Interference sensor and method of measuring a physical quantity using such an interference sensor.

0001The present invention relates to an interference sensor for measuring a physical quantity. It is particularly, but not exclusively, concerned with an interference sensor being an optical gyroscope.

0002It is well known to measure a physical quantity using a sensor in which two beams of light, or other radiation, are caused to interfere, with that interference being dependent on the physical quantity to be measured. Thus, optical gyroscopes are known in which two beams of light are caused to propagate in opposite directions through a loop of optical fibre. The two light beams will interfere when they emerge in opposite directions from the loop, and are caused to follow the same optical path. When the loop rotates, the propagation path lengths of the two light beams are changed, so that there is a change in the interference between the light beams. The rotational angular velocity can then be determined on the basis of changes in the phase difference between the interfering light beams.

0003There are two known systems for measuring the change in the phase of the interference. The first known system is known as the "closed loop" type, in which the loop contains additional means for varying the phase of the beams to maintain a constant phase difference therebetween. The detector, which detects the interfering beams, therefore detects a substantially constant phase difference, and the phase difference caused by rotation of the loop of the optical gyroscope is determined from the degree of adjustment needed within the loop itself.

0004The second system, known as the "open loop" type, directly detects changes in the phase difference between the interferring beams. The present invention is primarily concerned with this latter system.

0005It is also known to introduce an optical modulator into the optical system of the interference sensor, and to analyse changes in phase on the basis of that modulation. Various modulation systems are known, of which one type is phase modulation. Examples of such phase modulation is shown in US 4545682, US 4634282, US 4645345, US 4687330, US 4707136, US 4728192, US 4765739, and Electronics Letter (19) (1983) pages 997 to 999.

0006The present invention seeks to provide an interference sensor in which the interference signal from optically phase modulated interferring radiation beams is analysed, in a way which permits such analysis to be carried out rapidly.

0007In a first aspect, a Fourier line spectrum of the electronic interference signal measured by the detector receiving the interfering radiation beams is obtained, and one or more lines of that spectrum compared with a sampling frequency at which the electronic interference signal is sampled. The comparison is on the basis of a frequency component corresponding to a difference relationship between the frequency of the one or more lines of the Fourier line spectrum and the sampling frequency. The present invention is concerned with an interference sensor according to the first aspect, an electronic analyser for such an interference sensor, a vehicle control system incorporating such an interference sensor, and a method of measuring a physical quantity using such an interference sensor.

0008The first aspect of the present invention is concerned with a sampling technique. However, the inventors of the present application have realised that the effect achieved by such sampling can also be achieved by electronically modulating the electronic interference signal from the detector which detects the interfering radiation beams, so that the analyser operates by investigating a property of a frequency component corresponding to a different relationship between the frequency of at least one line of the Fourier line spectrum and the or each frequency of the electronic modulation, since it is possible to use an electronic modulation with more than one frequency component, such as a square wave, rather than a sinusoidal wave with a single frequency component. Such electronic modulation can be used in conjunction with sampling, but is an independent aspect of the present invention.

0009The inventors of the present application realised further that such electronic modulation was equivalent to optically phase modulating the interfering radiation beams by modulation at two frequencies. Then, a property of a frequency component corresponding to a difference relationship between the frequency of at least one line of the Fourier line spectrum and the frequencies of the two modulations is investigated. This is a third, independent, aspect of the present invention, although it may be combined with the first and/or second aspect.

0010In all such systems, and indeed all the interference sensors of which the applicants is aware, consideration has been given to the frequency of the electronic interference signal from the detector which detects the interfering radiation beams. The processing is thus in the "frequency domain". However, the applicants have further realised that it is possible to analyse the phase-modulated signal in the time-domain, i.e. independent of frequency. The value of a time-dependent feature of the electronic interference signal could then be obtained, such as the value of the peak-to-peak interval of the wave form, and variations in this value are directly related to changes in the interference relationship between the two beams. Thus, it is possible to measure a physical quantity on which those changes are based, by measurements in the time domain. This then represents a fourth independent aspect of the present invention, although time domain investigation may be combined with sampling, or addition electronic or optical modulation.

0011With the present invention, the physical quantity which determines the changes in the phase relationship between the interfering radiation beams can be measured rapidly. The present invention is therefore applicable to the control of a vehicle in which changes in the movement of that vehicle are detected, and the subsequent movement of the vehicle controlled on the basis of the movement already detected.

0012Embodiments of the present invention will now be described in detail, by way of example, with reference to the accompanying drawings in which: <ul id="ul0001" list-style="none"><li>Fig. 1 shows schematically the general construction of an interference sensor according to a first embodiment of the present invention;</li><li>Fig. 2 are graphs illustrating the processing which can be carried out in the first embodiment;</li><li>Fig. 3 is a detailed block diagram of an arithmetic processing circuit;</li><li>Fig. 4 shows a signal processing circuit, being part of a second embodiment of the present invention;</li><li>Fig. 5 shows a signal processing circuit, being part of a third embodiment of the present invention;</li><li>Fig. 6 shows a signal processing circuit, being part of a fourth embodiment of the present invention;</li><li>Fig. 7 is a graph showing processing which occurs in the fourth embodiment of the present invention;</li><li>Fig. 8 is a block diagram illustrating the production of reference signal frequencies;</li><li>Fig. 9 shows a signal processing circuit being part of a fifth embodiment of the present invention;</li><li>Fig. 10 shows an operating sequence which may be used in the present invention;</li><li>Fig. 11 shows a signal sampling operation which may be used in the present invention;</li><li>Fig. 12 is a diagram showing the application of the present invention to control the vehicle;</li><li>Fig. 13 is a schematic diagram of the general construction of an interference sensor, being a sixth embodiment of the present invention;</li><li>Fig. 14 is a schematic diagram of the general construction of an interference sensor, being a seventh embodiment of the present invention;</li><li>Fig. 15 is a schematic block diagram showing the general construction of an interference sensor, being an eighth embodiment of the present invention;</li><li>Fig. 16 is a waveform diagram showing the timing of signals in the eighth embodiment;</li><li>Fig. 17 illustrates the structure of the signal processing circuit used in the eighth embodiment of the present invention;</li><li>Fig. 18 is a waveform diagram showing the timing of signal in a ninth embodiment of the present invention;</li><li>Fig. 19 is a block diagram of a signal processing circuit, being part of the ninth embodiment of the present invention;</li><li>Fig. 20 is a block diagram of a signal processing circuit, being part of a tenth embodiment of the present invention;</li><li>Figs. 21 and 22 are waveform diagrams showing the timing of signals in the tenth embodiment of the present invention;</li><li>Fig. 23 is a block diagram showing a signal processing circuit, being part of an eleventh embodiment of the present invention; and</li><li>Fig. 24 is a block diagram of a signal processing circuit, being part of a twelfth embodiment of the present invention.</li></ul>

0013Before discussing embodiments of the present invention in detail, the general operation of an interference sensor, according to the present invention, will be discussed. As mentioned above, there are six different situations that need to be considered. Firstly, the present invention may operate in the frequency domain, in which case consideration is given to the frequency of the electronic interference signal of the detector. Then, when operating the frequency domain, there are three possibilities. Firstly, handling methods can be used in which the signal is sampled at a suitable sampling frequency. Preferably, this frequency is less than the frequency of the signal, and therefore such an arrangement is referred to as a "down sampling method". However, it is also possible to use sampling frequencies which are higher than the frequency of the signal being measured. Secondly, it is possible to add to the optical modulation of the beams a second optical modulation, such an arrangement will be referred to as "cross modulation". Thirdly, there is the possibility of adding an additional electronic modulation after detection of the interference beam, and such an arrangement will be referred to as "direct modulation". However, the present invention may alternatively operate in the time domain, in such cases it is again possible to use sampling methods, a method in which additional optical modulation is provided, and methods in which additional electron modulation is provided.

0014The time waveform or frequency spectrum of a modulated interference signal is determined by the property of a modulation input signal (the time waveform or the frequency spectrum) and the phase difference of the light beams. Where the modulation input signal is a periodic signal and where the phase difference of the light beams has a constant value, the interference signal becomes a regular periodic signal. In principle, the phase difference of the light beams, which is related to a physical quantity to be detected by the interference sensor, can be measured by subjecting the waveforem of one cycle of the interference signal to signal processing. However, when the interference signal is processed in real time, the sampling and arithmetic circuits of high speed are needed.

0015In the interference sensor for an optical fiber gyro etc., the phase difference of the light beams is a quantity fluctuating every moment, but it may normally be regarded as being a constant value, at least in the short term. For example, in an optical fiber gyro, the smoothing time of an output value is as long as several tens of msec. to several tens of sec. Consequently, in many applications of the optical fiber gyro, the light phase difference to be measured (herein, proportional to the angular velocity of rotation) may be considered to have a constant value for a period of time of several msec. to several tens of msec. This is evident when it is considered that the sudden changes in angular velocity are limited in a moving object such a aircraft or vehicle.

0016Assuming, for example, that the phase modulation signal of the optical fiber gyro is set at 20 kHz, it has a period of 50 µsec. Under the assumed condition that the light phase difference to be measured does not change for the period of time of several msec. or several tens msec., the waveform of the interference signal repeates a fixed shape over 100 or 1000 cycles. Therefore, when the interference signal waveform for such many cycles is to be handled, equivalent signal processing can be executed corresponding to a time signal whose period is extended. Accordingly, the requirements for the sampling frequency and the processing speed of the arithmetic circuit can be significantly reduced.

0017To obtain equivalent time (frequency domain) signal processing described above, a down sampling method can be used in which the interference signal is sampled at a frequency lower than a detection frequency. Further, when the equivalent time (frequency domain) interference signal waveform which is similar to the waveform of the interference signal in real time is composed using sampled values, the phase difference of the interference sensor is obtained from the equivalent time (frequency domain) interference signal. Alternatively, the phase difference can be obtained even when aliasing frequency components based on the sampling are extracted from the sampled values obtained by the down sampling method.

