WO2006013614A1 - レーダ装置 - Google Patents
レーダ装置 Download PDFInfo
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- WO2006013614A1 WO2006013614A1 PCT/JP2004/011055 JP2004011055W WO2006013614A1 WO 2006013614 A1 WO2006013614 A1 WO 2006013614A1 JP 2004011055 W JP2004011055 W JP 2004011055W WO 2006013614 A1 WO2006013614 A1 WO 2006013614A1
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- Prior art keywords
- frequency
- distance
- radar
- radar apparatus
- wave
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/08—Systems for measuring distance only
- G01S13/32—Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated
- G01S13/34—Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated using transmission of continuous, frequency-modulated waves while heterodyning the received signal, or a signal derived therefrom, with a locally-generated signal related to the contemporaneously transmitted signal
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/50—Systems of measurement based on relative movement of target
- G01S13/52—Discriminating between fixed and moving objects or between objects moving at different speeds
- G01S13/536—Discriminating between fixed and moving objects or between objects moving at different speeds using transmission of continuous unmodulated waves, amplitude-, frequency-, or phase-modulated waves
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/50—Systems of measurement based on relative movement of target
- G01S13/58—Velocity or trajectory determination systems; Sense-of-movement determination systems
- G01S13/583—Velocity or trajectory determination systems; Sense-of-movement determination systems using transmission of continuous unmodulated waves, amplitude-, frequency-, or phase-modulated waves and based upon the Doppler effect resulting from movement of targets
- G01S13/584—Velocity or trajectory determination systems; Sense-of-movement determination systems using transmission of continuous unmodulated waves, amplitude-, frequency-, or phase-modulated waves and based upon the Doppler effect resulting from movement of targets adapted for simultaneous range and velocity measurements
Definitions
- the present invention relates to a technique for suppressing unwanted signals in a radar, and in particular, by combining the characteristics of a continuous wave radar and the characteristics of a pulse radar, the resolution of the continuous wave radar and the unnecessary signal by the pulse radar are related.
- the present invention relates to radar technology that simultaneously achieves suppression. Background art
- radar systems for use in automobiles include pulse radar, pulse compression radar (spread spectrum radar), frequency modulation continuous wave radar (FMCW radar, FMCW: Frequency Modulated Continuous Wave), 2 frequency CW level. ⁇ Gu (CW: Continuous Wave) is known.
- the pulse radar system transmits short pulses with sufficient distance resolution.
- Pulse compression radar is a radar system that transmits a wide-band signal with a wide pulse width by spectrum spreading and obtains a predetermined distance resolution by compression (despreading).
- Pulse radar and pulse compression radar require a bandwidth of 150 (MHz) to obtain a distance resolution of lm, and the computation load of correlation processing is large and high-speed signal processing is required. This is a disadvantageous method for the required on-vehicle radar.
- the FMCW radar system and the two-frequency CW radar system can obtain a distance resolution of about lm in a receiver band of several ⁇ ( ⁇ ), and will be widely used in automotive radars in the future. Expected.
- the received signal includes reflected waves from moving targets and stationary objects at any distance. It will be rare. As a result, when there are many strong clutters, it is difficult to estimate the target distance and target speed by mistake.
- Patent Document 1 Japanese Patent No. 3102224
- Patent Document 2 Japanese Patent Laid-Open No. 2002-071793
- the method according to Patent Document 2 is characterized in that a slope period in which the frequency changes is provided in a part of two frequency periods of the transmission wave.
- a slope period in which the frequency changes is provided in a part of two frequency periods of the transmission wave.
- the two-frequency CW method has a problem in principle that if the difference between the two frequencies is not sufficient, distance ambiguity occurs due to the return of the distance.
- the maximum detection distance required for a car-mounted radar is about 150m. If you try to select two frequencies to suppress the distance ambiguity while achieving this maximum detection distance, you must keep the difference between the two frequencies below l (MHz).
