WO2011021262A1

WO2011021262A1 - Radar device

Info

Publication number: WO2011021262A1
Application number: PCT/JP2009/064390
Authority: WO
Inventors: 俊夫若山; 洋酒巻; 論季小竹
Original assignee: 三菱電機株式会社
Priority date: 2009-08-17
Filing date: 2009-08-17
Publication date: 2011-02-24
Also published as: JP5398838B2; JPWO2011021262A1

Abstract

Provided is a radar device capable of improving both distance resolution and velocity resolution at the same time. The radar device is provided with a Fourier transformation section (11) for extracting a signal in a section having the same width as pulses included in a transmission wave from a received signal, executing Fourier transformation on the extracted signal, and generating the received signal after the Fourier transformation, a peak extraction section (14) for extracting the signal component at the frequency point where the value of power is maximized from the received signal after the Fourier transformation as a maximum power frequency component, a multiplication section (15) for selecting two arbitrary components out of a plurality of the maximum power frequency components obtained at the same time intervals as the intervals of the pulses included in the transmission wave to calculate a complex conjugate product, and a multiplied-value integration section (16) for adding the complex conjugate product calculated by the multiplication section to a plurality of times of observations to calculate the complex conjugate product after the integration, and a velocity calculating section (17) for calculating the Doppler velocity from the phase of the complex conjugate product after the integration.

Description

Radar equipment

This invention relates to a radar apparatus that measures the distance to a target by transmitting and receiving electromagnetic waves.

Conventionally, a device such as a coherent rider is known as a device for measuring wind at a remote point. The coherent rider cuts out a reception IF (intermediate frequency) signal for each transmission pulse width, and calculates a Doppler frequency by frequency analysis such as Fourier transform (see, for example, Non-Patent Document 1).

Here, as shown in Non-Patent Document 1, when measuring the wind speed in the viewing direction of −37 to 37 m / s using laser light having a transmission wavelength of about 1.5 μm, the Doppler frequency is −50 ~ 50MHz. That is, since it is necessary to measure a Doppler frequency with a bandwidth of 100 MHz, based on the sampling theorem, the received signal is collected by AD conversion of 200 MSsample / s or more, and the frequency analysis is executed.

Further, the distance measurement is executed by applying pulse modulation to the transmission laser beam and measuring a transmission / reception time difference. Therefore, the distance resolution is determined by the pulse width. For example, in the coherent rider of Non-Patent Document 1, if the transmission pulse width is 200 ns, the distance resolution is 30 m.

On the other hand, the speed resolution is determined by the resolution of the Doppler frequency. Here, since the resolution of the Doppler frequency is the reciprocal of the observation time of the received signal, the resolution of the Doppler frequency becomes higher as the observation time becomes longer. However, the observation time of the received signal is at most the transmission pulse width.

Therefore, in the coherent lidar of Non-Patent Document 1, when the transmission pulse width is 200 ns, the resolution of the Doppler frequency is 5 MHz, and the speed resolution when the transmission wavelength is 1.5 μm is 3.75 m / s. Therefore, both the distance resolution and the speed resolution are determined by the transmission pulse width. Also, there is a relationship that the distance resolution is higher when the transmission pulse width is shorter, but the speed resolution is lower.

However, the prior art has the following problems.
In the coherent lidar of Non-Patent Document 1, the distance resolution when the transmission pulse width is 200 ns is 30 m. For example, since the diameter of one vortex of the wake turbulence generated behind the aircraft is about several tens of meters, It is not always sufficient distance resolution to accurately capture the structure of the vortex. At this time, since it is not realistic to reduce the velocity resolution below 3.75 m / s, after all, sufficient distance resolution cannot be obtained.

In the coherent rider, since the beam hardly spreads at a short distance, an extremely high angular resolution can be obtained as compared with a radar that transmits and receives radio waves. However, as described above, the distance resolution is insufficient.
As described above, the conventional coherent rider has a problem in that the distance resolution and the speed resolution are in a trade-off relationship with each other, so that both cannot be improved at the same time.

The present invention has been made to solve the above-described problems, and an object of the present invention is to obtain a radar apparatus capable of improving both distance resolution and speed resolution at the same time.

