Priority is claimed to Japan Patent Application Serial No. 2017-033282 filed on Feb. 24, 2017.
The present technology relates to a data processing method, which uses a computer to process measurement data of a wave, such as an electromagnetic wave, whose value is fixed by a frequency of the wave generated in a space and a value of a spatial coordinate of the space, and a measurement device which measures a wave and perform data processing thereof.
Conventionally, a radar apparatus, which employs an array antenna obtained by arranging a plurality of antenna on a plane, has been known for a method of inspecting an inside of a non-metal structure, such as concrete and wood, in a non-destructive manner. For example, the array antenna is configured by arranging antennas, such as planar antennas, side by side in one direction such that a transmission array antenna and reception array antenna are arranged to be adjacent to each other. In addition, in the radar apparatus, an object to be measured is measured using wide-band frequencies while changing a frequency of an electromagnetic wave with a set frequency interval in order to accurately measure the inside of the structure.
For the radar apparatus, it is desired to enhance high spatial resolution in measurement in order to accurately inspect the inside of the structure. In general, spatial resolution of data obtained by radiation of a wave having a frequency, such as an electromagnetic wave, is determined based on a center frequency of the wave when a distance between a structure that is an object to be measured and both of measurement surfaces of a transmission array antenna and a reception array antenna is relatively close, for example, the distance is a fourth of an array length of the array antennas and a measurement interval of measurement data is small. Herein, the spatial resolution is a resolution in a plane in which the respective antennas of the array antenna are arranged.
For example, a theoretical spatial resolution in a case where the measurement interval along the plane of the measurement data is sufficiently small becomes a fourth of a wavelength of the wave at a center frequency of a frequency band when the frequency of the radiating wave is swept with the frequency band on consideration of a reciprocating path of the electromagnetic wave. However, when the measurement interval of the measurement data is large, and this measurement interval exceeds a fourth of a minimum wavelength of the electromagnetic wave, the spatial resolution in actual measurement becomes rougher than the theoretical spatial resolution and becomes a measurement interval in some cases.
In regard to the radar apparatus using the array antenna, for example, a radar apparatus that is configured such that a transmission array antenna and a reception array antenna each of which is configured using a plurality of planar antennas are formed on the common dielectric substrate has been known (Japanese Unexamined Patent Application Publication No. 2015-095840 A). In this radar apparatus, an arrangement direction of the planar antennas of the transmission array antenna is parallel to an arrangement direction of the planar antennas of the reception array antenna, and each of the planar antennas of the reception array antenna is located between two adjacent planar antennas of the transmission array antenna in the arrangement direction.
In the above-described radar apparatus, an electromagnetic wave is measured with a wide frequency band from a low frequency to a high frequency, and thus, a maximum wavelength of the electromagnetic wave becomes long. Thus, a size of each antenna forming the array antenna becomes large, and a length of the antenna in the array antenna in the arrangement direction becomes long. As a result, an arrangement interval of the antennas in the reception array antenna becomes long, and the above-described measurement interval of measurement data is likely to exceed a fourth of a minimum wavelength of the radiating electromagnetic wave, the spatial resolution decreases to be rougher than the theoretical resolution, and further, an aliasing component is easily generated in the measurement data. It is necessary to decrease the arrangement interval and increase the number of arranged antennas of the reception array antenna in order to set the spatial resolution to be the theoretical spatial resolution (a fourth of the wavelength of the electromagnetic wave at the center frequency), which is in the most preferable condition. However, when the number of arranged antennas is increased, cost of the radar apparatus increases, and further, a circuit configuration of the radar apparatus becomes complicated, which is not preferable.
Thus, the present technology aims to provide a data processing method and a measurement device capable of improving the spatial resolution in measurement while maintaining the number of arranged antennas to be constant.
An aspect of the present technology is a data processing method that causes a computer to process measurement data of a wave whose value is fixed by a frequency of the wave generated in a space and a value of a spatial coordinate of the space.
The data processing method includes:
The extension processing is preferably performed using a corrected temporal waveform data set (e.g. d: see
The extension processing preferably includes:
The extension processing preferably includes
The extension processing more preferably includes causing the computer to execute repeatedly the step (E4) by using a calculation result obtained by multiplying or dividing the third extended/corrected frequency and wavenumber data (e.g. D3(kx, ky, ω)) by the ratio (e.g. [D1(kx, ky, ω)/D2(kx, ky, ω)]) as the processing data, and to determine the calculation result obtained after repeatedly executing the step (E4) a plurality of times as extended data of the first processing data.
A minimum frequency of the frequency can be set to be a half of the maximum frequency or higher.