- the present invention is intended to solve the above-described problem, and it is easy to suppress clutter while pulsing the continuous wave and taking over the characteristic of continuous wave, which is high resolution. For the purpose of proposing a radar system with the characteristics that pulse radar is proud of!
- a radar apparatus according to the present invention provides:
- a radar device that obtains the frequency of the beat signal obtained by mixing the signal and the reference continuous wave and calculates the distance and speed of the external target.
- Band selection processing means for classifying the frequency components of the beat signal based on the spectrum spread corresponding to the pulse width of the Norse transmission wave
- At least one of the relative distance and relative speed of the moving target reflecting the pulse transmission wave and the relative distance of the stationary target reflecting the pulse transmission wave is determined.
- the continuous wave referred to here may be any of FMCW, dual frequency CW, and step chirp continuous wave. Regardless of the radar system using any continuous wave, by adopting the features of the present invention, high resolution and unnecessary wave suppression can be achieved at the same time.
- the radar apparatus classifies the frequency components of the beat signal based on the spectrum spread corresponding to the pulse width, the clutter is mixed while maintaining the resolution of the continuous wave radar system.
- the frequency component corresponding to the moving external target can be efficiently selected from the frequency components of the beat signal. Therefore, false detection of external targets can be suppressed and the reliability of radar measurement results can be improved.
- FIG. 1 is a block diagram showing a configuration of a radar apparatus according to Embodiment 1 of the present invention
- FIG. 2 is a block diagram showing a detailed configuration of the radar apparatus according to Embodiment 1 of the present invention.
- FIG. 3 is a diagram showing waveforms of transmission / reception pulses by the radar apparatus according to Embodiment 1 of the present invention.
- FIG. 4 is an explanatory diagram for explaining the relationship between transmission / reception pulses and sampling intervals by the radar apparatus according to Embodiment 1 of the present invention
- FIG. 5 is a block diagram showing a detailed configuration of a radar apparatus according to Embodiment 2 of the present invention.
- FIG. 6 is a diagram showing waveforms of transmission / reception pulses by the radar apparatus according to Embodiment 2 of the present invention.
- FIG. 7 is a block diagram showing a detailed configuration of a radar apparatus according to Embodiment 3 of the present invention.
- FIG. 8 is a block diagram showing a detailed configuration of the radar apparatus according to Embodiment 4 of the present invention.
- 9] A block diagram showing a detailed configuration of a radar apparatus according to Embodiment 5 of the present invention.
- FIG. 1 is a block diagram showing a configuration of a radar apparatus according to Embodiment 1 of the present invention.
- the radar device 1 shown in the figure is a moving body that moves at a velocity V (also called a mobile platform).
- the reference signal generator 11 is a circuit or element that generates a reference signal having a predetermined continuous waveform.
- the frequency of the reference signal generated by the reference signal generator 11 rises continuously at regular intervals. Repeat the frequency drop.
- a radar system that measures the relative speed and relative distance of an external target using such frequency-modulated waves is known as the FMCW radar system.
- the noise generator 12 is an element or circuit that converts the reference signal generated by the reference signal generator 11 into a pulse signal having a predetermined pulse width. Where T is the predetermined pulse width
- the circulator 13 is an element or circuit that switches the connection of the antenna 14 between the pulse generator 12 and the receiver 15 at regular intervals.
- the antenna 14 functions as a transmitting antenna when connected to the pulse generator 12 by the circulator 13 and functions as a receiving antenna when connected to the receiver 15.
- the antenna 14 is configured as a transmission / reception antenna in order to simplify the configuration of the device, but a configuration in which the transmission antenna and the reception antenna are independent may be employed. Needless to say. In that case, a component such as the circulator 13 is not necessary.
- the antenna 14 irradiates the external target 2 with the pulse signal generated by the pulse generator 12 as a transmission wave 81-a.
- the transmitted wave 8 li is reflected by the external target 2 and arrives at the antenna 14 again as a reflected wave 81-b.
- the receiver 15 performs detection processing on the received signal obtained by the antenna 14 receiving the reflected wave 81-b, converts it to a digital signal at the sampling interval T, and then digitizes the digital signal.