A radar apparatus according to the present invention radiates a transmission wave including a plurality of pulses generated by a transmission unit to a space and reflects a reception wave received by a target existing in the space using the transmission wave. A radar device that generates a received signal by frequency conversion and measures the distance to a target based on the delay time of the received signal with respect to the transmitted wave, and has the same width as the pulse included in the transmitted wave from the received signal The frequency of the power value is maximized from the Fourier transform unit that extracts the signal of the section having, and performs the Fourier transform on this signal to generate the received signal after the Fourier transform, and the received signal after the Fourier transform A peak extraction unit that extracts the signal component of the point as the maximum power frequency component and any two of the plurality of maximum power frequency components obtained at the same time interval as the interval of the pulses included in the transmission wave are selected. The complex conjugate product to calculate the complex conjugate product, the complex conjugate product calculated by the multiplication unit is added for a plurality of observations, a multiplication value integration unit to calculate the integrated complex conjugate product, and an integrated complex conjugate product And a speed calculation unit that calculates the Doppler speed from the phase.

According to the radar apparatus according to the present invention, in the radar apparatus that measures the distance to the target based on the delay time of the reception signal with respect to the transmission wave, the Fourier transform unit converts the pulse included in the transmission wave from the reception signal. A signal in a section having the same width is extracted, and a Fourier transform is performed on this signal to generate a received signal after the Fourier transform. The peak extraction unit extracts, as a maximum power frequency component, a signal component at a frequency point at which the power value is maximum from the received signal after Fourier transform. The multiplier selects any two of the plurality of maximum power frequency components obtained at the same time interval as the pulse interval included in the transmission wave, and calculates a complex conjugate product. The multiplication value integration unit adds the complex conjugate product calculated by the multiplication unit for a plurality of observations, and calculates a post-integration complex conjugate product. The velocity calculation unit calculates the Doppler velocity from the phase of the complex conjugate product after integration. Thereby, the distance resolution can be determined by the pulse width, and the velocity resolution can be determined by the pulse interval.
Therefore, it is possible to obtain a radar apparatus that can improve both distance resolution and velocity resolution at the same time.

It is a block block diagram which shows the radar apparatus which concerns on Embodiment 1 of this invention. Example 1 It is a schematic diagram which shows the amplitude shape of the transmission wave of the radar apparatus which concerns on Embodiment 1 of this invention. Example 1 It is a schematic diagram which shows the relationship between the transmission timing of the transmission wave in the radar apparatus which concerns on Embodiment 1 of this invention, and the reception timing of a received signal. Example 1 It is a block block diagram which shows the signal processing part of the radar apparatus which concerns on Embodiment 1 of this invention. Example 1 It is explanatory drawing explaining the generation | occurrence | production state of the unnecessary reflection component contained in a received signal in the radar apparatus which concerns on Embodiment 1 of this invention. Example 1 It is a schematic diagram which shows the Doppler spectrum of the received signal in the radar apparatus which concerns on Embodiment 1 of this invention. Example 1 In the radar apparatus which concerns on Embodiment 2 of this invention, it is explanatory drawing explaining the generation | occurrence | production state of the unnecessary reflection component contained in a received signal. (Example 2) It is a block block diagram which shows the signal processing part of the radar apparatus which concerns on Embodiment 2 of this invention. (Example 2) It is a schematic diagram which shows the amplitude shape of the transmission wave of the radar apparatus which concerns on Embodiment 3 of this invention. (Example 3)

Hereinafter, preferred embodiments of a radar apparatus according to the present invention will be described with reference to the drawings. In the drawings, the same or corresponding parts will be described with the same reference numerals.

Embodiment 1 FIG.
1 is a block diagram showing a radar apparatus according to Embodiment 1 of the present invention.
In FIG. 1, the radar apparatus includes a transmission unit 1, a switching unit 2, a radiation unit 3, a reception unit 4, an AD (Analog to Digital) conversion unit 5, and a signal processing unit 6.

