'1 ± circulating in the device 300 reaches the detector 150. Also, the explanations given for the equalization of the return light power READY with the output light power For and for the time delay ti between the output light signal SUL1 and the compensation light signal SprL remain valid in the case of a device 300 designed for a light source 110 not p olarisée. In particular, it will be noted that the device 300 of FIG. 4, which also comprises an optical attenuator 333, differs only from the device of FIG. 2 in that it comprises the optical isolator 332.
    [0029] Thus, with the difference that the losses introduced by the optical isolator 332 on the compensation light signal SprL, the values of the transmission coefficient Ti and of the coupling coefficient C1 of the first coupler 321 are identical. Alternatively, the polarization splitter could be replaced by another two by two four-port coupler and a linear polarizer oriented in the compensation path would be provided to block the propagation of the parallel component S'31 to that other coupler. FIFTH EMBODIMENT In a fifth embodiment shown in FIG. 6, the optical coupling means 320 of the device 300 further comprise a second two-to-four pair coupler 322, this second coupler 322 forming part of the balancing means. power. Advantageously, the first coupler 321 may be an optical coupler of the low polarization dependence type, having for each of the crossed polarizations a transmission coefficient of 50% and a coupling coefficient close to 50%. In this case, it is then possible to adjust the REW and RE output light powers thanks to the second coupler 322. SIXTH EMBODIMENT In a sixth embodiment shown in FIG. 7, instead of using two optical couplers 321, 322, as in the fifth embodiment (see FIG. 6), provision can be made to use a first coupler 422 in combination with an optical circulator 421 placed upstream of the first coupler 422, this optical circulator 421 having three connected ports respectively to the light source 110, to one of the ports of the first coupler 422, and to the detector (150). In this embodiment, it is then possible to balance the light powers by adjusting the transmission and coupling coefficients of the first coupler 422.
    [0030] SEVENTH EMBODIMENT In a seventh embodiment shown in FIG. 8, similar to the sixth embodiment of FIG. 7, the device 400 is such that the polarization separator 434 and the first coupler 422 have been changed in position. polarization separator 434 is now placed between the optical circulator 421 and the first coupler 422. Despite this reversal, the device 400 of this seventh embodiment operates as the previous. In all embodiments of the device 100; 200; 300; 400 interferometric measurement shown in Figures 1 to 8, can advantageously operate the device 100; 200; 300; 400 closed loop (see for example H. Lefèvre, "The Fiber-Optic Gyroscope", Artech House, 1993 - Chapter 8). In this case, it will then be possible to correct the output light power For output light signal S01 out of the measurement interferometer 140 by changing the modulation depth with the phase modulator 143 and the processing and control means Electrical control 160 controlling this modulator 143. For this, we choose a wavelength modulation bias that does not degrade the photonic noise on the detector 150, for example with a biasing phase shift (usually denoted Ob) between ± 3n / 4 and ± 7n / 8. This allows a fine adjustment of the balancing of the output light pulses PouT and P RET return electronically, through the modulator 143 and the processing and electrical control means 160. In general, one can combine these balancing means "Electronic" with "optical" balancing means, such as an attenuator or a coupler, which allow a first rough adjustment of power balancing.
    [0031] Moreover, when the power balancing means comprise the modulator and the electrical control and control means, it is possible to compensate for the drift in time of the return power For the measurement interferometer by modifying the value of the phase shift (Pb of slot modulation ± (Pb of bias).