- the signal processor 16 is a circuit or element that detects the relative distance and relative speed of the external target 2 based on the beat signal generated by the receiver 15.
- FIG. 2 is a block diagram showing a detailed configuration of the signal processor 16.
- a phase shifter 17 is a circuit or element for facilitating signal processing by adjusting the phase of the beat signal based on the own speed obtained from an unillustrated own speed sensor.
- the frequency analyzer 18 is a circuit or element that performs a fast Fourier transform (hereinafter referred to as "FFT") on the signal output from the phase rotation compensator 17 and performs frequency analysis. is there.
- FFT fast Fourier transform
- the band selection processor 19 is based on the speed obtained by the frequency analyzer 18 based on its own speed. This is a circuit or element that classifies the signal frequency into a frequency component corresponding to a moving external target and a frequency component corresponding to a stationary external target.
- FIG. 3 shows the time variation of the frequency of the continuous wave and the frequency of the transmission / reception pulse generated by the reference signal generator 11.
- the broken line shown as the transmission wave frequency is the frequency of the continuous wave generated by the reference signal generator 11.
- the reference signal generator 11 generates a linear FM modulated wave whose frequency increases for a certain period and then decreases for a certain period.
- the period during which the frequency rises is called the frequency rise period or up-chirp.
- the period during which the frequency drops is called the frequency drop period or down-chirp.
- the time length of the frequency modulation period, such as the frequency rise period or the frequency fall period is called the sweep time, and is expressed as T here.
- the difference between the lower limit and the upper limit of the frequency is called the sweep bandwidth and is represented by B.
- the amplitude of the transmission signal T (t) generated by the reference signal generator 11 during the frequency rise period is
- Equation (1) the envelope is set to 1 for simplicity.
- the transmission frequency f is 76.5 (GHz) and the sweep bandwidth B is about 100.
- a set of one frequency rise period and one frequency fall period is generally called a burst. Although only one burst is shown in the figure, the reference signal generator 11 actually repeatedly generates a plurality of burst reference signals.
- the pulse generator 12 converts a part of the continuous wave generated by the reference signal generator 11 to a pulse width T.
- a transmission nors 82-a and a transmission nors 83a are generated as transmission pulses.
- the transmission pulses 82-a and 83-a are radiated from the antenna 14 to the space as a transmission wave 81-a via the circulator 13.
- a part of the external target 2 is reflected, and the reflected radio wave arrives at the antenna 14 again as received pulses 82-b and 83-b.
- the reception pulse 82-b is a reflection of the transmission pulse 82-a
- the reception pulse 83-b is a reflection of the transmission pulse 83-a.
- the broken line indicated as the reception wave frequency represents the reception wave frequency when the transmission wave shown in the equation (1) is reflected by the external target 2 and arrives at the antenna 14 as the reception wave. is there.
- the received wave with respect to the transmitted wave represented by Equation (1) is affected by the time delay and Doppler shift due to the distance to the external target 2 and the relative speed of the external target 2.
- Equation 2 It becomes.
- the envelope is also 1.
- V is the relative speed of external target 2 and c is the speed of light.
- ⁇ is a term representing the time delay, and R is the relative distance to the external target 2.
- the receiver 15 samples the received noise at a sampling interval ⁇ .
- Figure 4 shows the layout of
- the distance R (k) of the external target 2 is
- Equation (2) the reception wave expressed by Equation (2) and the transmission wave expressed by Equation (1) are mixed and LPF (Low Pass Filter) is applied.
- LPF Low Pass Filter
- the receiver 15 also mixes the reception signal in the imaginary part, and obtains the complex beat signal B (t) of Expression (7) in the frequency increase period.
- the receiver 15 obtains the complex beat signal B (down t) of Expression (8) even in the frequency drop period.
- the frequency of the beat signal is determined by the distance R to the external target 2 and the relative speed V of the external target 2. Therefore, once the beat signal frequencies B (up t) and B (t) are determined, the external target 2 down is obtained by solving the simultaneous equations (7) and (8).