A data interval of a spatial coordinate component (e.g. the y component) corresponding to the extended second wavenumber component is preferably a fourth or smaller of a wavelength corresponding to the maximum frequency.
When an object to be measured is irradiated with an electromagnetic wave from each of a plurality of transmission antennas arranged at a certain first interval in a first direction, the measurement data is preferably data, which is obtained by causing a reflected wave of the electromagnetic wave reflected from the object to be measured to be received by each reception antenna, which is at a position closest to each of the transmission antennas, among a plurality of the reception antennas. The reception antennas are preferably arranged at the first interval in the first direction and are provided to be shifted in the first direction by a length, which is a half of the first interval, with respect to arrangement of the transmission antennas. A sampling interval of a spatial coordinate component corresponding to the second wavenumber component is preferably a length which is a half of the first interval.
The second wavenumber component preferably includes a wavenumber component (e.g. the ky component) corresponding to a spatial coordinate component (e.g. the y component) in the first direction.
The second wavenumber component preferably includes a wavenumber component (e.g. the kx component) which corresponds to a spatial coordinate component (e.g. the x component) in a second direction that is an in-plane direction of a plane in which the transmission antennas and the reception antennas are provided and is orthogonal to the first direction.
Preferably, the transmission antennas and the reception antennas relatively move with respect to the object to be measured in the second direction.
The first spatial coordinate component (e.g. the z component) is preferably a spatial coordinate component in a normal direction of the plane in which the transmission antennas and the reception antennas are provided.
When all the wavenumber components are set to kx, ky, and kz and the frequency is set to f, the restraint condition is preferably kx2+ky2+kz2=4×εr×(ω/c0)2, where c0 is speed of light in vacuum, εr is a relative dielectric constant of a medium propagated in the electromagnetic wave, and ω is 2πf.
Another aspect of the technology is a measurement device that measures a wave whose value is fixed by a frequency of the wave generated in a space and a value of a spatial coordinate of the space and performs data processing. The measurement device includes:
The data processing unit includes:
The second processor is configured to perform extension processing of extending a maximum wavenumber of a second wavenumber component, which corresponds to at least one of the second spatial coordinate components, on the first processing data.
The second processor preferably includes:
The fifth processor preferably includes:
Preferably, the fifth processor further includes:
The transmission unit preferably includes a plurality of transmission antennas which are configured to emit an electromagnetic wave to an object to be measured and are arranged at a certain first interval in a first direction. The reception unit preferably includes a plurality of transmission antennas which are configured to receive reflected wave of the electromagnetic wave reflected from the object to be measured and are arranged at the first interval in the first direction. The reception antennas are preferably provided to be shifted in the first direction by a length, which is a half of the first interval, with respect to arrangement of the transmission antennas. A sampling interval of a spatial coordinate component corresponding to the second wavenumber component is preferably a length which is a half of the first interval.
Examples of the measurement device include a radar apparatus.
According to the data processing method and the measurement device described above, it is possible to improve the spatial resolution in measurement.
Hereinafter, a data processing method and a measurement device according to an embodiment of the present technology will be described in detail.
A radar apparatus 60 according to an embodiment illustrated in
In (2) described above, the extended first processing data obtained by extending the maximum wavenumber is calculated in order to suppress generation of an aliasing component in the third processing data.
In this manner, in the present embodiment, it is possible to shorten at least one measurement interval (sampling interval) of the x-coordinate component and the y-coordinate component of the third processing data when the triple inverse DFT processing is performed. The shortened measurement interval is achieved by extending the range in which at least one of the kx component and the ky component can vary, that is, the maximum wavenumber. The shortened measurement interval is achieved even in the case of sampling a response of the space of the electromagnetic wave with a sampling interval which is rough as compared to the spatial resolution determined from a maximum frequency of frequencies according to a sampling theorem. The response is sampled regarding at least one of the x-coordinate component and the y-coordinate component (second spatial coordinate components) except for the z-coordinate component (first spatial coordinate component) among the spatial coordinate components of the space. Accordingly, it is possible to suppress the generation of the aliasing component. Hereinafter, embodiments will be described in detail using the radar apparatus 60.
The radar apparatus 60 includes a measurement unit 61, a data processing unit 66, and an image display unit 68. The measurement unit 61 includes a transmission array antenna 50, a reception array antenna 52, high-frequency switches 58 and 59, a high-frequency circuit 62, and a system control circuit 64. The radar apparatus 60 allows the electromagnetic wave of 10 MHz or higher, for example, 10 to 20 GHz to radiate, but a frequency of the electromagnetic wave is not particularly limited thereto.