0018Alternatively, cross modulation methods may be used to achieve equivalent tone (frequency domain) signal processing. Cross modulation uses a first modulation signal and a second phase modulation signal, to which modulation signals are added. The optical phase modulator acting on the light beams is driven with the sum signal. Thus, the low frequency components of an interference signal frequency spectrum produced by cross modulation may be detected, and extracted, and the result processed in equivalent time (frequency domain).

0019The third alternative is to use a direct modulation method, which extracts the frequency components of a mixing signal obtained by electrically multiplying the interference signal and a local oscillation signal generated by means of a mixer circuit.

0020The above discussion has been concerned with processing in the frequency domain, in order to obtain an equivalent time processing. It is also possible to measure the characteristic of the time waveform, to operate in the time domain. The interference signal has equal information in the light phase difference which is measured relative to the phase modulation, for both the time domain and the frequency domain. Therefore, it is possible to make use of the waveform moment in the time domain, as a characteristic variable of that waveform, and operate in the time domain, rather than considering lines in a Fourier spectrum when operating in the frequency domain.

0021Thus, in an interference measuring method operating in the time domain, the phase difference between the interfering waves can be determined by using time information from the time waveform characteristic points of the interference wave signal and calculating the phase difference between the interfereing waves from the result of that measurement.

0022An interference sensor operating in the time domain may then extract the time waveform characteristic points of the interference wave signal and calculate the time intervals between the extracted waveform characteristic points or time intervals between the waveform characteristic points and specified time reference points associated with the interfering waves. From the calculated time intervals, it is possible to determine the phase difference between the interfering waves or a physical quantity represented by the phase difference.

0023Such an interference sensor may adjust the phase difference of interference between the interfering waves by phase-modulating the interference signal with an optical phase modulation extract the time waveform characteristic points of the interference wave signal, which was formed of two phase-modulated interfering waves combined, and calculate the time intervals between the extracted waveform characteristic points or the time intervals between the waveform characteristic points and the specified time reference points of the phase modulation drive signal. To simplify the construction of and processing by the interference sensor, the optical phase modulation preferably uses a periodically recurring signal as the drive signal in phase-modulating the interfering waves. Also for improved precision, it is desirable to compensate for the quantity of phase modulation on the basis the quantity of phase modulation resulting from the optical phase modulation detected from the measured value of the time intervals.

0024It is also desirable that the maximum or minimum points of the time waveform of the interference signal or the center of the time waveform be used as the waveform characteristic points. It is further desirable for the simplified processing that the waveform characteristic points be distinguished according to their time intervals with respect to the specified time reference points.

0025The interference measurement may involve modulating the intensity of a wave source by using a locally oscillated signal, the locally oscillated signal having a frequency difference from that of the optical phase modulation drive signal and also having a frequency spectrum such that its amplitude characteristic is flat up to a specified high-order frequency component.

0026Embodiments of the present invention operating in either the time domain or the frequency domain will now be described. It should be noted that the present invention can make use of digital circuitry, which permits integration of the signal processing circuit, and also permits the present invention to make use of integrated circuit technology.

0027Thus the apparatus may be made small in size by implementing the signal processing circuit in the form of an LSI and may be used as a sensor for measuring rotational motion or as an azimuth sensor. This enables a vehicular control system of high precision to be constructed.

0028Fig. 1 shows an example of the general arrangement of a phase modulation type optical fiber gyro according to a first embodiment of the present invention.

0029A light beam from a light source 10 propagates via a first fiber coupler 21 and a polarizer 30 and reaches a second fiber coupler 22, in which the beam branches into two light beams that propagate through a fiber loop 40 respectively counterclockwise and clockwise. These light beams have their light phases modulated by a phase modulator (PM) 50 in accordance with a modulation signal generated by a phase modulator driver circuit (PMPC) 60. This imposes a primary modulation. Thereafter, the two beams reach the fiber coupler 22 and are recombined causing an interference beam to be generated. The interference beam 1 passes from the fiber coupler 22 to the first fiber coupler 21 via the polarizer 30. In the first fiber coupler 21, the interference signal branches into two beams, one of which returns to the light source 10 and the other of which passes to a photoelectric converter circuit 70 employing a photodiode and is output as an interference signal therefrom. The interference signal is transmitted to a signal processing circuit 100 and is processed so as to extract the angular velocity of rotation of the optical fiber gyro.

0030Next, the interference signal will be explained. If the interference signal is denoted by P, it can be expressed by Eqs. (1) and (2) in accordance with the principle of interference:<maths id="math0001" num="(1)"><math display="block"><mrow><mtext>P = K {1 + v cos ψ}</mtext></mrow></math><img file="EP0444843A2_D0001.tif" /></maths><maths id="math0002" num="(2)"><math display="block"><mrow><msub><mrow><mtext>ψ = ø</mtext></mrow><mrow><mtext>S</mtext></mrow></msub><mtext> + ø(t) - ø(t-τ)</mtext></mrow></math><img file="EP0444843A2_D0002.tif" /></maths>

0031Here, ψ denotes the phase difference of the beams, K a coefficient which is proportional to the intensity of the beams and the gain of the photoelectric converter circuit, <u style="single">v</u> a transmission characteristic of the interferometer, and ø_S the Sagnac phase difference which is proportional to the rotational angular velocity of rotation. In addition, τ denotes the propagation delay time of the light wave which propagates through the fiber loop.

0032In this embodiment, a sinusoidal wave at a frequency f_m is employed as the phase modulation signal. Assuming the characteristics of the phase modulator to be ideal, the interference signal P is as shown in Eq. (3):<maths id="math0003" num="(3)"><math display="block"><mrow><msub><mrow><mtext>P = K{1 + v cos (øs - ø</mtext></mrow><mrow><mtext>e</mtext></mrow></msub><mtext> sin ϑ)</mtext></mrow></math><img file="EP0444843A2_D0003.tif" /></maths><maths id="math0004" num="(4)"><math display="block"><mrow><msub><mrow><mtext>ϑ = w</mtext></mrow><mrow><mtext>m</mtext></mrow></msub><mtext> (t - τ/2)</mtext></mrow></math><img file="EP0444843A2_D0004.tif" /></maths><maths id="math0005" num="(5)"><math display="block"><mrow><msub><mrow><mtext>ø</mtext></mrow><mrow><mtext>e</mtext></mrow></msub><msub><mrow><mtext> = 2 ø</mtext></mrow><mrow><mtext>m</mtext></mrow></msub><msub><mrow><mtext> sin (w</mtext></mrow><mrow><mtext>m</mtext></mrow></msub><mtext> τ/2)</mtext></mrow></math><img file="EP0444843A2_D0005.tif" /></maths>

0033Here ø_e denotes the effective phase modulation index, w_m = 2πf_m a modulation angular frequency, and ø_m a modulation amplitude.

0034The interference signal P in Eq. (3) is expanded into a Fourier series employing Bessel functions, and it becomes a line spectrum with lines at frequencies f_m, 2f_m, 3f_m, 4f_m .... For the purpose of eliminating fluctuations in the light intensity coefficient K and the effective phase modulation index ø_e and them measuring the Sagnac phase difference ø_S, the amplitudes of at least three of the lines of the spectrum need to be determined. In this embodiment, the first-order, second-order and fourth-order frequency components of the phase modulation are extracted from the interference signal by the signal processing circuit 100 to which the technique of equivalent time processing is applied. The arrangement and operation of the signal processing circuit 100 in this embodiment will be described below.

0035The arrangement of the signal processing circuit 100 may be divided into the following four sections: a sampling circuit 111 which samples the photoelectrically-converted interference signal and converts the sampled signal into a digital signal; a timer circuit 112 which generates timing signals for the sampling time, processing time, etc; a digital signal processor 180 which executes digital processing on the results of the sampling, so as to determine the angular velocity of rotation; and a control circuit 170 which controls the sampling circuit and the arithmetic processing circuit.

0036The processing circuit 100 is thus relatively simple, and the signals at lower frequencies corresponding to the interference signal can be obtained by sampling the interference signal at a sampling frequency different e.g., lower, than the frequency of the interference signal. This gives the advantage that neither high-speed sampling processing nor a high-speed A/D converter is required.

0037The sampling circuit 111 has an input buffer 110 which receives the interference signal and adjusts the signal level thereof, a sample-and-hold circuit 120 which samples the output signal of the input buffer at a predetermined frequency, and an A/D converter 130 by which the signal from the sample-and-hold circuit is converted into a digital signal.

0038The timer circuit 112 includes a crystal oscillator (OSC) 140, a frequency divider 150 which is formed e.g. by a high-speed TTL and which divides the frequency of the output signal of the oscillator 140, and a programmable timer 160 which receives a clock signal produced by the frequency division of the frequency divider 150. This timer 160 supplies the sampling circuit, the digital signal processor 180 and a microcomputer (CPU) 170 with clock signals respectively corresponding thereto.

0039The programmable timer 160 operates with reference to the clock signal which is fed from the frequency divider 150. Thus, a pulse signal is generated at a predetermined frequency f_s; and is applied to the sample-and hold circuit 120 and the A/D converter 130 as a sampling timing. The sample-and-hold circuit 120 and the A/D converter 130 perform the above-described operations of sampling and holding the interference signal and A/D converting the sampling timing at the sampling frequency f_s.