- the receiver 15 also generates a beat signal for the received reception wave in the same manner as the FMCW radar described above.
- the external target of interest is only one of the external targets 2, the relative distance of the external target 2 is R, and the relative velocity ⁇ V.
- other radio waves are also generated.
- the relative distance of each reflector is RC and the relative speed is vc ⁇ . Further, as described at the beginning of the first embodiment, it is considered that the speed of the radar apparatus 1 is V. Then, during a frequency rise period within a certain sweep time
- the sampling data (beat signal) B (k, n) obtained when sampling k times after the nth transmission of the noise is
- the second term corresponds to radio waves reflected by other reflectors and can be regarded as clutter. Therefore, ⁇ represents the complex amplitude of each clutter reflected wave. As can be seen from the second term force in Eq. (9), the clutter frequency f is
- the signal processor 16 performs frequency filtering.
- the signal processor 16 first acquires the complex beat signal generated by the receiver 15.
- the phase shifter 17 adjusts the phase of the beat signal so that the frequency of the spectrum center of the clutter spectrum clutter becomes almost zero.
- the phase shift adjustment method depends on the time delay: number k and relative speed V as shown in equation (11).
- the frequency analyzer 18 applies the equation (12) up to the phase-adjusted beat signal Y (k, n).
- Equation (12) N is the total number of pulses transmitted at the sweep time T, and m is the order of the frequency spectrum component.
- the band selection processor 19 classifies the output channels of the FFT into output channels satisfying the equation (13) and other output channels.
- An output channel satisfying the equation (13) may have a clutter spectrum. It is le.
- BSC band stop channel
- CFC Clutter Free Channel
- Equation (13) ⁇ f is the frequency spectrum spread of the clutter and depends on the spread ⁇ f and angle as shown in Equation (14).
- the distance error ⁇ f is obtained by using the uniform distribution error ⁇ R obtained by the equation (15),
- the relative speed with the reflector that generates clutter is the maximum value in the moving direction of the platform. As the angle with the direction of the antenna 14 increases, the relative speed with the reflector that generates clutter decreases. Go. At this time, the Doppler frequency difference ⁇ between the direction of the antenna 14 and the direction of the transmission angle ⁇ is
- the distance 'velocity detector 20 searches for the absolute value peak of the spectrum F (k, m) in the CFC. Spectrum of frequency rise period is F (k, m), spectrum of frequency fall period is up
- F (k, m) is the frequency and the absolute value of F (k, m) and the absolute value of F (k, m) peak.
- BSC down may be used.
- the radar apparatus 1 of the first embodiment of the present invention by dividing the FFT output channel of the beat signal into bands, the false detection probability of the target distance ′ speed is reduced. be able to.
- phase of the beat signal is adjusted by the phase shifter 17 in the radar device 1. Instead of such processing, a channel having a center frequency depending on the time delay sampling number. In this case, the phase shifter 17 can be omitted.
- the fast Fourier transform which is best known as a spectral analysis method, is used, but other methods may be used.
- the second embodiment of the present invention shows that unnecessary waves can be suppressed by dividing the FFT output channel of the beat frequency into bands even in the two-frequency CW radar system.
- FIG. 5 is a block diagram showing the configuration of the signal processor 16 according to the second embodiment of the present invention. As apparent from comparison with the configuration of the signal processor in the first embodiment shown in FIG. 2, the phase shifter 17 is omitted in the signal processor 16 in the second embodiment of the present invention.
- FIG. 6 shows the time series of the reference signal generated by the reference signal generator 11 of the radar apparatus 1 and the pulses generated by the pulse generator 12 and the received pulses received by the antenna 14 in the second embodiment of the present invention.
- the reference signal generator 11 generates a reference signal 84 having a frequency f for a time T, and then generates a reference signal 85 having a frequency f2 only for the time T. Then, the reference signal generator 11 repeats a plurality of bursts with a period of the reference signal 84 and the reference signal 85 as one burst.