In the present embodiment, arrangement directions of transmission antennas 10a in the transmission array antenna 50 and reception antennas 10b in the reception array antenna 52 are parallel to each other, and these arrangement directions is set as a y-direction as illustrated in
In the transmission array antenna 50, a plurality of the transmission antennas 10a are arranged in one direction, that is, the y-direction, and the respective transmission antennas 10a causes electromagnetic waves to radiate toward the object to be measured.
In the reception array antenna 52, a plurality of the reception antennas 10b are arranged along the y-direction, which is the arrangement direction of the transmission antennas 10a, and the respective reception antennas 10b receive electromagnetic waves reflected from the object to be measured. The transmission antennas 10a of the transmission array antenna 50 and the reception antennas 10b of the reception array antenna 52 are provided on one plane, and the transmission array antenna 50 and the reception array antenna 52 are arranged such that this plane faces the object to be measured.
The data processing unit 66 processes a plurality of measurement data, obtained by performing transmission toward the object to be measured using the plurality of transmission antennas 10a of the transmission array antenna 50 and reception using the plurality of reception antennas 10b of the reception array antenna 52, thereby calculating image data of the object to be measured. The transmission antennas 10a and the reception antennas 10b according to an embodiment are preferably planar antennas in which an antenna pattern is formed to be planar on a substrate. However, the transmission antennas 10a and the reception antennas 10b are not limited to the planar antennas.
The transmission array antenna 50 and the reception array antenna 52 are configured to move in parallel to a surface of the object to be measured. That is, the transmission array antenna 50 and the reception array antenna 52 perform measurement while scanning along the surface of the object to be measured. When the transmission array antenna 50 and the reception array antenna 52 move, the system control circuit 64 controls an operation of the high-frequency circuit 62 such that the electromagnetic wave radiates while switching the transmission antennas 10a of the transmission array antenna 50 every unit length of a movement distance of the transmission array antenna 50 and the reception array antenna 52 by the high-frequency switch 58. The movement of the transmission array antenna 50 and the reception array antenna 52 is sensed by an encoder 69 which is integrally provided in the substrate in which the transmission array antenna 50 and the reception array antenna 52 are provided and generates a pulse signal every certain movement distance. At this time, a plurality of the receptions of the reception antennas 10b by sequentially switching the plurality of reception antennas 10b every time when the electromagnetic wave radiates from the respective transmission antennas 10a are performed using the high-frequency switch 59.
Incidentally, the electromagnetic wave is caused to radiate while sweeping the frequency of the electromagnetic wave radiating from the transmission array antenna 50 in a range of 10 to 20 GHz, for example, in a certain period of time at a set frequency interval. Accordingly, the measurement data obtained from the high-frequency circuit 62 is data whose value is fixed based on a reception position of the reception antenna 10b and the frequency.
At this time, the operation of the high-frequency switch 59 is controlled such that the reflected wave of the electromagnetic wave on the object to be measured is received by the reception antenna 10b that is the closest to the transmission antenna 10a from which the electromagnetic wave has radiated. A microwave amplifier for reception (RF amplifier) is set such that a gain is changed for each pair of the transmitting transmission antenna 10a and the receiving reception antenna 10b. It is also possible to increase a depth of a defect or the like that can be inspected in the object to be measured by providing a variable gain amplification function capable of switching a gain depending on selection of a pair of the transmission antenna 10a and the reception antenna 10b.
When the number of the arranged reception antennas 10b is increased in the radar apparatus 60, cost of the radar apparatus increases, and further a circuit configuration of the radar apparatus becomes complicated. Thus, it is difficult to increase the number of the arranged reception antenna 10b. Thus, a sampling interval Δy (see
The data processing unit 66 processes the measurement data s(x′, y′, ω), which is obtained by the transmission and reception of the electromagnetic wave using the transmission array antenna 50 and the reception array antenna 52, and generates the third processing data which corresponds to the image data representing the inside of the object to be measured. The data processing unit 66 is, for example, configured in a computer. It is possible to demonstrate a function of the data processing unit 66 by calling out and activating a program stored in a storage unit 66a. That is, the data processing unit 66 can be configured using a software module. An image inside the object to be measured is displayed on the image display unit 68 using the generated image data.
Herein, f(x, y, z) and s(x′, y′, ω) has a relationship of the following Formula (1).
Wherein, k=ω/c (c=c0/εr1/2, where c0 is the speed of light in vacuum, and εr is the relative dielectric constant of the object to be measured).
In the above-described Formula (1), the electromagnetic wave is expressed as a spherical wave, and distance attenuation is omitted. The distance attenuation has no influence on the following process, and thus, is omitted. If an exponent part of an integrand of an expression at the second line in the above-described Formula (1) is expressed in the Fourier transform, the following Formula (2) is obtained.