0040The programmable timer 160 generates a square wave signal at the frequency f_m of the primary modulation and supplies that square wave to the phase modulator driver circuit 60. The phase modulator driver circuit 60 has a filter circuit, and a transistor buffer circuit which drives the phase modulator 50 as a capacitive load. In such a phase modulator driver circuit 60, the higher harmonic components of the square wave signal received from the programmable timer 160 are removed by filtering by a filter circuit, and a substantially sinusoidal signal at the frequency f_m is set as the primary modulation signal so as to drive the phase modulator 50.

0041The microcomputer 170 is connected through a bus line with the programmable timer 160, A/D converter 130 and digital signal processor 180. The oscillation operation of the programmable timer 160 is controlled by the microcomputer 170. The sampling frequency f_s and the phase modulation frequency f_m are set by the microcomputer 170. The microcomputer 170 monitors the A/D conversion operation of the A/D converter 130, and it senses the end of the A/D conversion after receiving the sampling timing signal from the programmable timer 160. The interference signal converted into a digital code by the A/D converter 130 is read out of this A/D converter 130 as interference signal data every sampling step by the microcomputer 170. The microcomputer 170 transfers the interference signal data to the digital signal processor 180. Since the production of the interference signal data by the A/D converter 130 is synchronous with the sampling timing, the data transfer is also performed at the same frequency as the sampling frequency f_s.

0042On receiving the interference signal data from the microcomputer 170, the digital signal processor 180 extracts the component at the phase modulation frequency f_m, the component at the second-order harmonic 2f_m and the component at the fourth-order harmonic 4f_m, which components are contained in the interference signal. In this embodiment, the equivalent time signal processing is carried out in accordance with the present invention using the techniques referred to above as "down sampling". More specifically, the aliasing signal components Δf etc. of lower frequencies corresponding to the phase modulation frequency components are extracted by using the relationships of Eqs. (6) - (8) below which are expressed in terms of the sampling frequency f_s and the phase modulation frequency f_m.<maths id="math0006" num="(6)"><math display="block"><mrow><msub><mrow><mtext>Δf = f</mtext></mrow><mrow><mtext>m</mtext></mrow></msub><msub><mrow><mtext> - nf</mtext></mrow><mrow><mtext>s</mtext></mrow></msub></mrow></math><img file="EP0444843A2_D0006.tif" /></maths><maths id="math0007" num="(7)"><math display="block"><mrow><msub><mrow><mtext>2Δf = 2f</mtext></mrow><mrow><mtext>m</mtext></mrow></msub><msub><mrow><mtext> - 2nf</mtext></mrow><mrow><mtext>s</mtext></mrow></msub></mrow></math><img file="EP0444843A2_D0007.tif" /></maths><maths id="math0008" num="(8)"><math display="block"><mrow><msub><mrow><mtext>4Δf = 4f</mtext></mrow><mrow><mtext>m</mtext></mrow></msub><msub><mrow><mtext> - 4nf</mtext></mrow><mrow><mtext>s</mtext></mrow></msub></mrow></math><img file="EP0444843A2_D0008.tif" /></maths> In these equations, n is an integer.

0043The above situation is illustrated in Fig. 2 (a). The generation of the aliasing frequencies resembles the principle of a stroboscope or a sampling scope. It should be noted that f_s may be greater or less than f_m, although only the latter case will be discussed in detail below. By digital calculations based on the interference signal data items received, the digital signal processor 180 extracts the value of Δf, 2Δf and 4Δf frequency components in place of the frequencies f_m, 2f_m and 4f_m. The filter calculations in this embodiment will be described below.

0044Fig. 3 is a block diagram of the digital arithmetic processing which is executed in the digital signal processor 180. Individual functional blocks are preferably achieved by suitable software, but dedicated circuits may be used.

0045The interference signal data items from the microcomputer 170 are input to band-pass filters 201, 202 and 204 of center frequencies Δf, 2Δf and 4Δf previously set by the microcomputer and are extracted as the first-order, second-order and fourth-order component signals, respectively. Amplifiers 211, 212 and 214 amplify the respective signals to suitable magnitudes. At this stage, the respective signals contain, not only the principle components of the corresponding frequencies Δf, 2Δf, and 4Δf, but also noise and other frequency components which have not been completely suppressed by the band-pass filters 201, 202, and 204. Multipliers 221, 222 and 224 detect the rspective signals of the first-order, second-order and fourth-order components at high sensitivities by a lock-in operation. More specifically, the first-order component signal from the amplifier 211, for example, is multiplied by the first-order reference signal of a frequency Δf in the multiplier 221. As a result, the output signal of the multipler 221 has a component of frequency 2Δf and D.C. components and other noise frequency components. The D.C. component is extracted from these components by a low-pass filter 231.

0046The above lock-in operation is similar for the second-order and fourth-order component signals. The multiplier 222 and a low-pass filter 232 constitute a lock-in detector for the second-order frequency 2Δf. Therefore, the second-order reference signal of the frequency 2Δf is input to the multiplier 222. Likewise, the multiplier 224, and a low-pass filter 234 constitute a lock-in detector for the fourth-order frequency 4Δf, and the fourth-order reference signal of a frequency 4Δf is used.

0047In this embodiment, however, it is sometimes difficult to produce suitable low-pass filters in the form of digital filters for the sampling frequency. In this embodiment, therefore, the low-pass filters 231, 232 and 234 are succeeded by diminution sampling units 241, 242 and 244 as shown in Fig. 3. The diminution sampling units 241, 242 and 244 sample input data at a frequency f_d. The diminution frequency f_d should normally be lower than the sampling frequency f_s and higher than the frequency response to be achieved by the optical fiber gyro.

0048Low-pass filters 251, 252 and 254 subject the output data items of the respective diminution sampling units 241, 242 and 244 to filtering. Accordingly, the first-order D.C. signal S₁, second-order D.C. signal S₂ and fourth-order D.C. signal S₄ which are the outputs of the low-pass filters 251, 252 and 254 are proportional to the amplitudes of the Δf, 2Δf and 4Δf frequency components contained in the interference signal data items, respectively. The Δf, 2Δf and 4Δf frequency components in the interference signal data items are the reflexes of the phase modulation frequency f_m and the higher harmonic components 2f_m and 4f_m thereof which are originally contained in the interference signal, so that the D.C. signals S₁, S₂ and S₄ are proportional to the amplitudes of the f_m and 2f_m and 4f_m frequency components in the interference signal respectively.

0049The D.C. signals S₁, S₂ and S₄ are input to dividers 261 and 262, by which the first ratio signal x = S₁/S₂ and the second ratio signal <u style="single">y</u> = S₄/S₂ are respectively output. The second ratio signal <u style="single">y</u> is a variable dependent upon only the effective phase modulation index ø_e of Eq. (5), and is expressed by Eq. (9):<maths id="math0009" num="(9)"><math display="block"><mrow><msub><mrow><mtext>y = J₄(ø</mtext></mrow><mrow><mtext>e</mtext></mrow></msub><msub><mrow><mtext>)/J₂(ø</mtext></mrow><mrow><mtext>e</mtext></mrow></msub><mtext>)</mtext></mrow></math><img file="EP0444843A2_D0009.tif" /></maths>

0050The first ratio signal <u style="single">x</u> is expressed by Eq. (10) with the Sagnac phase difference ø_S:<maths id="math0010" num="(10)"><math display="block"><mrow><msub><mrow><mtext>k x = tan ø</mtext></mrow><mrow><mtext>S</mtext></mrow></msub></mrow></math><img file="EP0444843A2_D0010.tif" /></maths><maths id="math0011" num="(11)"><math display="block"><mrow><msub><mrow><mtext>k = J₁(ø</mtext></mrow><mrow><mtext>e</mtext></mrow></msub><msub><mrow><mtext>)/J₂(ø</mtext></mrow><mrow><mtext>e</mtext></mrow></msub><mtext>)</mtext></mrow></math><img file="EP0444843A2_D0011.tif" /></maths>

0051The constant <u style="single">k</u> in Eq. (11) is determined by only the effective phase modulation index ø_e. In Eqs. (9) and (11), J_n (n = 1, 2, 4) denotes a Bessel function of the first kind of order <u style="single">n</u>.

0052The effective phase modulation index ø_e fluctuates in dependence on the voltage amplitude of the drive signal produced by the phase modulator driver circuit 60, and in addition, on the characteristics of the phase modulator 50 itself. Consequently, the constant <u style="single">k</u> of Eq. (11) also fluctuates. The second ratio signal <u style="single">y</u> compensates for the fluctuations of the effective phase modulation index ø_e. When the index ø_e is obtained from the value of the signal <u style="single">y</u> in accordance with Eq. (9), the constant <u style="single">k</u> can be determined by Eq. (11). The relationship between the second ratio signal <u style="single">y</u> and the constant <u style="single">k</u> need not be calculated on each occasion, but the corresponding values thereof can be found by tabulating them in advance. A look-up table 270 stores the relationship between the parameters <u style="single">y</u> and <u style="single">k</u>, and it generates the constant <u style="single">k</u> in response to a <u style="single">y</u> input.

0053An angular velocity calculator 280 receives the first ratio signal <u style="single">x</u> from the first divider 261 and the constant <u style="single">k</u> from the look-up table 270, and calculates the rotational angular velocity,Ω,in accordance with Eq. (12) and delivers it as an output:<maths id="math0012" num="(12)"><math display="block"><mrow><mtext>Ω = A tan ⁻¹k x</mtext></mrow></math><img file="EP0444843A2_D0012.tif" /></maths> where the constant A is given by<maths id="math0013" num="(13)"><math display="block"><mrow><msub><mrow><mtext>A ø</mtext></mrow><mrow><mtext>S</mtext></mrow></msub><mtext> = Ω</mtext></mrow></math><img file="EP0444843A2_D0013.tif" /></maths> and it is stored in accordance with the angular velocity calculator 280.