The function of this radar apparatus will be described below.
The transmission unit 1 generates and outputs a transmission wave including a plurality of transmission pulses generated by amplitude-modulating a single frequency continuous wave. Further, the transmission unit 1 outputs a transmission wave to the reception unit 4.
In the first embodiment, the case where the transmission wave is a laser beam will be described. However, the transmission wave is not limited to the laser beam, but may be a general electromagnetic wave or a sound wave other than the frequency region of the light. However, the same can be applied.

The switching unit 2 outputs the transmission wave from the transmission unit 1 to the radiation unit 3 and outputs the reception wave from the radiation unit 3 to the reception unit 4.
The radiating unit 3 radiates the transmission wave from the switching unit 2 to the space, and receives a part of the transmission wave reflected by the target 100 existing in the space as a reception wave.

The receiving unit 4 converts the received wave input from the radiating unit 3 via the switching unit 2 into a received signal having an intermediate frequency (IF) using the transmitted wave from the transmitting unit 1. The intermediate frequency reception signal (IF reception signal) frequency-converted by the reception unit 4 is an analog signal.

The AD conversion unit 5 performs AD conversion (analog-digital conversion) on the IF reception signal from the reception unit 4 in order to digitally execute the signal processing, and digitized IF reception signal (hereinafter referred to as “reception signal”). Is abbreviated as "."
The signal processing unit 6 performs signal processing based on the received signal from the AD conversion unit 5.

Here, the amplitude shape of the transmission wave generated by the transmission unit 1 and radiated into the space by the radiation unit 3 is schematically shown in FIG.
In FIG. 2, the transmission wave includes two transmission pulses generated by amplitude-modulating a single frequency continuous wave. Here, a transmission wave shape composed of the pulse 101a and the pulse 101b is referred to as a frame.

The pulse width 102a of the pulse 101a and the pulse width 102b of the pulse 101b are equal to each other. Further, the transmission wave of one frame has a shape interrupted by the time interval 103, and the pulse interval 104a is an interval from the center of the pulse 101a to the center of the pulse 101b. The frame of the transmission wave is repeated at the time interval 105.

The pulse width 102a and the pulse width 102b are determined according to the distance resolution to be realized. When the desired distance resolution is Δr, the pulse width τ is expressed by the following equation (1). In the formula (1), c represents the speed of light.

Τ = 2Δr / c (1)

Further, when the time interval 105 is expressed as T, T is set so as to satisfy the following expression (2). In Expression (2), Rmax indicates the maximum observation distance.

T> 2Rmax / c (2)

Equation (2) means that the next frame is transmitted after the transmission wave reflected by the target existing at the maximum observation distance is received.

Subsequently, the relationship between the transmission timing of the transmission wave and the reception timing of the reception signal is schematically shown in FIG.
In FIG. 3, data recording by the AD conversion unit 5 is executed in a period from timing 116 to timing 117. Here, the timing 116 is set to be after the end of transmission of the pulse 101b, and the timing 117 is set to be before the start of the next transmission frame determined by the time interval 105. The received signal obtained during this period is assumed to be 110.

Note that the received signal 110 is sampled at a sampling interval Δt. The sample interval Δt is set so as to satisfy the following expression (3). In Equation (3), λ represents the transmission wavelength, and Va represents the width of the Doppler speed range to be measured.

Δt <λ / Va (3)

For example, when the measurement range of the Doppler velocity is from −Vmax to + Vmax (Vmax> 0), the width Va of the Doppler velocity range to be measured is expressed by the following equation (4).

Va = 2Vmax (4)

Further, when the speed measurement of the distance r is executed, the samples in the section 112a and the section 112b among the samples obtained by the AD conversion unit 5 are used. Assume that the widths of the section 112a and the section 112b are equal to the pulse width 102a and the pulse width 102b, respectively. The time interval 113 is also assumed to be equal to the time interval 103 between the pulse 101a and the pulse 101b.

Therefore, the time interval 114a from the center of the section 112a to the center of the section 112b is equal to the pulse interval 104a from the center of the pulse 101a to the center of the pulse 101b. At this time, when the time difference 118 between the pulse 101a and the pulse 111a is tr, tr is expressed by the following equation (5).