    权利要求:
    Claims (15)
    [0001]
    REVENDICATIONS1. Interferometric measurement device (100; 200; 300; 400) of a parameter (sep) to be measured comprising: a broad-spectrum spontaneous emission light source (110) emitting a source light signal (S1,11; detector (150) providing an electrical signal representative of the result of a measurement of said parameter (np) to be measured, - electrical processing and control means (160) processing said electrical signal to provide said measurement of said parameter (sep) to measuring, and - optical coupling means (120; 220; 320; 420): receiving said source light signal (S1,11, S'1, ±), directing a portion (S21, S'2, ±) at least said source light signal (S1,11, S'1, ±) to a measurement channel (102) comprising a measurement interferometer (140) which comprises a phase modulator (143) and a Sagnac ring (141), own frequency fp, responsive to said parameter (sep) to be measured, said interferometer receiving, as input, a read signal light input (Sul) of input light power (P, n) and producing, at the output, a light output signal (Sourl) of output light power (Pour) dependent on said physical parameter (sep) to be measured and proportional to said input light power (P ,,), said output light signal (Sour1) being biased in a first polarization direction and modulated at a modulation frequency f, by said phase modulator (143), sampling a another portion (S31, S'3, ±) of said source light signal (Sil, S'1, ±) to a compensation channel (103) separate from said measurement path (102), said compensation path (103) generating a compensation light signal (SR, ±) having a return light power (P RET) directing said output light signal (Sun1) and said compensation light signal (SR, ±) to said detection means (150), characterized in what: said compensation channel (103) comprises: means for polarization rotation (131) adapted to produce said compensation light signal (SR, ±) in a second polarization direction crossed with said first polarization direction, and optical loopback means (132; 134; 234; 334; 434) of said compensation path (103) on said measuring path (102), said optical feedback means (132; 134; 234; 334; 434) receiving said compensation light signal (SR, ±) flowing on said path compensating (103) and redirecting at least a portion of said compensating light signal (SR, ±) to said measurement path (102), said detecting means (150) comprises a single optical radiation detector (150) connected to said optical coupling means (120; 220; 320; 420), said optical coupling means (120; 220; 320; 420) receiving said output light signal (Sour, ") and said compensation light signal (SR, ±); circulating on said measurement path (102) for routing to said detector (150), said device (100; 200; 300; 400) further comprises power balancing means (132; 121,133). ; 222; 223; 233; 321,333; 321,322; 422) correcting said output light power (For) and / or said return light power (PRET) 1 conveyed to said detector (150) such that said return light power (PRET) is substantially equal to said output light power (For) at said detector (150), and - said compensation channel (103) has a length adjusted so that said output light signal (Sour ") has at the detector (150) a time delay with respect to said compensation light signal (SR, ±) substantially equal to 1 / ( 2 * fp).
    [0002]
    An interferometric measurement device (100; 200) according to claim 1, further comprising a linear polarizer (111) downstream of said light source (110) for biasing said source light signal (S11) in said first polarization direction .
    [0003]
    An interferometric measurement device (100; 200) according to claim 2, wherein said optical coupling means (120; 220) comprises a first two-to-four port coupler (121; 222; 223).
    [0004]
    An interferometer measuring device (200) according to claim 3, wherein said optical coupling means (220) comprises an optical circulator (221) located upstream of said first coupler (222; 223), said optical circulator (221) having three ports respectively connected to said light source (110), to one of said first coupler ports (222; 223), and to said detector (150).
    [0005]
    5. interferometric measuring device (100) according to one of claims 3 and 4, wherein said optical loopback means comprises a second coupler (132) two by two to four ports, said power balancing means also comprising said second coupler (132).
    [0006]
    The interferometric measurement device (100; 200) according to one of claims 3 and 4, wherein said optical loopback means comprises a polarization splitter (134; 234).
    [0007]
    An interferometric measurement device (100; 200) according to one of claims 5 and 6, wherein said power balancing means comprises an optical attenuator (133; 233) for a polarized light signal (S3 ±) according to said second polarization direction so as to correct said return light power (13 'RET) -
    [0008]
    Interferometer measuring device (300; 400) according to claim 1, designed for a light source (110) emitting an unpolarized light source signal (S1, 11, S'1, ±), in which: compensation (103) comprises an optical isolator (332; 432) for blocking a polarized light signal (S'2, ±) in the second polarization direction propagating on said compensation path (103) in the opposite direction of said light signal of compensation (SR, ±), and said optical loopback means comprises a polarization splitter (334; 434).
    [0009]
    An interferometric measurement device (300; 400) according to claim 8, wherein said optical coupling means (320; 420) comprises a first four-port two-by-two coupler (321; 422).