Herein, kx, ky, and kz are wavenumber components of a wavenumber vector k of the electromagnetic wave, each corresponding to the x-coordinate component, the y-coordinate component, and the z-coordinate component. The wavenumber vector k is the wavenumber vector of an electromagnetic wave propagated while reciprocating between the above-described transmitting and receiving point and a reflection point of the object to be measured. Herein, an exponent part of an expression at the first line and an exponent part of an expression at the second line are the same in the Formula (2), and thus, kx, ky, and kz satisfy an expression of kx2+ky2+kz2=4k2(=4×εr×(ω/c0)2). This expression is a restraint condition to be described later.
Herein, Formula (2) can be simplified as Formula (3).
Herein, an inner part { } of an expression at the second line in the above-described Formula (3) is an expression of the triple Fourier transform relating to x, y, and z. In addition, an outer part of [ ] of an expression at the second line is an expression of the double inverse Fourier transform relating to kx and ky. Thus, when the double Fourier transform is performed on both the sides in relation to x′ and y′, a function of f(x, y, z) after being subjected to the Fourier transform is set as F(kx, ky, kz), and a function of the measurement data s(x′, y′, ω) after being subjected to the Fourier transform is set as S(kx, ky, ω), the expression at the second line in the above-described Formula (3) can be written as the following Formula (4).
S(kx,ky,ω)=F(kx,ky,kz)efk
F(kx,ky,kz)=S(kx,ky,ω)e−ik
When the triple inverse Fourier transform is performed on both the sides of an expression at the second line in the Formula (4) with respect to kx, ky, and kz, it is possible to obtain the third processing data f(x, y, z), which is a final target, as the following Formula (5).
Herein, Formula 5 can be simply summarized as the following. Formula (6) by setting the position of the transmitting and receiving point in the z-direction such that z0=0.
That is, the third processing data f(x, y, z) is calculated, in the data processing according to the present embodiment, by performing the double Fourier transform on the measurement data s(x′, y′, ω) with respect to x and y, then, converting kx, ky and ω into the kz component using the angular frequency ω under the restraint condition of kx2+ky2+kz2=4k2 (=4×εr×(ω/c0)2)), and performing the triple inverse Fourier transform on the converted result in relation to the kx component, the ky component, and the kz component. This data processing is implemented by the data processing unit 66.
To be specific, the data processing unit 66 is provided with a first processor 66b, a second processor 66c, and a third processor 66d, and is configured to calculate f(x, y, z) whose value is fixed by values of the x-coordinate component, the y-coordinate component, and the z-coordinate component, which are all the spatial coordinate components inside the space, from the measurement data s(x′, y′, ω). The second processor 66c is provided with a fourth processor 66c1 and a fifth processor 66c2 as illustrated in
The first processor 66b is configured to calculate first processing data S(kx, ky, ω) by converting the x-coordinate component and the y-coordinate component (second spatial coordinate components) of the measurement data s(x′, y′, ω) into the kx component and the ky components as the wavenumber components. That is, the first processing data S(kx, ky, ω) is a wavenumber conversion result of the measurement data s(x′, y′, ω), and the value of the S(kx, ky, ω) is fixed by values of the positive and negative kx component and ky component corresponding to the x-coordinate component and the y-coordinate component, and the angular frequency ω (or the frequency f). In the present embodiment, the x-coordinate component, the y-coordinate component, and the angular frequency ω or the frequency f are the variables taking discrete values, and thus, a discrete Fourier transform (DFT) is used as the Fourier transform or the wavenumber conversion. In addition, the inverse DFT is used as the inverse Fourier transform.
The second processor 66c is configured to calculate second processing data S′(kx, ky, kz) whose value is fixed by values of the kx component, the ky component, and the kz component corresponding to all the spatial coordinate components inside the space by reconstructing the first processing data S(kx, ky, ω). The kz component is obtained from the angular frequency ω (or the frequency f), the kx component, and the ky component under the restraint condition (kx2+ky2+kz2=4×εr×(ω/c0)2) among the kx component, the ky component, and the kz component, which are all the wavenumber components corresponding to all the spatial coordinate components inside the space, and the angular frequency ω (or the frequency f). Details of the above-described reconstruction will be described later.
The third processor 66d is configured to calculate the third processing data f(x, y, z) by converting all the wavenumber components of the second processing data S′(kx, ky, kz) into all the spatial coordinate components (the triple inverse Fourier transform). The value of the f(x, y, z) is fixed by values of all the spatial coordinate components (the x-coordinate component, the y-coordinate component, and the z-coordinate component)
A value of the kz component, which satisfies the above-described restraint condition with respect to a value of the kx component, a value of the ky component, and a value of ω of the first processing data S(kx, ky, ω), is obtained in the reconstruction, which is performed for the calculation of the second processing data performed by the second processor 66c.