Tr = 2r / c (5)

Note that the above-described processing flow from the transmission unit 1 to the signal processing unit 6 is a conventional one. The feature of the radar apparatus according to the first embodiment of the present invention resides in signal processing by the signal processing unit 6 described below.

FIG. 4 is a block configuration diagram showing the signal processing unit 6 of the radar apparatus according to Embodiment 1 of the present invention.
In FIG. 4, the signal processing unit 6 includes a Fourier transform unit 11, a spectrum integration unit 12, a peak detection unit 13, a peak extraction unit 14, a multiplication unit 15, a multiplication value integration unit 16, a speed calculation unit 17, and a loop correction unit 18. Have.

Hereinafter, functions of the signal processing unit 6 will be described.
The Fourier transform unit 11 performs Fourier transform on the received signal from the AD conversion unit 5 for each of the pulse 112a and the pulse 112b. The received signal after Fourier transform obtained in this way has a peak at a frequency point corresponding to the Doppler frequency.

The spectrum integration unit 12 obtains the power spectrum of the received signal by calculating the power value of the received signal after the Fourier transform from the Fourier transform unit 11. Here, the spectrum integrator 12 adds power, that is, integrates the power spectrum obtained by a plurality of transmissions in order to improve detection performance when performing peak detection from the obtained power spectrum.
The peak detection unit 13 performs a peak detection process on the integrated power spectrum from the spectrum integration unit 12, detects a peak at which the power spectrum is maximum, and sets the frequency point at the peak position to the peak extraction unit 14 and The result is output to the aliasing correction unit 18.

The peak extraction unit 14 extracts the signal component at the frequency point detected by the peak detection unit 13 from the received signal after the Fourier transform obtained by the Fourier transform unit 11. Here, since the subsequent Doppler velocity is calculated using the phase information of the signal to be extracted, the signal component is extracted from the output of the Fourier transform unit 11 including the phase information. In addition, since the power spectrum integrated by the spectrum integration part 12 is a power value, it does not include phase information. Therefore, the power spectrum information is used only for extracting the frequency point at the peak position.

Specifically, the peak extraction unit 14 extracts a signal component from both the pulse 112a and the pulse 112b. Let the extracted signal components be a (i) and b (i), respectively. However, i has shown that it is a signal obtained by observation by the i-th transmission.
The multiplication unit 15 takes the complex conjugate product of the two signal components a (i) and b (i), thereby expressing the two signal components a (i) and b ( The cross-correlation value R (i) of i) is calculated.

The phase of the cross-correlation value R (i) represents how much the phase of the signal has advanced during the time interval 114a (= pulse interval 104a) shown in FIG. Therefore, the Doppler frequency can be calculated from the phase of the cross-correlation value R (i). However, the signal components a (i) and b (i) include unnecessary components.
Hereinafter, unnecessary components included in the signal components a (i) and b (i) will be described with reference to FIG. In FIG. 5, the horizontal direction indicates time, and the vertical direction indicates distance.

The pulse 101a and the pulse 101b of the transmission wave generated by the transmission unit 1 and radiated into the space from the radiation unit 3 are reflected by the target existing at the distance B, received by the section 112a and the section 112b, respectively, and after Fourier transform A signal component is extracted by the peak extraction unit 14 to become a signal component a (i) and a signal component b (i).
Here, the signal component a (i) includes an unnecessary reflection component in which the pulse 101b is reflected at the distance C, and the signal component b (i) includes an unnecessary reflection component in which the pulse 101a is reflected at the distance A. Therefore, the cross-correlation value R (i) includes the influence of unnecessary reflection components from the distance A and the distance C.

The multiplication value integration unit 16 integrates the cross-correlation value R (i) as expressed by the following equation (7) in order to remove the influence of the unnecessary reflection component, and the cross-correlation value R (tilde) after integration. Is calculated.

Since the unnecessary reflection component at the distance C is included only in the signal component a (i), there is no correlation with the signal component b (i), and the unnecessary reflection component at the distance A is the signal component b (i). Therefore, there is no correlation with the signal component a (i). Therefore, by taking an average of a plurality of observations, the unnecessary reflection component at the distance A and the distance C becomes relatively smaller than the reflection component from the distance B. Therefore, from Equation (7), if the number of integrations N is sufficiently large, the influence of the unnecessary reflection components from the distance A and the distance C on the post-integral cross-correlation value R (tilde) is sufficiently small.