    [0010]
    10. Interferometric measuring device (400) according to claim 9, wherein: said optical coupling means (420) comprise an optical circulator (421) placed upstream of said first coupler (321; 422), said optical circulator (421); ) having three ports respectively connected to said light source (110), to one of said first coupler ports (321; 422), and to said detector (150), and said power balancing means includes said first coupler (321; 422).
    [0011]
    The interferometric measurement device (300) according to claim 9, wherein: said optical coupling means (320) further comprises a second two-to-four port dual coupler (322), and said power balancing means comprise said second coupler (322).
    [0012]
    An interferometric measuring device (300) according to one of claims 8 to 11, wherein said power balancing means comprises an optical attenuator (333) for a polarized light signal (S3, ±) along said second direction of polarization so as to correct said return light power (P REL
    [0013]
    An interferometric measurement device (100) according to one of claims 1 to 12, wherein said power balancing means comprises said phase modulator (143) and said electrical control and control means (160) controlling said modulator (143) for correcting said output light power (For).
    [0014]
    14. Gyrometer comprising an interferometric measuring device (100; 200; 300; 400) according to one of claims 1 to 13, said physical parameter (SIR) to be measured being a component of the speed of rotation of said gyrometer about its axis of rotation.
    [0015]
    15. Center of attitude or inertial navigation comprising at least one gyrometer according to claim 14.
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    同族专利:
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    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US5331404A|1992-11-30|1994-07-19|The United States Of America As Represented By The Secretary Of The Navy|Low noise fiber gyroscope system which includes excess noise subtraction|
    US20030081219A1|2001-10-31|2003-05-01|Bennett Sidney M.|Angle random walk noise reduction in fiber optic sensors using an optical preamplifier|
    EP2251641A1|2009-05-11|2010-11-17|Honeywell International Inc.|Systems and methods for effective relative intensity noise subtraction in depolarized gyros|
    US5469257A|1993-11-24|1995-11-21|Honeywell Inc.|Fiber optic gyroscope output noise reducer|
    US5898496A|1997-02-14|1999-04-27|Allied Signal Inc|Optical signal noise reduction for fiber optic gyroscopses|
    US6765678B2|2002-01-08|2004-07-20|Honeywell International Inc.|Relative intensity noise controller with maximum gain at frequencies at or above the bias modulation frequency or with second order feedback for fiber light sources|FR3023609B1|2014-07-08|2016-07-29|Ixblue|INTERFEROMETRIC SYSTEM WITH OPTICAL FIBER|
    WO2017138884A1|2016-02-12|2017-08-17|Agency For Science, Technology And Research|Optical gyroscope, electro-optic system, and methods of forming the same|
    FR3052859B1|2016-06-20|2018-11-23|Ixblue|MEASUREMENT SYSTEM AND GYROMETER COMPRISING SUCH A SYSTEM|
    US10415971B2|2018-01-15|2019-09-17|Honeywell International Inc.|Apparatus and method for diminished bias error due to polarization mismatch|
    CN109099899B|2018-09-15|2020-06-09|西安奇芯光电科技有限公司|Passive bias optical gyroscope|
    US10731988B1|2019-07-10|2020-08-04|Anello Photonics, Inc.|System architecture for integrated photonics optical gyroscopes|
    RU2743815C1|2020-03-24|2021-02-26|Акционерное общество "Центр эксплуатации объектов наземной космической инфраструктуры"|Ring interferometer of fiber optical gyroscope|
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    CN113739782B|2021-11-03|2022-03-01|华中光电技术研究所（中国船舶重工集团公司第七一七研究所）|Fiber-optic gyroscope closed-loop control method and system, electronic equipment and storage medium|
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    FR1451543A|FR3017945B1|2014-02-26|2014-02-26|INTERFEROMETRIC MEASURING DEVICE|FR1451543A| FR3017945B1|2014-02-26|2014-02-26|INTERFEROMETRIC MEASURING DEVICE|
    PCT/FR2015/050464| WO2015128588A1|2014-02-26|2015-02-26|Interferometric measurement device|
    EP15713202.8A| EP3111167B1|2014-02-26|2015-02-26|Interferometric measurement device|
    US15/121,620| US9945670B2|2014-02-26|2015-02-26|Interferometric measurement device|
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