0054Next, the generation of the first-order, second-order and fourth-order reference signals will be discussed. As explained before, the reference signal whose frequency is equal to the signal frequency to be detected is required for lock-in detection. In this embodiment, the reference signals are generated by sampling a square wave signal which is synchronous with the phase modulation signal.

0055The square wave signal of frequency f_m generated by the programmable timer 160 is supplied to the digital signal processor 180 as shown in Fig. 1, and is applied to a digital input terminal 300 as shown in Fig. 3. A sampling circuit 310 checks the input state of the input terminal 300, whereupon it provides a numerical value +1 for an input of high level and numerical value -1 for an input of low level. Checking of the input to the input terminal by the sampling circuit 310 is performed every time there is input of interference signal data. Accordingly, the sampling circuit samples the input signal at a period corresponding to the sampling frequency f_s and produces a square wave at values +1 or-1.

0056The sampling operation of the sampling circuit 310 causes the reflex frequency Δf based on Eq. (6) to appear at the output of the sampling circuit 310. A band-pass filter 321 extracts the reflex frequency component Δf from the output signal of the sampling circuit 310. The signal at frequency Δf derived by the band-pass filter 321 has its phase adjusted by a phase shifter 331 and has its amplitude set to an appropriate value by an amplifier 341. The resulting signal is used as the first-order reference signal.

0057In the operations discussed above, the phase adjustment by the phase shifter 331 is important for enhancing the sensitivity of lock-in detection. Thus, the first-order reference signal is adjusted so as to be substantially in-phase with the first-order component signal to be detected in the multiplier 221, to make optimum the sensitivity of lock-in detection. Simultaneously, the plus or minus polarity of the angular velocity data for counterclockwise rotation is determined.

0058In lock-in detection, the reference signal must have a fixed phase relative to the input signal. If this does not happen, the D.C. signal level and polarity of lock-in detection output change with the phase. In this embodiment, all timing operations are derived from the crystal oscillator 140 and the programmable timer 160, and phase relationships do not change.

0059The generation of the second-order and fourth-order reference signals are similar to that of the first-order reference signal described above. In order to produce the signal of the frequency 2Δf, however, the output signal of the band-pass filter 321 is multiplied by an integer by a multiplier 351. A band-pass filter 322 extracts the components of frequency 2Δf from the integral-times output of the multiplier 352, and the component of frequency 4Δf is derived from the product by a band-pass filter 324. The operations of phase shifters 332, 334 and amplifiers 342, 344 are the same as for the first-order reference signal.

0060When the apparatus is operated with the above arrangement, the interference signal can be sampled at a frequency lower than that of the interference signal, and the sampled signal may be processed by a A/D converter of low operating speed. Therefore, an A/D converter of high speed and high cost in unnecessary, permitting savings in cost and size. Furthermore, the required number of sampling data items decreases, and the time required for calculations etc. may be shortened, to give the advantage that the accuracy of the processing can be enhanced and the time of processing can be shortened.

0061Next, a practical example of the above embodiment will be described.

0062First, the frequency response characteristic of the optical fiber gyro is set at 30 Hz, and an A/D converter of 12 bits is employed as the A/D converter 130. The crystal oscillator 140 employed produces a frequency of 40 MHz, which is divided into clock signals at 2.5 MHz of 1/16 frequency and of 5 MHz of 1/8 frequency by the frequency divider 150, the clock signals being respectively fed to the programmable timer 160 and the microcomputer 170. In addition, a clock signal at a frequency of 40 MHz is fed to the digital signal processor 180. Since the microcomputer 170 has a data bus of 8 bits, data is transferred at two divided steps each handling one byte.

0063When the phase modulation frequency is about 20.5 kHz and the sampling frequency is set at 5kHz, the value of n is given as n = 4 which is the closest value to the phase modulation frequency, in accordance with Eqs. (6) to (8). With the above setting, the reflex frequency components of the fundamental wave component f_m, second-order harmonic component 2f_m and fourth-order harmonic component 4f_m of the interference signal appear as Δf = 0.5 kHz, 2Δf = 1 kHz and 4Δf = 2 kHz as illustrated in Fig. 2 (b).

0064In order to extract the reflex frequency components from the interference signal and on the basis of the commands of the microcomputer 170, the interference signal data items are passed through the band-pass filters 201, 202 and 204 of the digital signal processor 180 whose center frequencies are pre-set at frequencies Δf, 2Δf and 4Δf. In this example, the digital signal processor 180 is operated by a clock signal of 40 MHz, so that a multiplication and an addition can be processed once in 100 nsec. Since the sampling frequency is 5 kHz (a period of 200 sec.), filter calculations based on at most 2000 multiplications and additions are possible.

0065However, the outputs of the band-pass 201, 202 and 204 contain not only the components of the signal frequencies Δf, 2Δf and 4Δf bit also other frequency components and noise. The Δf, 2Δf and 4Δf of components are therefore detected at high sensitivities by the lock-in operation, using the multipliers 221, 222 and 224 and the reference signals (the output signals of the components 341, 342 and 344) equal to the signal frequency components. Subsequently, the cut-off frequencies of the low-pass filters 231, 232 and 234 are set at 200 Hz, and D.C. components proportional to the center frequency components of the corresponding band-pass filters are extracted.

0066It is difficult, however, to achieve a low-pass filter having the cut-off frequency of 30 Hz in the form of a digital filter when the sampling frequency f_s is set at 5 kHz. The reason is that the digital signal processor 180 used in this example executes a floating point calculation having a mantissa part of 4 bits and an exponent part of 6 bits, and the finite calculation makes it difficult to fabricate the filter whose cutoff frequency is very different from the sampling frequency. In this example, therefore, the diminution sampling units 241, 242 and 244 are placed behind respective low-pass filters 231, 232 and 234. These diminution sampling units 241, 242 and 244 are set at a frequency f_d = 500 Hz. Each of the diminution sampling units 241, 242 and 244 delivers one output data item for ten input data items so that the sampling rate of the output data is changed from 5 kHz to 500 Hz.

0067As the frequency response of the optical fiber gyro is set at 30 Hz. Therefore frequency components of and above 30 Hz which are contained in the D.C. signals which are the outputs of the diminution sampling units are eliminated by the low-pass filters 251, 252 and 254. The outputs of the low-pass filters 251, 252 and 254 are processed by the dividers 261 and 262. The processed results are input to the angular velocity calculator 280 and are changed into a rotational angular velocity measurement.

0068Thus, the angular velocity of rotation is obtained with high precision.

0069An optical phase modulator having a structure in which an optical fiber is wound around a piezo-ceramic cylinder may be used in the present invention. In a phase modulation type optical fiber gyro, a phase modulator of this type has a mechanical resonance frequency f_r which is determined by the dimenions and material of the piezo-ceramic cylinder. The phase modulation frequency f_m is usually set in the vicinity of the mechanical resonance frequency f_r. The voltage amplitude of the phase modulation signal can be reduced by utilizing mechanical resonance.

0070In order to attain a predetermined phase modulation amplitude, the voltage amplitude of the phase modulation signal may be adjusted. Since, however, the mechanical resonance is used in the phase modulator, the phase modulation amplitude depends greatly upon the modulation frequency f_m. For this reason, the frequency with which the voltage amplitude of the phase modulation signal reaches an appropriate level and which can mitigate modulation distortion and fluctuation in a modulation characteristic needs to be selected as the phase modulation frequency f_m.

0071Nevertheless, even when the piezo-ceramic cylinders for use in the phase modulators are baked with the same dimensions and under the same conditions, there is normally a wide variation in the mechanical resonance characteristics. Thus, the phase modulation frequency f_m differs from one phase modulator to another. In order to bring the mechanical resonance frequency f_r, to a predetermined value, it is known to polish the piezo-ceramic cylinder to achieve a suitable adjustment. The need for this polishing step is a serious obstacle to a reduction in the fabrication cost of the optical fiber gyro.

0072In this embodiment, as shown in Fig. 1, the microcomputer 170 is provided with means 190 for receiving external data, thereby making it possible to set the phase modulation frequency f_m at an optimum value in accordance with the mechanical resonance characteristic of each individual phase modulator 50. Hence, the microcomputer 170 receives the phase modulation frequency f_m in the form of data from means 190 and controls the programmable timer 160 so as to generate a square wave signal of this frequency. Similarly, the microcomputer 170 receives the sampling frequency f_s in the form of data from the means 190 and controls the programmable time 160 so as to generate the pulses at the sampling timings of this frequency. In this embodiment, the setting of the data items of the phase modulation frequency f_m and sampling frequency f_s, with which the reflex frequencies Δf, 2Δf and 4Δf determined by Eqs. (6) to (8) have predetermined values, is achieved using the means 190 to control the microcomputer 170. Accordingly, the filter processing steps of the digital signal processor 180 in Fig. 3 for the frequencies Δf, 2Δf and 4Δf become arithmetic processing steps which use the same filter coefficients at all times without regard to the value of the phase modulation frequency f_m.

0073The means 190 described above may provide the microcomputer 170 with either the phase modulation frequency f_m or the sampling frequency f_s. The other frequency may be calculated from the one provided, by the microcomputer 170 in accordance with Eq. (6) under the condition that the reflex frequency Δf is held constant. The reflex frequencies Δf, 2Δf and 4Δf can be altered so as to satisfy Eqs. (6) to (8) so that the phase modulation frequency f_m is provided as external data and that the sampling frequency is held at a constant value. In this case, the filter calculations of the digital signal processor 180 need to change calculation coefficients in accordance with the alterations of the frequencies Δf, 2Δf and 4Δf, and the microcomputer 170 instructs the digital signal processor 180 to change the calculation coefficients.

0074As stated above, the influence of the different characteristics of the phase modulators can be corrected by the means 190 for receiving external data so that the phase modulator 50 need not be of high precision and can have its cost minimized.