The velocity calculation unit 17 calculates the Doppler velocity v _D using the following equation (8) from the phase of the post-integral cross-correlation value R (tilde) in which the influence of the unnecessary reflection component is reduced. In the equation (8), Ti represents a time interval 114a (= pulse interval 104a).

From equation (8), it can be seen that the velocity resolution is determined by the pulse interval. Further, the Doppler velocity v _D calculated by the equation (8) is a value calculated based on the phase difference at the time interval Ti. Therefore, when there is a phase rotation exceeding 2π during the time interval Ti, the calculated Doppler velocity v _D includes ambiguity. That is, the interval of the Doppler velocity v _{D that} can be calculated without ambiguity is λ / (2Ti).

On the other hand, in the Fourier transform of the section 112a or the section 112b, the speed calculation ambiguity is determined by the above-described sample interval Δt. Therefore, if the AD conversion unit 5 executes a sample with a sufficiently small sample interval Δt, the Doppler speed v _D is not ambiguous. Therefore, the ambiguity of the Doppler speed v _D calculated by the speed calculation unit 17 can be resolved by using the detection result of the peak detection unit 13.

However, with this Fourier transform, only the resolution of the Doppler frequency determined by the time length of the section 112a can be obtained. Specifically, since the time width of the section 112a is equal to the pulse width τ of the pulse 101a, the Doppler frequency resolution is 1 / τ and the Doppler velocity resolution is λ / (2τ).

Here, when the time interval Ti becomes larger than the pulse width τ, the resolution of the Doppler velocity by the Fourier transform becomes larger than the ambiguity included in the Doppler velocity v _D calculated by the velocity calculation unit 17.
This means that the Fourier transform is not accurate enough to completely eliminate the ambiguity of the speed calculation result of the speed calculation unit 17.

Therefore, it is considered that an estimated value is obtained with accuracy finer than the velocity resolution in the velocity estimation by Fourier transform. As an example, for example, a sequence of 0 is added (padded with 0) after a sequence of received signals input to the Fourier transform unit 11. As a result, the actual length of the received signal cannot be increased, but the apparent signal length can be increased.

FIG. 6 schematically shows the result when the Fourier transform is performed on the received signal after zero padding. In FIG. 6, a broken line represents a true Doppler spectrum.
In the Fourier transform for a received signal that is not zero-padded, as described above, the resolution of the Doppler frequency is 1 / τ, and the result of the Fourier transform is obtained as indicated by the black circle in FIG.

At this time, for example, if the Fourier transform is executed after adding 0 having the same length as the original received signal, the signal length to be subjected to the Fourier transform is doubled. Therefore, the resolution of the Doppler frequency can be halved. Therefore, in this case, the result of the Fourier transform can be obtained at the position of the white circle in FIG. As a result, the peak frequency extraction accuracy can be improved.

Thus, in the calculation of the velocity by Fourier transform, the Doppler velocity v _D can be calculated with higher accuracy than the velocity resolution determined from the conventional observation time. However, when the received signal contains noise, there is a limit to the improvement in speed resolution by the above-described method.

Therefore, in order to calculate the Doppler velocity v _D with higher accuracy, to calculate the Doppler velocity v _D by observation time longer received signal, i.e., the velocity calculation unit 17, the time interval 114a (= pulse interval 104a) Consider combining Doppler velocities v _D calculated according to the observation time.

Specifically, in consideration of ambiguity, the calculation result of the Doppler velocity v _D by the velocity calculation unit 17 is expressed by the following equation (9). In the formula (9), n is an integer, v _a denotes a Doppler velocity corresponding to 2 [pi.

The aliasing correction unit 18 has a true Doppler velocity v _D that is the closest to the Doppler velocity obtained at the peak of the power spectrum detected by the peak detector 13 among the Doppler velocities v _D obtained by changing the integer n. Assuming there is a measured value. The loopback correction unit 18 performs such ambiguity resolution, that is, speed loopback correction.