Herein, the values of the kx component, the ky component, and ω are represented by discrete values. For example, a positive kx component is represented as kx=nkx/(Nkx/2)kxmax, a negative kx component is represented as kx=(nkx−Nkx)/(Nkx/2)kxmax, a positive ky component is represented as ky=nky/(Nky/2)kymax, a negative ky component is represented as ky=(nky−Nky)/(Nky/2)kymax, and ω is represented as ω=(nf/Nf)2π fmax.
Herein, Nkx and Nky are the number of measurement points of each of the x-coordinate component and the y-coordinate component. Further, nkx is an integer that is 0 or larger and smaller than Nkx, and nky is an integer that is 0 or larger and smaller than Nky, which are discrete value parameters which determine values of the kx component and the ky component. Assuming that Nkx and Nky are even numbers, the positive kx component and ky component correspond to that nkx is 1 or larger and Nkx/2 or smaller and nky is 1 or larger and Nky/2 or smaller, and the negative kx component and ky component correspond to that nkx is Nkx/2+1 or larger and smaller than Nkx, and nky is Nky/2+1 or larger and smaller than Nky. Further, kxmax and kymax are the respective maximum wavenumbers of the kx component and the ky component, and are π/Δx and π/Δy which are determined based on the sampling theorem. Herein, Δx is a sampling interval (measurement interval) in the x-direction (scan direction) illustrated in
The kz component is also subjected to the inverse DFT processing as described above, and thus, a positive kz component is represented as kz=nkz/(Nkz/2)kzmax, and a negative kz component is represented as kz=(nkz−Nkz)/(Nkz/2)kzmax. Herein, Nkz is a sampling number of the z-coordinate component. Further, nkz is an integer that is 0 or larger and smaller than Nkz, and is a discrete value parameter that determines the value of the kz component. Assuming that Nkz is an even number, the positive kz component corresponds to that nkz is 1 or larger and Nkz/2 or smaller, and the negative kz component corresponds to that nkz is Nkz/2+1 or larger and smaller than Nkz. Further, kzmax is a maximum wavenumber of the kz component and is π/Δz which is determined based on the sampling theorem. Herein, Δz is a data interval in the z-direction illustrated in
In this manner, the value of the kx component, the value of the ky component, the value of ω, and the value of the kz component are discretized, and thus, it is difficult to determine the discrete value parameter nkz, which corresponds to the kz component, as the integer at the time of converting ω to kz. Thus, it is preferable to set a value of the discrete value parameter nkz as an integer from 0 to Nkz in order, and at this time, calculate a value of ω obtained under the restraint condition using a value of the kx component and a value of the ky component, and calculate a value of the first processing data S(kx, ky, ω) based on the calculated value of ω, the value of the kx component, and the value of the ky component using interpolation of the first processing data S(kx, ky, ω).
However, the second processing data S′(kx, ky, kz) reconstructed by such conversion from ω to kz causes generation of aliasing in the third processing data f(x, y, z) when the triple inverse DFT processing is performed on the second processing data S′(kx, ky, kz).
The generation of the aliasing component is caused when the response of the space of the electromagnetic wave is sampled at the sampling interval rougher than the spatial resolution which is determined according to the sampling theorem from the maximum frequency fmax of the frequency, for the y-coordinate component. Accordingly, when the rough sampling for the y-coordinate component is performed, the extension of the wavenumber is performed for the first processing data S(kx, ky, ω) in order to suppress the generation of the aliasing component in the third processing data f(x, y, z) in the present embodiment. In the following description, the case of extending the maximum wavenumber of the ky component from kymax to 2 kymax will be mainly described in order to facilitate the understanding. However, the following method can be applied to not only the extension of the maximum wavenumber of the ky component but also extension of a maximum wavenumber of the kx component, and further, can be applied to a case of simultaneously extending the maximum wavenumbers of the kx component and the ky component.
In the present embodiment, the reconstruction is performed using the extended first processing data.
As illustrated in
First, a temporal waveform data set including temporal waveform data whose waveform is provided for each of value of the y-coordinate component is generated by performing double inverse DFT processing on the first processing data S(kx, ky, ω) in order to convert a set of the ky component and the frequency into a set of the y-coordinate component and a time component (Step ST100). The ky component is intended for extending the maximum wavenumber of the first processing data S(kx, ky, ω).
Next, a corrected temporal waveform data set including corrected temporal waveform data whose waveform is provided for each value of the y-coordinate component. In the corrected waveform data, only values of data points of a local maximum values of absolute values of the temporal waveform data on a time base is held, and values other than the value of the data point of the local maximum value are set as zero (Step ST102). The corrected waveform data is generated for each value of the y-coordinate component, in the generated temporal waveform data set.