0075Fig. 4 shows a second embodiment of the present invention. The second embodiment differs from the first embodiment only in the method of supplying the external frequency data. Apart from this, other parts of this embodiment are similar to those of the embodiment of Fig. 1 and the same reference numerals are used. However, the second embodiment is furnished with a rewritable nonvolatile memory device 191. Data items representing the phase modulation frequency f_m and sampling frequency f_s which are set as appropriate for every phase modulator are recorded in the memory device 191. The microcomputer 170 reads out the frequency data items from the nonvolatile memory device 191 at the resetting of power-ON, and controls the operation of the programmable timer on the basis of the data items calculation. Similarly, either the reflex frequency or the sampling frequency may be fixed. The data items which are set as appropriate for each individual phase modulator are recorded in the nonvolatile memory device 191.

0076In this manner, once the optimum values corresponding to the characteristics of the phase modulator 50 have been recorded in the nonvolatile memory device 191 it is not necessary to supply input data each time the apparatus is switched on, and the labor of the input operation can be saved.

0077Fig. 5 shows a third embodiment of the present invention. In each of the first and second embodiments, the sampling means, timing generation means, arithmetic means and control means are shown as individual functional elements. The third embodiment uses a signal processing LSI 101 in which these elements are integrated on a single substrate. The signal processing LSI 101 includes therein a sample-and-hold circuit and an A/D converter as the sampling means, a digital numerical operation circuit as the arithmetic means, and a logical operation circuit and a memory circuit as the control means. Part of the memory circuit is a rewritable nonvolatile memory, in which data appropriate for each phase modulator is recorded. The control of the timing generation means and the transfer of the interference signal data by the control means, the generation of the phase modulation signal and sampling timings by the timing generation means, and the digital calculation processing of the interference signal by the arithmetic means are the same as in the first embodiment.

0078By constructing the detection circuit in the form of a single LSI as described above, the detector can be reduced in size, and the range of applications of the optical fiber gyro may be expanded.

0079Fig. 6 shows a fourth embodiment of the present invention. In the fourth embodiment, the operations of the programmable timer 160 and digital signal processor 180 are somewhat difference from those in the first embodiment, and a signal adder circuit 61 is included as will be described. The other components are the same as in the first embodiment, and the same reference numerals are used.

0080In the fourth embodiment, the programmable timer 160 genetates a first square wave signal of a frequency f_m1 and a second square wave signal of a frequency f_m2. These signals are input to the signal adder circuit 61, and the sum thereof is supplied to the phase modulator driver circuit 60. Accordingly, the phase modulator 50 is driven by a phase modulation signal which has both the frequencies f_m1 and f_m2 as its frequency components. First and second square wave signals are fed to the digital signal processor 1780, and they are utilized for lock-in detection of the frequency components in the same manner as in the first embodiment.

0081In consequence of cross modulation based on the two frequencies there is an interference signal spectrum with the frequencies f_m1, f_m2 and the higher harmonic components thereof, together with the beat frequency of Eq. (14) and the higher harmonic components thereof:<maths id="math0014" num="(14)"><math display="block"><mrow><msub><mrow><mtext>B = f</mtext></mrow><mrow><mtext>m1</mtext></mrow></msub><msub><mrow><mtext> - f</mtext></mrow><mrow><mtext>m2</mtext></mrow></msub></mrow></math><img file="EP0444843A2_D0014.tif" /></maths>

0082In this embodiment, the beat frequency and the higher harmonic components thereof are used for detection and correction of the Sagnac phase difference. Also, reflex frequencies produced by "down sampling" are used. The reflexes of the first and second frequencies f_m1 and f_m2 based on "down sampling" appear as:<maths id="math0015" num="(15)"><math display="block"><mrow><msub><mrow><mtext>Δf = f</mtext></mrow><mrow><mtext>m1</mtext></mrow></msub><msub><mrow><mtext> - f</mtext></mrow><mrow><mtext>s</mtext></mrow></msub></mrow></math><img file="EP0444843A2_D0015.tif" /></maths><maths id="math0016" num="(16)"><math display="block"><mrow><msub><mrow><mtext>Δf + B = f</mtext></mrow><mrow><mtext>m2</mtext></mrow></msub><msub><mrow><mtext> - f</mtext></mrow><mrow><mtext>s</mtext></mrow></msub></mrow></math><img file="EP0444843A2_D0016.tif" /></maths>

0083In this embodiment, the Sagnac phase difference using the beat frequency components of lower frequencies as described above, so that the requirements of frequency characteristics at the input ends of the input buffer 110 and sample-and-hold circuit 120 can be mitigated. However, high frequencies may also be used. Since the first embodiment uses the reflex of the fourth-order higher harmonic component of the phase modulation frequency, response of the circuitry is required up to the frequency of the fourth-order higher harmonic component at stages previous to the completion of the sampling. In contrast, in this embodiment, the frequencies of the beat frequency components suffice, and the frequency characteristics of the input buffer 110 and sample-and-hold circuit 120 can be relieved.

0084As in the first embodiment, lock-in detection is used to extract the frequency spectrum components by the digital signal processor 180. The arrangements and operations of the lock-in detectors are the same as in the first embodiment, and only the frequencies of the reference signals are different. Thus, as illustrated in Fig. 7 the beat frequency B, reflex frequency Δf and sum frequency Δf + B, and the higher harmonics thereof are needed.

0085Referring now to Fig. 8, methods for producing the reference signal frequencies will be described.

0086The first and second square wave signals of frequencies f_m1 and f_m2 are respectively supplied to digital input terminals 400 and 401 of the digital signal processor 180. As in the first embodiment, sampling circuits 410 and 411 refer to these signal inputs with the sampling frequency f_s and generate numerical sequences of +1 and -1 in accordance with the input logic levels. The numerical sequences are respectively input to band-pass filters 420 and 421 having Δf and Δf + B as their center frequencies whereby signals of frequencies Δf and Δf + B ate produced. In addition, these signals are multiplied by each other using a multiplier 430, and a signal corresponding to the difference frequency B between the signals is derived using a band-pass filter having B as its center frequency. As in the first embodiment, these signals of the respective frequencies are multiplied by integers so as to generate higher harmonic components, and they are converted into reference signals of appropriate amplitude levels and phase by phase shifters and amplifiers.

0087Next, a specific example of the fourth embodiment will be described. First, if the first modulation frequency f_m1 is set at 20.5 kHz and the second modulation frequency f_m2 at 21.5 kHz, the beat frequency B becomes 0.75 kHz in accordance with Eq. (14). The frequency spectrum of the interference signal is shown in Fig. 7. In this figure, assuming the sampling frequency f_s to be 5 kHz, the reflex frequency component Δf of the first modulation frequency f_m1 becomes 0.5 kHz, and the reflex frequency component Δf + B of the beat frequency component (the second modulation frequency component f_m2) becomes 1.25 kHz. When the beat frequency component is used in this manner, the frequencies need not be handled up to the fourth-order higher harmonic frequency 82 kHz as in the first embodiment, but the frequencies of up to the second modulation frequency f_m = 21.5 kHz may be handled, so that the frequency characteristics of the input buffer and the sample-and-hold circuit can be simplified.

0088As described above, the frequency characteristics to be attained may be of the lower frequency owing to the adoption of the present invention. Therefore the apparatus can be simplified, and the number of data items to be handled in the digital processing.

0089Fig. 9 shows a fifth embodiment of the present invention. The signal procesing circuit 100 of the fifth embodiment is substantially the same as that of the first embodiment, but the former differs from the latter in that it has a rewritable memory device 192 instead of the digital signal processor 180. As in the first embodiment, the interference signal is sampled and converted into the digital signal by the sample-and-hold circuit 120 and the A/D converter 130 in accordance with the sampling timings which the programmable timer 160 generates. The sampling timing signal from the progammable timer 160 is input to the microcomputer 170, and the sampled values of the interference signal are successively accumulated and stored in the rewritable memory device 192.

0090As illustrated in Fig. 10, the operation of the microcomputer 170 is divided into a data sampling period and a calculation processing period, which repeat alternately. The microcomputer 170 first accumulate a predetermined number of sampled values of the interference signal in the rewritable memory device 192 and subsequently reads out these differences of the interferometer. Then it calculates the angular velocity of rotation detected by the optical fiber gyro. As show in in Fig. 11 the microcomputer 170 reads out the interference signal data sampled in an equivalent time, from the rewritable memory device 192 and thereafter generates a signal waveform for one or more cycles of the time waveform of the interference signal, in the course of calculating the phase differences of the interferometer. The frequencies of the interference signal are analysed, on the basis of the composed waveform and using a well-known high-speed Fourier transform method.

0091As described above, according to this embodiment, the data sampling and the calculation processing are separated in time, so that the signal processing of the interference sensor is possible without requiring a numerical calculation processing capability of very high speed.

0092In any of the first to fifth embodiments explained above, the phase difference of the interferometer is determined by analyzing the frequency spectrum of the interference signal. As stated below, however, the phase difference of the interferometer can be determined even by computing the waveform moment of the time waveform of the interference signal.