As described above, according to the first embodiment, in the radar apparatus that measures the distance to the target based on the delay time of the reception signal with respect to the transmission wave, the Fourier transform unit is included in the transmission wave from the reception signal. A signal in a section having the same width as the pulse to be extracted is extracted, and a Fourier transform is performed on this signal to generate a received signal after the Fourier transform. The peak extraction unit extracts, as a maximum power frequency component, a signal component at a frequency point at which the power value is maximum from the received signal after Fourier transform. The multiplier selects any two of the plurality of maximum power frequency components obtained at the same time interval as the pulse interval included in the transmission wave, and calculates a complex conjugate product. The multiplication value integration unit adds the complex conjugate product calculated by the multiplication unit for a plurality of observations, and calculates a post-integration complex conjugate product. The velocity calculation unit calculates the Doppler velocity from the phase of the complex conjugate product after integration. Thereby, the distance resolution can be determined by the pulse width, and the velocity resolution can be determined by the pulse interval.
Therefore, it is possible to obtain a radar apparatus that can improve both distance resolution and velocity resolution at the same time.

The aliasing correction unit receives the frequency obtained by extracting the maximum power frequency component by the peak extraction unit, obtains a coarsely accurate Doppler velocity from the frequency, and matches the coarsely accurate Doppler velocity with the velocity calculating unit. The loopback correction of the calculated Doppler speed is executed. The Fourier transform unit adds a series of 0 to the received signal before Fourier transform.
Therefore, the ambiguity included in the Doppler speed can be resolved and the Doppler speed can be calculated with high accuracy.

In the first embodiment, the aliasing correction unit estimates the frequency that is the center of gravity of the power value distribution in the vicinity of the frequency from which the maximum power frequency component is extracted by the peak extraction unit, and the Doppler speed with coarse accuracy from the frequency. In addition, the loop correction of the Doppler speed calculated by the speed calculation unit may be executed so as to match the Doppler speed with coarse accuracy.
In the first embodiment, the aliasing correction unit estimates a frequency at which the power value is maximum by applying a theoretical power distribution model to the power value distribution, and calculates a coarsely accurate Doppler speed from the frequency. In addition, the loop correction of the Doppler speed calculated by the speed calculation unit may be executed so as to match the coarse Doppler speed.
Furthermore, at this time, the transmission unit generates a transmission wave so that the interval of the pulses included in the transmission wave changes at a predetermined period for each transmission, and the aliasing correction unit performs the observation with the transmission waves having different pulse intervals. The loop correction of the Doppler speed may be executed so as to be consistent with all the Doppler speeds calculated by the speed calculation unit.
In these cases, the same effect as in the first embodiment can be obtained.

Embodiment 2. FIG.
In the first embodiment, the transmission wave including two transmission pulses in the transmission waveform has been described as an example. However, the present invention is not limited to this, and the transmission wave may include three or more transmission pulses. Good.
Hereinafter, a case where a transmission wave including three transmission pulses is used will be described.
FIG. 7 is an explanatory view schematically showing a state of transmission and reception in the radar apparatus according to Embodiment 2 of the present invention. In FIG. 7, as compared with FIG. 5, the number of transmission wave pulses 101c is increased, and the interval 112c of the received signal is increased.

In FIG. 7, the received signal includes reflected waves from distances D, E, and F in addition to reflected waves from distances A, B, and C. However, only the reflected wave from the distance B is received in a plurality of sections among the three

sections

112a, 112b, and 112c of the received signal. Therefore, for example, the Doppler speed v1 calculated using the received signals of the

sections

112a and 112b and the Doppler speed v2 calculated using the received signals of the

sections

112b and 112c are correct except for the return of the speed. Value.

Here, since the Doppler speed v1 and the Doppler speed v2 are different in the time interval of the received signals to be used, the method of returning the speed is different between the two. Therefore, if a value that can be matched between the Doppler speed v1 and the Doppler speed v2 calculated in consideration of ambiguity is selected, a correct Doppler speed without aliasing can be obtained.