The fourth processor 66c1 illustrated in
It is possible to extract information on the low frequency, which is a minimum frequency or lower, by generating such a corrected temporal waveform even when the minimum frequency of the frequency is a half the maximum frequency fmax or higher, for example, when the minimum frequency is 10 GHz or higher for the maximum frequency of 20 GHz. This point will be described later.
Next, the fifth processor 66c2 performs Steps ST104 to ST108 illustrated in
That is, the fifth processor 66c2 is configured to perform the extension processing using the corrected temporal waveform data set which is generated in Step ST102.
A processor A of the fifth processor 66c2 arranges the corrected temporal waveform data set in a range of 1 to M of the y-coordinate component before being extended and a range of 1 to N of the time component before being extended on an extended coordinate space. In the extended coordinate space, the range of the y-coordinate component (corresponding spatial coordinate component) of the corrected temporal waveform data set d and the range of the time component are extended from 1 to M and 1 to N, respectively, to 1 to 2·M and 1 to 2·N. By such arrangement, a first corrected temporal waveform data set d1 including first corrected temporal waveform data is generated.
In this manner, the processor A generates the first extended/corrected temporal waveform data set d1, and the processor B generates the second extended/corrected temporal waveform data set d2 (Step ST104).
Next, a processor C of the fifth processor 66c2 generates a ratio between the first extended/corrected frequency and wavenumber data D1(kx, ky, ω) and the second extended/corrected frequency and wavenumber data D2(kx, ky, ω) (Step ST106). The first extended/corrected frequency and wavenumber data D1(kx, ky, ω) that is expressed by the kx component, the ky component (second wavenumber component) and the frequency is obtained by performing the double DFT processing on the first extended/corrected temporal waveform data set d1. The second extended/corrected frequency and wavenumber data D2(kx, ky, ω) that is expressed by the kx component, the ky component (second wavenumber component) and the frequency is obtained by performing the double DFT processing on the second extended/corrected temporal waveform data set d2. When a value of the ratio at this time is one or more, the value is set to one.
Further, a processor D of the fifth processor 66c2 generates a third extended/corrected temporal waveform data set d3 including third extended/corrected temporal waveform data d3 by arranging the corrected temporal waveform data dij at a certain interval, for example every other one, of the y-coordinate components (corresponding spatial coordinate components) on the extended coordinate space, that is, in the extended range of 1 to 2·M of the y-coordinate component and the extended range of 1 to 2·N of the time component, and assigning the value 0 to a portion other than the portion in which the corrected temporal waveform data dij is arranged.
A processor E of the fifth processor 66c2 generates third extended/corrected frequency and wavenumber data D3(kx, ky, ω) that is expressed by the kx component, the ky component (second wavenumber component) and the frequency by performing the double DFT processing on the third extended/corrected temporal waveform data set d3.
Further, the processor E multiplies or divides the third extended/corrected frequency and wavenumber data D3(kx, ky, ω) by the ratio generated in Step ST106 or by the processor C.
In this manner, extended first processing data S2(kx, ky, ω) obtained by extending the first processing data is generated (Step ST108).
The ratio, which is used for generation of the extended first processing data S2(kx, ky, ω) in this manner, is [D1(kx, ky, ω))/D2(kx, ky, ω)] in the case illustrated in
In this manner, the maximum wavenumber among the wavenumbers is extended by generating the waveform data of the y-coordinate component through interpolation using the ratio having the filter function that suppresses generation of the aliasing component in the extension processing according to the present embodiment, and thus, the ratio is also referred to as an interpolation filter.
The aliasing component is not sufficiently removed in some cases only by applying such an interpolation filter once. Thus, the interpolation filter is preferably applied a plurality of times in the present embodiment as will be described hereinafter.
As illustrated in
Next, the processor G of the fifth processor 66c2 multiplies or divides the third extended/corrected frequency and wavenumber data D3(kx, ky, ω) by the ratio [D1(kx, ky, ω)/D2(kx, ky, ω)]. D3(kx, ky, ω) is expressed by the kx component, the ky component (second wavenumber component) and the frequency and is obtained by performing the double DFT processing on the newly generated third extended/corrected temporal waveform data set d3.
In this manner, the ratio, that is, the interpolation filter can be used twice.
Further, it is also possible to generate the third extended/corrected frequency and wavenumber data D3(kx, ky, ω) again in the processor G by applying a result of the calculation of the third extended/corrected frequency and wavenumber data D3(kx, ky, ω) and the ratio in the expression illustrated in
In this manner, the ratio, that is, the interpolation filter can be repeatedly used a plurality of times.