0093P′ is defined as indicated in Eq. (17) for the interference signal P which is expressed by Eq. (1):<maths id="math0017" num="(17)"><math display="block"><mrow><mtext>P′ = P - a₀</mtext></mrow></math><img file="EP0444843A2_D0017.tif" /></maths><maths id="math0018" num="(18)"><math display="block"><mrow><mtext>a₀ = (1/2π) ∫ </mtext><mfrac linethickness="0"><mrow><mtext>π</mtext></mrow><mrow><mtext>-π</mtext></mrow></mfrac><mtext> Pdϑ</mtext></mrow></math><img file="EP0444843A2_D0018.tif" /></maths>

0094Here, a₀ denotes the D.C. component of the interference signal. For P′, the waveform moment m of order <u style="single">m</u> is computed as follows:<maths id="math0019" num=""><img file="EP0444843A2_D0019.tif" /></maths>

0095ø_s denotes the phase difference of the interferometer, and α_2n and β_2n denote coefficients which are determined by the effective phase modulation index ø_e. As is evident from Eq. (20), the m-th-order waveform moment of the interference signal is proportional to cos ø_s when <u style="single">m</u> is an even number, and it is proportional to sin ø_s when <u style="single">m</u> is an odd number. This is in a dual relationship with the fact that the even-numbered-order frequency spectrum of the interference signal is proportional to cos ø_s, while the odd-numbered-ordet frequency spectrum thereof is proportional to sin ø_s.

0096In each of the first to fifth embodiments, the phase difference ø_s of the interferometer can be determined by computing the waveform moment of the interference signal time waveform instead of calculating the frequency spectrum. The calculation of the frequency spectrum and that of the waveform moment may be combined so as to reduce the amount of calculation needed.

0097As described above, the adoption of the present invention enables the interference sensor to be of high precision and small size, so that the sensor may be applied in various uses.

0098Fig. 12 shows an example of a control system when the present invention is applied to sensors for an automobile.

0099An interference sensor 511 for measuring the yawing of the car body, an interference sensor 512 for measuring the rolling of the car body, and an interference sensor 510 for measuring the pitching of the car body are respectively installed in an automobile 500. Although, as illustrated, individual sensors are located in different places, they may be collectively located in one place.

0100The outputs of the respective sensors are fed to a signal processor 600 and are convered into controlling signals, which are sent to an input/output controller 700. This input/output controller 700 is supplied with the detection results of the interference sensors for e.g. a car speed, temperature in the interior of the car etc. Although not shown, the output of the yawing sensor which indicates the rotational direction and rotational angle of the automobile, is supplied from the input/output controller 700 to a navigation system. In the navigation system, the current position of the car is found using the above signal and the distance of travel evaluated by a separate speedometer or the like and is displayed by display means or the like and further the route leading to the destination, etc. may also be displayed.

0101In addition, the input/output controller 700 sends signals to an engine controller 800, an antiskid brake controller 900, an active suspension controller 550, a car height controller 560 and so forth.

0102When the automobile brakes the antiskid brake controller 900 controls the braking forces of the right and left wheels so as to generate torques opposite in sign to the angular velocity or rotation of the car body based on the signal representing the angular vlocity of rotation from the yawing sensor, and to decrease the absolute value of the signal representing the angular velocity of rotation, thereby to stop the automobile.

0103The active suspension controller 550 holds the car body stable while controlling the right and left and front and rear suspension elements so as to generate torques opposite in sign to the angular velocity of rotation from the pitching sensor 510 or the rolling sensor 512, and suppressing the absolute value of the signal representing the angular velocty of rotation so as to decrease that rotation.

0104In addition, the car receives a signal representing angular velocity from the rolling sensor 512 and holds the car body stable while controlling the suspension elements on the right and left of the car body so as to limit changes in the height of the car body.

0105It is also possible to employ the apparatus of the present invention in an arrangement in which the fiber loop 40 is mounted in a vertical plane so as to detect the rotation of the earth on its own axis, or in which the fiber loop 40 is turned round a vertical axis so as to find an absolute azimuth from a detected change in the angular velocity of the rotation of the earth on its own axis.

0106In the above description, an analysis was carried out on the basis of sampling the signal corresponding to the detection of the modulated and interfering beams. However, an equivalent effect can be achieved by applying an electronic modulation to the output of the detector which detects the modulated and interfering beams. A sixth embodiment of the present invention, shown in Fig. 13, illustrates such operation. In Fig. 13, components corresponding to components of the interference sensor shown in Fig. 1 are indicated by the same reference numerals.

0107In Fig. 13, the output of the converter (Phase Detector) 70 is amplified by an amplifier 200, and the resulting signal is modulated by a modulator 201. Thus, the signal from the modulator 201 has effectively had two modulations imposed on it, being the optical modulation imposed on the interfering beam by the optical phase modulator 50, and the second modulation imposed by the modulator 201. The modulation frequencies of these two modulations are different. The output of the modulator is passed via lock-in amplifiers 202 to an analog to digital and a digital to analog converter 203, which is controlled by the microcomputer 170. That microcomputer 170 also controls the lock-in amplifiers 202 and the phase modulator driver circuit 60.

0108The resultant processing is generally similar to the first to fifth embodiments, although sampling is then not necessary. However, it is possible to operate the interference sensor shown in Fig. 13 in combination with the sampling operations described earlier.

0109The seventh embodiment of the present invention is shown in Fig. 14. With the exception of the arrangement for modulating the signals, the arrangement is similar to the sixth embodiment of Fig. 13, and the same reference numerals are used for corresponding parts. In the embodiment of Fig. 14, however, the modulator 201 is omitted, and instead the microcomputer 170 supplies drive signals to the phase modulator drive circuit at two different frequencies f_m1 f_m2. These frequencies are different, so that the modulator 50 applies two different optical modulations to the interfering beams in the fiber loop 40. When the converter 70 detects the interference of those doubly-modulated beams, the signal is amplified via amplifier 200, the resulting input to the lock-in amplifiers 202 is exactly the same as the embodiment of Fig. 13. Therefore, a similar processing may be used, and indeed this can be combined with the sampling arrangement described with reference to the first to fifth embodiments.

0110All the embodiments described above have operated within the frequency domain for which consideration is given to the frequency of the electronic interference signal from the detector which detects the interfering radiation beams. However, it is also possible to analyse the phase-modulated signal in the time-domain, i.e. independent of frequency.

0111Embodiments of the present invention operating in the time domain will now be described with reference to Figs. 15 to 24. Fig. 15 shows a general view of the interference sensor operating in the time domain, and it can immediately be seen that the general structure is similar to that of the first embodiment of Fig. 1, except that there is a difference in the processing circuit, which is therefore indicated at 1000. Other components, which correspond to the interfering sensor of Fig. 1, are indicated by the same reference numerals. Before describing the processing circuit 1000, however, it is necessary to re-consider the characteristics of the interference signal which is detected by the converter 70.

0112Assuming the characteristic of the phase modulator 50 to be ideal, the optical phase difference ψ can be expressed by equation (21) and equations (4) and (5)<maths id="math0020" num="(21)"><math display="block"><mrow><msub><mrow><mtext>ψ = ø</mtext></mrow><mrow><mtext>s</mtext></mrow></msub><mtext> + η cosϑ</mtext></mrow></math><img file="EP0444843A2_D0020.tif" /></maths> where η is an effective phase modulation index.

0113The eighth embodiment takes the maximum and minimum point of the interference signal waveform as waveform charactetistic points.

0114At the maximum and minimum points, the differential of the interference signal P must satisfy the following equation (22) as a necessary condition.<maths id="math0021" num="(22)"><math display="block"><mrow><mtext>dP/dt = -Kνwmη sinϑ sin ψ = 0</mtext></mrow></math><img file="EP0444843A2_D0021.tif" /></maths> asuming døs/dt = 0 and d /dt = 0.

0115Therefore, at time t when sinϑ = 0 or sinψ = 0, the interference signal will take an extrenum.

0116The first embodiment uses the following equations (23) to (25) as design conditions of the optical fiber gyro.

0117Effective phase modulation index :<maths id="math0022" num="(23)"><math display="block"><mrow><mtext>π/2 ≦ η &lt; π</mtext></mrow></math><img file="EP0444843A2_D0022.tif" /></maths> Phase difference to be measured :<maths id="math0023" num="(24)"><math display="block"><mrow><mtext>|øs| &lt; π/2</mtext></mrow></math><img file="EP0444843A2_D0023.tif" /></maths> Optical phase difference :<maths id="math0024" num="(25)"><math display="block"><mrow><mtext>|ψ| &lt; π</mtext></mrow></math><img file="EP0444843A2_D0024.tif" /></maths>

0118Under these conditions, the interference signal waveform will be as shown in Fig. 14, with four maximum and minimum points appearing in one cycle of the phase modulation signal.

0119Suppose the solutions for sinϑ = 0 are ϑ1 and ϑ3 and those for sinψ = 0 are ϑ2 and ϑ4. Then with ϑ1 = 0 taken as a reference, ϑ3 = π. From equation (21) and (24) it follows that:<maths id="math0025" num="(26)."><math display="block"><mrow><mtext>øs = - ηcosϑ2 = - ηcosϑ4</mtext></mrow></math><img file="EP0444843A2_D0025.tif" /></maths>

0120Hence, the time positions of ϑ2, ϑ4 will change with the optical phase difference being measured øs (in this embodiment, proportional to the rotational angular velocity) according to equation (25).

0121The minimum points ϑ1, ϑ3 are fixed points independent of øs. η is a constant determined by the phase modulator characteristic and the phase modulator drive signal.

0122When the phase difference of ϑ2 (or ϑ4) with respect to ϑ1 (or ϑ3) is measured, the phase difference to be measured øs can be determined from equation (26).

0123Since, from equation (21), the phase distance between ϑ2 and ϑ3 (= π) and that between ϑ4 and ϑ3 (= π) are equal, it is also possible to determine the phase difference øs by measuring the phase difference between ϑ2 and ϑ4 and solving the equation (26).

0124Measuring the phase difference between the maximum and minimum points is equivalent to measuring the time intervals between each point, as is seen from equation (4). So, this embodiment measures the time difference.

0125As a time reference for measuring the time intervals, a highly accurate and stable clock can be obtained relatively easily with a quartz oscillator. The use of high-speed clock will increase the resolution and therefore the magnitude of the effective digits of measurement, expanding the dynamic range.