FIG. 8 is a block diagram showing a signal processing unit 6A of the radar apparatus according to Embodiment 2 of the present invention.
In FIG. 8, the signal processing unit 6A includes a Fourier transform unit 11, a switching unit 19, spectral integration units 12a and 12b,

peak detection units

13a and 13b,

peak extraction units

14a and 14b,

multiplication units

15a and 15b, and a multiplication value integration unit. 16a, 16b, speed calculation units 17a, 17b, and a speed correction unit 20.

Further, in FIG. 8, the spectrum integration units 12a and 12b to the speed calculation units 17a and 17b are doubled. In addition, what added a to the code | symbol is a system which processes the received signal of the area 112a and the area 112b, and what added b to the code | symbol is a system which processes the received signal of the area 112b and the area 112c. That is, the switching unit 19 outputs a signal corresponding to the section 112a and the section 112b among the received signals after the Fourier transform from the Fourier transform section 11 to a system in which a symbol is added to the section 112b and the section 112c. The corresponding signal is output to a system with b added to the code.

The Doppler speed calculated by the speed calculation unit 17a and the Doppler speed calculated by the speed calculation unit 17b are equal to each other except for the return of the speed. Therefore, the speed correction unit 20 calculates a Doppler speed candidate assuming a plurality of numbers of folds for the Doppler speeds calculated by the speed calculation unit 17a and the speed calculation unit 17b, and sets a value that matches both to the correct Doppler. Select as speed.

As described above, according to the second embodiment, the transmission unit generates a transmission wave including three or more pulses, the multiplication unit calculates a complex conjugate product with a combination of different time intervals, and a speed calculation unit. Computes the Doppler velocity to match all of the post-integral complex conjugate products computed for different time interval combinations.
Therefore, even when the pulse interval is shortened in order to improve the distance resolution, the Doppler velocity can be calculated with high accuracy. Further, since three or more transmission pulses are included in the transmission waveform, aliasing correction is possible, and the Doppler speed can be calculated with high accuracy.

Embodiment 3 FIG.
In the second embodiment, the transmission wave including three or more transmission pulses in the transmission waveform has been described as an example. However, the present invention is not limited to this, and two transmission pulses included in the transmission waveform are used for transmission. A plurality of pulse intervals may be changed every time.
Hereinafter, a case will be described in which observation is performed by using a transmission wave including two transmission pulses and changing a plurality of pulse intervals for each transmission.
Since the configuration of the signal processing unit of the radar apparatus according to Embodiment 3 of the present invention is the same as that of Embodiment 2 described above, description thereof is omitted.

FIG. 9 is a schematic diagram showing the amplitude shape of the transmission wave of the radar apparatus according to Embodiment 3 of the present invention.
In FIG. 9, the transmission wave is transmitted at the pulse interval 104a in the first transmission, the pulse interval 104b in the second transmission, the pulse interval 104c in the third transmission, and the pulse interval 104d in the fourth transmission. Thereafter, it is continuously transmitted.

Here, the pulse interval 104a and the pulse interval 104c are the same interval, and the pulse interval 104b and the pulse interval 104d are also the same interval. The

pulse intervals

104b and 104d are longer than the

pulse intervals

104a and 104c. At this time, the Doppler velocity calculated using the reception signal corresponding to the transmission wave of the

pulse intervals

104a and 104c and the Doppler velocity calculated using the reception signal corresponding to the transmission wave of the

pulse interval

104b and 104d are: Each value is correct except for the return of speed.

Therefore, similarly to the second embodiment described above, in the speed correction unit 20, the Doppler speed calculated by the speed calculation unit 17a (corresponding to the transmission waves of the

pulse intervals

104a and 104c) and the speed calculation unit 17b are used. With regard to the Doppler speed (corresponding to the transmission waves of the

pulse intervals

104b and 104d), a Doppler speed candidate is calculated assuming a plurality of folding numbers, and a value matching both is selected as the correct Doppler speed.

As described above, according to the third embodiment, the transmission unit generates a transmission wave so that the interval between pulses included in the transmission wave changes at a predetermined cycle for each transmission, and the multiplication unit has an equal pulse. The complex conjugate product is calculated by the combination of intervals, and the velocity calculation unit calculates the Doppler velocity so as to match all of the post-integration complex conjugate products calculated for the combination of equal pulse intervals.
Therefore, similarly to the above-described second embodiment, the Doppler speed can be calculated with high accuracy even when the pulse interval is shortened in order to improve the distance resolution. In addition, since only two transmission pulses are included in the transmission waveform, the generation of unnecessary reflection components is small, and the Doppler velocity can be calculated at a plurality of pulse intervals. The speed can be calculated with high accuracy.