Accordingly, it is possible to suppress the generation of the aliasing component. The number of times of application of the ratio, that is, the interpolation filter may be a predetermined number. In addition, the ratio, that is, the interpolation filter processing may be repeatedly performed until a level of the aliasing component included in a result obtained by multiplication or division between the third extended/corrected frequency and wavenumber data D3(kx, ky, ω) and the ratio [D1(kx, ky, ω)/D2(kx, ky, ω)] fits within a predetermined range.
In this manner, a reason why the information on the low frequency is extracted by performing the local maximum value processing is because the information on the low frequency is information that is necessary for generation of the interpolation filter. The interpolation filter demonstrates the function of suppressing the aliasing component using the information on the low frequency.
The result obtained by applying the ratio (interpolation filter) for the first time, illustrated in
As described above, the extension processing of the first processing data S(kx, ky, ω) includes the interpolation filter processing using the local maximum value processing and the ratio (interpolation filter) according to the flow illustrated in
Such extension and reconstruction are performed by the second processor 66c. Accordingly, the second processing data S′(kx, ky, kz) calculated by the second processor 66c includes the extended ky component.
The data processing unit 66 first acquires the measurement data s(x′, y′, ω) and stores the acquired data in the storage unit 66a (ST10).
Then, the first processor 66b calculates the first processing data S(kx, ky, ω) by performing frequency conversion processing (DFT processing) with respect to to the x-coordinate component and the y-coordinate component, on the measurement data s(x′, y′, ω) (ST12).
Then, the second processor 66c generates the extended first processing data S2(kx, ky, ω) in which the extended data is incorporated into the first processing data S(kx, ky, ω) by increasing kymax by extending the ky component of the first processing data S(kx, ky, ω) as described above (ST14).
Further, the second processor 66c calculates the second processing data S′(kx, ky, kz) from the extended first processing data S2(kx, ky, ω) by seeking the kz component (first wavenumber component) using the angular frequency ω (or the frequency f), the kx component, and the ky component under the restraint condition of kx2+ky2+kz2=4×εr×(ω/c0)2 (ST16).
Finally, the third processor 66d calculates the third processing data f(x, y, z) by performing a process of converting (inverse DFT) the kx component, the ky component, and the kz component of the second processing data S′(kx, ky, kz) into the x-coordinate component, the y-coordinate component, and the z-coordinate component (ST18). The value of f(x, y, z) is fixed by values of the x-coordinate component, the y-coordinate component, and the z-coordinate component.
In this manner, the ky component can be extended since the measurement number Nf of the frequency f of the electromagnetic wave is large, and the measurement data s(x′, y′, ω) includes information related to a wavenumber of the ky component larger than the value of the maximum wavenumber of the ky component kymax(=π/Δy) that is determined based on the sampling theorem at the sampling interval Δy. In particular, Δy is the sampling interval of the transmitting and receiving points determined by the transmission antenna 10a and the reception antenna 10b, Thus, to decrease Δy results in the increase of the number of the arranged transmission antennas and reception antennas. Accordingly, Δy is restricted. In the present embodiment, it is possible to increase the maximum wavenumber of the ky component kymax by extending the ky component described above even when the sampling interval Δy is large. Thus, the data interval of the y-coordinate component of the third processing data f(x, y, z) obtained by the inverse DFT processing becomes shorter. For example, when the maximum wavenumber kymax becomes n times, the data interval of the y-coordinate component becomes 1/n times. Accordingly, it is possible to improve the spatial resolution in the measurement. For example, it is possible to set the spatial resolution to be the theoretical resolution (a fourth of the wavelength corresponding to the center frequency of the electromagnetic wave). Although the example of extending the ky component has been described in the present embodiment, the kx component can be also extended. Since the x-direction is the scan direction of the transmission array antenna 50 and the reception array antenna 52 as illustrated in
Of course, it is also possible to simultaneously extend the kx component and the ky component using three factors of the kx and ky components, and the frequency at the same time in the local maximum value processing used at the time of the above-described extension and the processing using the interpolation filter. In this case, the triple DFT processing and the triple inverse DFT processing are used instead of the double DFT processing and the double inverse DFT processing.