0126As is obvious from equation (26), when øs = 0, which represents a zero rotational angular velocity, cosϑ2 = cosϑ4 = 0, that is, ϑ2 = ϑ4 = 90° ± 180°.

0127In other words, when øs = 0, øs can be expressed as øs = ±ηcos(90°+Δϑ) = ±ηsin(Δϑ). A change in phase that corresponds to a change in the value of the sine function ±ηsin(Δϑ) becomes maximum at a point close to øs = ± νsin(Δϑ) = 0.

0128Equation (5) indicates that the change in time position is proportional to the phase change.

0129Thus, the measurement of øs based on the measurement of time position at points ϑ2 and ϑ4 according to this embodiment can have a maximum measuring sensitivity at a point close to øs = 0.

0130In this way, this invention is intended to improve the ease and performance of interference measurement by making use of high precision clocking.

0131Now, the signal processing circuit 1000 of the eighth embodiment will be explained.

0132Fig. 17 shows a block diagram of the signal processing circuit 1000 of the eighth embodiment.

0133In Fig. 17 there is shown a photoelectric conversion circuit 70 to convert the interference light into an electric signal and output an interference signal. The interference signal from the photoelectric conversion circuit 70 is applied to a differentiating circuit 1010 where it is differentiated. A zero-crossing detection circuit 1020 detects the zero-crossing point of the differential signal and generates an extremum timing pulse train representing the times at which the interference signal becomes the maximum or minimum.

0134A level comparing circuit 1040 compares the level of the interference signal with a specified threshold level and outputs a rectangular level signal in dependence on the result of comparison.

0135A fixed phase pulse generating circuit 1030 generates a specified phase timing by taking as a reference input a modulating signal from the phase modulator drive circuit (PMDC) 60.

0136A count control circuit 105 generates a count start pulse and a count stop pulse for controlling the operation of a counting circuit 106 in dependence on the extremum timing pulse from the zero-crossing detection circuit 102, the fixed timing pulse from the fixed phase pulse generating circuit 103, and the level signal from the comparison circuit 104.

0137In response to the count start and stop pulses, the counting circuit 106 counts the clock pulses output from the clock circuit 107. An arithmetic and logic unit 108 reads the count value from the counting circuit 106, calculates the phase difference øs to be measured by using equation (26), and converts that phase difference into a measurement of the angular velocity of rotation.

0138A suitable device for detecting the time at which the maximum and minimum of the interference signal occur may be, for example, a peak detection circuit.

0139The time waveform of the interference signal may use other characteristic points such as a waveform center, that is determined from the n-th order moment of the time waveform.

0140The operation of the eighth embodiment will now be described.

0141The zero-crossing detection circuit 1020 of this embodiment generates four extremum timing pulses in one cycle of the phase modulation signal.

0142To calculate øs by using equation (26), each of the four pulses must be correspondent to ϑ1 to ϑ4. For this purpose, this eighth embodiment provides a fixed phase pulse generating circuit 1030, which generates a specified phase timing according to the modulation signal supplied as a reference input from the phase modulator drive circuit 60, and a level comparison circuit 1040 that compares the interference signal level with the specified threshold level and outputs a rectangular level signal according to the result of comparison.

0143The count control circuit 1050 generates pulses to start and stop counting, to control the operation of the counting circuit 1060, in dependence on the extremum timing pulse from the zero-crossing detection circuit 1020, the fixed timing pulse from the fixed phase pulse generating cuircuit 1030, and the level signal from the level comparison circuit 1040. In this embodiment, as shown in Figure 16, the count start pulse and the count stop pulse are issued at the maximum point ϑ2 and the maximum point ϑ4, respectively. Therefore the time interval between the points ϑ2 and ϑ4 can be measured. The counting circuit 1060 counts the clock pulses supplied from the clock circuit 107 according to the count start and stop pulses from the count control circuit 1050. The arithmetic and logic unit 1080 reads the count value from the counting circuit 1060 to calculate the phase difference ϑs to be measured by using equation (26) and then transforms the calculated phase difference into a rotating angular velocity. The fixed timing pulse gives the start timing for this series of operations.

0144The phase modulator drive circuit 60 generates a phase modulation signal according to the clock pulses from the count clock generating circuit 1070. Hence, the phase modulator drive circuit 60 and the signal processing circuit 1000 operate in synchronism with each other.

0145A ninth embodiment of this invention will now be described.

0146When a piezo-ceramic element is used as the phase modulator, the modulation characteristic may exhibit a significant temperature dependency. This in turn causes the effective phase modulation index to drift with temperature, causing the output of the gyro to display a characteristic.

0147To eliminate this unwanted temperature dependency, means for compensating for variations in the modulation index is provided in the signal processing circuit 1000 of the ninth embodiment.

0148In the ninth embodiment, the design conditions for the optical fiber gyro are given by the following equations (27) to (29).

0149Effective phase modulation index:<maths id="math0026" num="(27)"><math display="block"><mrow><mtext>π ≦ η &lt; 2π</mtext></mrow></math><img file="EP0444843A2_D0026.tif" /></maths>

0150Phase difference to be determined:<maths id="math0027" num="(28)"><math display="block"><mrow><mtext>|øs| &lt; π</mtext></mrow></math><img file="EP0444843A2_D0027.tif" /></maths>

0151Optical phase difference:<maths id="math0028" num="(29)"><math display="block"><mrow><mtext>|ψ| &lt; 2π</mtext></mrow></math><img file="EP0444843A2_D0028.tif" /></maths>

0152In this case, the time waveform of the interference signal has eight maximum and minimum points during one cycle of the phase modulation signal starting from the zero point of the differential signal, as shown in Figure 18.

0153As shown in Figure 18, these maximum and minimum values are designated ϑ1 to ϑ8. ϑ1 to ϑ4 are solutions that satisfy sinϑ = 0 and sinψ= 0, as in the case of the eighth embodiment. Thus, ϑ1 = 0 and ϑ3 = π are fixed points independent of the phase difference to be determined øs (in this embodiment, proportional to the rotating angular velocity). ϑ5 = π to ϑ8 are solutions that satisfy sin ψ = 0, a condition that is added when the design conditions of the optical fiber gyro are converted into equations (27) to (29). ϑ2 and ϑ4, and ϑ5 to ϑ8 are all dependent on the phase difference øs. Therefore, øs can be determined by measuring the phase difference or angular velocty of rotation so as to decrease that rotation.

0154In addition, the car receives a signal representing angular velocity from the rolling sensor 512 and holds the car body stable while controlling the suspension elements on the right and left of the car body so as to limit changes in the height of the car body.

0155It is also possible to employ the apparatus of the present invention in an arrangement in which the fiber loop 40 is mounted in a vertical plane so as to detect the rotation of the earth on its own axis, or in which the fiber loop 40 is turned round a vertical axis so as to find an absolute azimuth from a detected change in the angular velocity of the rotation of the earth on its own axis.

0156In the above description, an analysis was carried out on the basis of sampling the signal corresponding to the detection of the modulated and interfering beams. However, an equivalent effect can be achieved by applying an electronic modulation to the output of the detector which detects the modulated and interfering beams. A sixth embodiment of t

0157The count control circuit 1050 generates a count start pulse at the phase timing ϑ1 and a first and second count stop pulse at the phase timing ϑ2 and ϑ3 respectively.

0158The counting circuit 1070 and the counting circuit 1090 measure the time interval Δ1 between ϑ5 and ϑ1 and a time interval Δ2 between ϑ2 and ϑ1, according to the instruction of the count start pulse and the first and second count stop pulses. At this time, the following equations (30) and (31) hold.<maths id="math0029" num="(30)"><math display="block"><mrow><mtext>øs + ηcos wmΔ1 = π</mtext></mrow></math><img file="EP0444843A2_D0029.tif" /></maths><maths id="math0030" num="(31)"><math display="block"><mrow><mtext>øs + ηcos wmΔ2 = 0</mtext></mrow></math><img file="EP0444843A2_D0030.tif" /></maths>

0159The arithmetic and logic circuit 1080 solves the equations (30) and (31) as simultaneous equations for øs and η . When the effective phase modulation index η thus obtained differs from a specified value (equation (5), the arithmetic and logic circuit 1080 adjusts the control signal to the phase modulator drive circuit 60 to keep at a specified value. The process of deriving the rotational angular velocity from the phase difference øs is the same as that carried out in the eighth embodiment.

0160As with the eighth embodiment, the fixed timing pulse gives the start timing for the above sequence of operations.

0161Rather than adjusting the control signal to the phase modulator drive circuit 60 to keep η at a specified value, the arithmetic and logic circuit 1080 may compensate for the quantity corresponding to the deviation in the value η.

0162Next, we will describe a tenth embodiment. Fig. 20 shows the configuration of the signal processing apparatus 100 of the third embodiment.

0163The conditions under which the optical fiber gyro of this embodiment is designed are similar to those of the eighth embodiment, except that a local oscillator 160 is provided to introduce a frequency converting means to improve the accuracy of measuring the extremum timing phase difference.

0164Fig. 20 shows the configuration of a signal processing apparatus according to the tenth embodiment.

0165In Fig. 20, the local oscillator 1600 generates a locally oscillated signal, which is a sinusoidal wave of angular frequency w_z, which is defined as follows.<maths id="math0031" num="(32)"><math display="block"><mrow><msub><mrow><mtext>w</mtext></mrow><mrow><mtext>z</mtext></mrow></msub><msub><mrow><mtext> = w</mtext></mrow><mrow><mtext>m</mtext></mrow></msub><mtext> -Δw</mtext></mrow></math><img file="EP0444843A2_D0031.tif" /></maths>

0166The local oscillation frequency w_z differs from the phase modulation angular frequency w_m by an angular frequency Δw. This oscillator operates according to the clock signals generated by the count clock generating circuit 1070.