Claims

A transmission wave including a plurality of pulses generated by the transmission unit is radiated to the space, and the reception wave reflected and received by the target existing in the space is frequency-converted using the transmission wave to obtain a reception signal. A radar device that generates and measures a distance to the target based on a delay time of the received signal with respect to the transmission wave,
A Fourier transform unit that extracts a signal in a section having the same width as the pulse included in the transmission wave from the received signal, performs Fourier transform on the signal, and generates a received signal after Fourier transform;
A peak extraction unit that extracts a signal component of a frequency point at which the power value is maximum from the received signal after the Fourier transform, as a maximum power frequency component;
A multiplying unit that selects any two of the plurality of maximum power frequency components obtained at the same time interval as a pulse interval included in the transmission wave, and calculates a complex conjugate product;
A multiplication value integration unit that adds the complex conjugate product calculated by the multiplication unit for a plurality of observations and calculates a complex conjugate product after integration;
A velocity calculation unit for calculating a Doppler velocity from the phase of the complex conjugate product after integration;
A radar apparatus comprising:
The radar apparatus according to claim 1, wherein the transmission unit generates the transmission wave so that an interval between pulses included in the transmission wave is equal to or wider than a pulse width.
The radar device according to claim 1 or 2, wherein the transmission unit repeatedly generates the transmission wave at a time interval longer than a delay time of the reception signal corresponding to an assumed maximum observation distance.
The transmission unit generates the transmission wave including three or more pulses,
The multiplication unit calculates the complex conjugate product with a combination of different time intervals,
The said speed calculation part calculates the said Doppler speed so that it may match with all the said post-integration complex conjugate products calculated about the combination of a different time interval. Radar device.
The transmission unit generates the transmission wave so that an interval of pulses included in the transmission wave changes at a predetermined cycle for each transmission,
The multiplication unit calculates the complex conjugate product with a combination of equal pulse intervals,
The said speed calculation part calculates the said Doppler speed so that it may match with all the said post-integration complex conjugate products calculated about the combination of an equal pulse interval, The statement of any one of Claim 1- Claim 3 Radar device.
A frequency obtained by extracting the maximum power frequency component by the peak extraction unit is input, and a coarsely accurate Doppler velocity is obtained from the frequency, and is calculated by the velocity calculating unit so as to match the coarsely accurate Doppler velocity. The radar apparatus according to any one of claims 1 to 3, further comprising a folding correction unit that performs loop correction of the Doppler speed.
The radar device according to claim 6, wherein the Fourier transform unit adds a series of 0 to the received signal before Fourier transform.
In the vicinity of the frequency where the maximum power frequency component is extracted by the peak extraction unit, a frequency serving as the center of gravity of the power value distribution is estimated, and a coarsely accurate Doppler velocity is obtained from the frequency, and is matched with the coarsely accurate Doppler velocity. The radar apparatus according to any one of claims 1 to 3, further comprising a folding correction unit that performs looping correction of the Doppler speed calculated by the speed calculation unit.
By applying a theoretical power distribution model to the power value distribution in the vicinity of the frequency from which the maximum power frequency component is extracted by the peak extraction unit, the frequency at which the power value is maximum is estimated, and coarse accuracy is determined from the frequency. The apparatus further comprises a folding correction unit that performs looping correction of the Doppler speed calculated by the speed calculation unit so as to obtain a Doppler speed of the same and match the coarse Doppler speed. The radar apparatus according to any one of the above.
The transmission unit generates the transmission wave so that an interval of pulses included in the transmission wave changes at a predetermined cycle for each transmission,
The loopback correction unit executes loopback correction of the Doppler speed so that the Doppler speed is matched with all the Doppler speeds calculated by the speed calculation unit in observation using the transmission waves having different pulse intervals. Item 10. The radar device according to any one of Items 9 to 9.