When the measurement data s(x′, y′, ω) is set such that Δx=2 mm, a measurement number Nx of the x-coordinate component (=Nkx)=256, Δy=7.5 mm, a measurement number Ny of the y-coordinate component (=Nky)=64, the maximum frequency fmax=20 GHz, a minimum frequency fmin=10 GHz, the measurement number Nf=64, and the relative dielectric constant εr=1, for example, a fourth of the minimum wavelength (the wavelength of 15 mm at the maximum frequency of 20 GHz) of the electromagnetic wave is 3.75 mm. Since Δx=2 mm is a fourth of the minimum wavelength (=3.75 mm) or smaller, the spatial resolution in the x-direction is 5 mm which is a fourth of a wavelength (minimum wavelength) at a center frequency of 15 GHz in the frequency band of 10 to 20 GHz, that is, the theoretical resolution. However, Δy=7.5 mm is larger than a fourth of the above-described minimum wavelength (=3.75 mm), and thus, the spatial resolution in the y-direction is 7.5 mm which is larger than a fourth of the above-described minimum wavelength. The spatial resolution in the y-direction is rough as compared to the theoretical resolution of 5 mm.
In the present embodiment, the ky component is extended by setting the sampling number Nky of the ky component as 2 Nky, and doubling the maximum wavenumber of the ky component kymax such that the sampling interval of the y-coordinate component after being processed becomes π/(2 kymax) when the inverse DFT processing is performed. Thus, the sampling interval becomes 3.75 mm which is a half of Δy=7.5 mm. Accordingly, this sampling interval is a fourth of the wavelength of the minimum wavelength or smaller (=3.75 mm), the spatial resolution in the y-direction becomes the theoretical resolution of 5 mm.
In this manner, the sampling interval (data interval) of the y-coordinate component becomes 1/n by extending the ky component n times. Accordingly, it is preferable that the sampling interval (data interval) corresponding to the extended ky component be a fourth of the minimum wavelength, which is the wavelength corresponding to the maximum frequency, or smaller in order to improve the spatial resolution in the y-direction in the radar apparatus 60 or the data processing according to the present embodiment. That is, it is preferable to extend the ky component such that the sampling interval (data interval) of the y-coordinate component becomes a fourth of the minimum wavelength, which is the wavelength corresponding to the maximum frequency, or smaller. At this time, it is preferable to repeat extension of the range of the ky component, the extension being arranged to double the range of the ky component before being extended each time such that the sampling interval (data interval) of the y-coordinate component becomes a fourth of the above-described minimum wavelength or smaller in the radar apparatus 60 or the data processing according to the present embodiment.
In such a preferable aspect, the ky component is set as the extension target, but the kx component can be set as an extension target when Δx is larger than a fourth of the above-described minimum wavelength. In addition, the kx component and the ky component can be also set as extension targets, simultaneously.
In the radar apparatus 60 or the data processing according to the present embodiment, a method (single-pass method) of using the pair of the transmission antenna 10a and the reception antenna 19b, which are the closest to each other, is used as the transmission and reception method of the electromagnetic wave. However, it is also possible to use a method (multi-pass method) of obtaining measurement data by causing the reflected wave of the electromagnetic wave radiating from the single transmission antenna 10a to be received not only by the reception antenna 10b which is the closest to this transmission antenna but also by the reception antenna 10b at a position separated from the transmission antenna. However, it is preferable to use the single-pass method described above. That is, the following aspect is preferable. The measurement data s(x′, y′, ω) is the data that can be obtained by causing the reflected wave of the electromagnetic wave that is transmitted from each of the plurality of transmission antennas 10a to be received by the reception antenna 10b at the position the closest to the corresponding transmission antenna 10a among the plurality of reception antennas 10b. The reception antennas 10b are arranged in the y-direction at the first interval (2Δy in
In the radar apparatus 60 or the data processing according to the present embodiment, the wavenumber component to be extended preferably includes the ky component which corresponds to the y-coordinate component in the arrangement direction (the y-direction) of the transmission antenna 10a and the reception antenna 10b.
In addition, the wavenumber component to be extended preferably includes the kx component which corresponds to the x-coordinate component in the x-direction, which is an in-plane direction of the plane in which the transmission antenna 10a and the reception antenna 10b are provided, and is orthogonal to the y-direction in the radar apparatus 60 or the data processing according to the present embodiment.
In the radar apparatus 60 or the data processing according to the present embodiment, the transmission antenna 10a and the reception antenna 10b preferably scan the object to be measured while relatively moving in the x-direction.
Incidentally, the restraint condition used at the time of obtaining the kz component from ω in the present embodiment is preferably kx2+ky2+kz2=4×εr×(ω/c0)2 (c0 is the speed of light in vacuum, εr is a relative dielectric constant of a medium propagated in the electromagnetic wave, and ω=2πf).
Although the data processing method and the measurement device according to the present technology have been described in detail as above, the present technology is not limited to the above-described embodiment. It is a matter of course that various types of improvement and modifications may be performed in a range without departing from a gist of the present technology.
Number | Date | Country | Kind |
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2017-033282 | Feb 2017 | JP | national |