0167Again the photoelectric conversion circuit 70 transforms the interference light into an electric signal and thereby generates an interference signal. The interference signal outputted from the photoelectric conversion circuit 70 enters the differentiating circuit 1010, where it is differentiated. The zero-crossing point of the differential signal is detected by the zero-crossing detection circuit 1020. A phase measuring oscillator 110 receives the extremum timing level from the zero-crossing detection circuit 102 and the level signal from the level comparison circuit 104 and generates a measurement-object signal, which is a sinusoidal wave whose zero-crossing point is at the phase of the maximum point. It also receives the fixed timing pulse from the fixed phase pulse generating circuit 103 and generates a measurement reference signal, being a sinusoidal wave whose zero-crossing point is the phase. The timing chart of these signals is shown in Fig. 21. The angular frequencies of the measuring signal and measurement reference signal are equal to the phase modulation angular frequency w_m.

0168The measuring signal outputted from the phase measuring oscillator 1100 is supplied to a mixer circuit 1110 where it is multiplied by the locally oscillated signal. Then, the output of the mixer circuit 1110 is fed to a low-pass filter 1130 which extracts only a measurement-object beat signal whose angular frequency is equal to the difference frequency Δ w between the phase modulation angular frequency w_m and the locally oscillated frequency w_z.

0169In other words, the frequency is changed by extracting, from a signal containing frequency components representing both the sum and difference of angular frequencies of two signals obtained as a result of multiplication, only the frequency component that represents the angular frequency difference.

0170To obtain the measurement reference signal, the same operation is performed, i.e., the measurement reference signal is fed to a mixer circuit 1120 and a low-pass filter 1140 and converted into a measurement reference beat signal whose angular frequency is equal to Δ w.

0171The count control circuit 1050 detects the zero-crossing points of the measurement reference beat signal and the measurement beat signal, and generates the count start and stop pulses at the corresponding zero-crossing timing. The counting circuit 1060, in response to the instruction of the count start and stop pulses, counts the count clock pulses from the count clock generating circuit 1070. The arithmetic and logic circuit 1080 reads the count value from the counting circuit 1060 to calculate the target phase difference øs and then converts it into a measurement of the angular velocity of rotation.

0172The phase modulator drive circuit 60 generates a phase modulation signal according to the count clocks from the count clock generating circuit 1070.

0173Now, the operation of the tenth embodiment will be described below.

0174Since the phase of the measurement reference signal is fixed and known, calculating the angular velocity output of the optical fiber gyro by using the equation (26) needs only measuring the phase difference Δϑ of the measurement signal with respect to the measurement reference signal, as mentioned in the eighth embodiment. Since there are two maximum points in one cycle of the phase modulation signal, as in the eighth embodiment, an alternative is to generate first and second measurement-object signals at these maximum point timings. In this case, the first and second maximums can easily be distinguished from each other by taking the fixed timing pulse as a reference. The phase difference of the light beams can be obtained from the phase difference between the first and second measurement-object signals.

0175Thus, in the tenth embodiment the measuring signal and the measuring reference signal are mixed with the locally oscillated signal to produce a low-frequency beat signal.

0176The measuring signal outputted from the phase measuring oscillator 1100 is fed to the mixer circuit 1110 to be multiplied by the locally oscillated signal. The output of the mixer circuit 1110 is passed through the low-pass filter 1130 to be converted into a measurement-object beat signal whose angular frequency is equal to the difference frequency Δw between the phase modulation angular frequency w_m and the locally oscillated frequency w_z.

0177The same operation is carried out also on the measurement reference signal. The measurement reference signal is sent to the mixer circuit 1120 and the low-pass filter 1140, and is transformed into a measurement reference beat signal of an angular frequency of Δ w.

0178The period T′ of these beat signals is expressed by equation (33).<maths id="math0032" num="(33)"><math display="block"><mrow><mtext>T′ = 2π/Δ w</mtext></mrow></math><img file="EP0444843A2_D0032.tif" /></maths>

0179In the above frequency conversion process, if the low-pass filters 113, 114 have the same phase characteristics, the phase difference between the measurement object signal and the measurement reference signal is retained as the phase difference between the measurement beat signal and the measurement reference beat signal.

0180In other words, as shown in Fig. 22, the phase relationship between the measurement-object beat signal and the measurement reference beat signal is identical to that between the measurement-object signal and the measuring reference signal before frequency conversion. Because the frequency has shifted to the beat signal frequency Δ w in the low frequency region, the measuring of the phase difference becomes relatively easy.

0181If the phase characteristics of the low-pass filters are not strictly identical, the offset phase difference that depends on the phase characteristic of the filter circuits may be examined beforehand and compensated for accordingly.

0182The detection of the phase difference between the measurement-object beat signal and the measurement reference beat signal can be realized as in the first embodiment.

0183That is, in Fig. 20 the count control circuit 1050 detects the zero-crossing points of the measurement reference beat signal and the measurement-object beat signal and generates count start and stop pulses at these zero-crossing timings.

0184In response to the pulses from the count control circuit 1050, the counting circuit 106 counts the clock pulses, the count value of which is supplied to the arithmetic and logic circuit 1080 which calculates the angular velocity according to equation (26), as the first embodiment. The timing relationships between these signals is shown in Fig. 22.

0185As explained above, the tenth embodiment shifts the phase difference measurement to the low frequency range by the frequency conversion, permitting measurement of phase difference or time integral with a higher resolution compared with that of the eighth embodiment when the same clock frequency is used.

0186In the tenth embodiment the locally oscillated signal, the measurement-object signal, and the measurement reference signal employ sinusoidal waves. However, the reference signals may be rectangular wave signals or other cyclically recurring signals. When rectangular waves are used, the mixer circuits 1110, 1120 may be formed by logic circuits using Exclusive-OR gates.

0187The frequency conversion employed in the tenth embodiment may be achieved by other means.

0188Next, an eleventh embodiment will be described. The eleventh embodiment mixed the interference signal and the phase modulation signal with the locally oscillated signal and modulates them into low-frequency signals.

0189Fig. 23 shows the configuration of the signal processing circuit 1000 of the eleventh embodiment.

0190The mixer circuit 1110 and the low-pass filter 1130 perform frequency conversion of the interference signal, while the mixer circuit 1120 and the low-pass filter 1140 perform frequency conversion of the phase modulator drive signal. A waveform shaping circuit 1200 modifies the shape of the locally oscillated signal generated by the local oscillator 1600. Other components are identical to those of the eighth embodiment, and corresponding reference numerals are used.

0191The operation of the eleventh embodiment will be now explained.

0192The design conditions of the optical fiber gyro of this embodiment are the same as those of the eighth embodiment, and the timings of signals are similar, except that the signals are processed in a low frequency range after the frequency conversion.

0193This reduces the weight in terms of phase or time integral measurement of each count clock pulse generated by the count clock generating circuit 1070, improving the resolution of measurement through counting a large number of pulses.

0194In order to retain the time waveform of the interference signal in the low frequency range, the locally oscillated signal must be such that a phase modulation angular frequency and its harmonic component contained in the locally oscillated signal have equal amplitude intensities. For this purpose, the eleventh embodiment includes a shaping circuit 1020 that modifies the shape of the locally oscillated signal generated by the local oscillator 1600.

0195While in the eleventh embodiment the time waveform of the signal is retained after the frequency conversion, the frequency conversion for retaining the time waveform need not be performed. Instead, other frequency conversion may be employed that will retain the correspondence between the signals before and after frequency conversion. In this case, the time intervals between points on the frequency-converted signal that correspond to the waveform characteristic points of the signal before being subjected to the frequency conversion may be measured to determine the phase difference between the interfering signals.

0196Next, a twelvth embodiment will be described.

0197The twelvth embodiment achieves frequency conversion by modulating the intensity of a light source 70 with a locally oscillated signal. This permits one mixer circuit in the eleventh embodiment to be eliminated. To retain the interference signal waveform in the low frequency region, each of the frequency spectra of the local oscillated signal is made to have equal amplitudes, as in the eleventh embodiment.

0198Fig. 24 shows the configuration of the signal processing apparatus of the twelvth embodiment.

0199The construction of the signal processing apparatus of the twelfth embodiment is similar to that of the eleventh embodiment except that the mixer circuit for mixing the interference signal and the locally oscillated signal is omitted. Thus, detailed explanation of the configuration of the circuit 1000 is not necessary.

0200Embodiments of the invention when applied to an optical fiber gyro have been discussed. However, this invention makes use of general properties of waves and thus can be applied not only to an optical fiber gyro but also to any apparatus or technique whereby physical quantities are measured by the interference of waves, such as phase-modulated electromagnetic waves (including light), sound waves or electron beams.

0201In the above eighth to twelfth embodiments, consideration is given to the time waveform of the interference signal and the optical phase difference of interfering waves is determined by measuring the phases of the characteristic points of the time waveform, i.e., time position or time interval of the characteristic points. Therefore, because analysis is in the time domain, not the frequency domain, no high-precision operational amplifier or analog digital converter is requited, making the electronic circuit simple. This invention also permits compensation of drift of a modulating means such as a phase modulator. Further, unlike systems that measure signal voltage amplitudes by a linear circuit with high accuracy, this invention can expand the dynamic range of interference measurement by using a high-speed clock or a frequency conversion means.

0202Also, as described above, an interference sensor according to the present invention permits lower frequencies to be processed owing to e.g., the use of "down sampling" and makes it possible to execute digital processing which has not been achievable with known interference sensors handling higher frequencies. This has the advantage that the interference sensor can be made small in size but provide good accuracy and that the interference sensor of the present invention may be applied to a rotational measuring sensor etc. for an automobile etc.