- the pulse generator 12 pulses the reference signal 84 and the reference signal 85 to generate a transmission signal.
- the generated transmission signal is radiated from the antenna 14 to the space via the circulator 13.
- the reflected waves from the external target 2 and the stationary reflector are incident on the antenna 14 with a time delay depending on the distance of the reflectors and a Doppler frequency change depending on the relative velocity.
- This received signal is input to the receiver 15 via the circulator 13.
- the receiver 15 performs IQF mixing of the reference signal (local signal) of the frequency f generated by the reference signal generator 11 and the received signal in the reception section of the frequency f, and performs LPF processing.
- Output signal B is obtained.
- the reference of the frequency f generated by the reference signal generator 11 is used.
- the envelope is assumed to be 1 for simplicity.
- T is the pulse width
- n is the pulse number
- V is the relative speed of the external target 2
- R is the distance to external target 2 and c is the speed of light.
- the same target has the same Doppler frequency in both intervals of frequency f and f. Therefore, the frequency
- the operation of the band selection processor 19 is almost the same as in the first embodiment.
- the clutter spread of the reflected wave from a stationary reflector that does not spread the spectrum due to time delay is ⁇ f
- the distance 'speed detector 20 is the same frequency channel at the frequency f and frequency f from the CFC by the band selection processor 19.
- the target speed is obtained from the frequency at which the peak is obtained in the absolute value. Also, the target distance can be obtained from the phase difference force equation (20) for that frequency.
- the frequency component can be separated into the moving target and the stationary target based on the spectrum spread even in the two-frequency CW radar system.
- Embodiment 3 shows a radar apparatus using HPF (High Pass Filter).
- FIG. 7 is a block diagram showing a detailed configuration of the signal processor 16 of the radar apparatus according to Embodiment 3 of the present invention.
- a novel part compared to the first embodiment is that an HPF (High Pass Filter) 21 is provided.
- HPF High Pass Filter
- speed information from an unillustrated self-speed sensor is also input to HPF21. Since other components are the same as those in the first embodiment, description thereof is omitted.
- the beat signal input to the signal processor 16 is first shown in Equation (11) to facilitate signal processing in the phase shifter 17.
- the phase rotation compensation as described above is performed.
- HPF21 performs HPF processing in the pulse direction for each time delay sampling number k of the beat signal compensated for phase rotation.
- HPF processing is performed in the pulse direction for each time delay sampling number k of the beat signal. This means that HPF processing is performed for the value.
- the sampling value obtained by performing the k-th sampling is Y (k, n).
- the filter output W (n) of HPF21 is the filter coefficients a, a,
- W (n) a x W (n _ 1) + a 2 W (n _ 2) +... ten ( ⁇ _ /?)
- the frequency analyzer 18 and the band selection processor 19 operate in the same manner as in the first embodiment, and finally the distance and speed of the external target are output through the distance / speed detector 20.
- the frequency analyzer 18 This problem is alleviated by installing HPF21 to suppress clutter power before.
- a radar apparatus using an adaptive filter is shown in a fourth embodiment as another embodiment of the present invention.
- FIG. 8 is a block diagram showing a detailed configuration of the signal processor 16 of the radar apparatus according to Embodiment 4 of the present invention.
- a novel part compared to the first embodiment is that an adaptive filter 22 is provided in place of the phase shifter 17 and the frequency analyzer 18. Since the other components are the same as those in Embodiments 1 to 3, description thereof is omitted.
- the adaptive filter 22 is called AMTI (Adaptive Moving Target Indicator). J82-B, No.3, pp.461-468, March, 1999. (hereinafter referred to as Non-Patent Document 1).
- the operations of the reference signal generator 11, the pulse generator 12, the circulator 13, the antenna 14, and the receiver 15 are the same as those in the first embodiment.
- the signal processor 16 first acquires the sampling value of the beat signal output from the receiver 15 and performs filter processing using the adaptive filter 22.
- the filter output value W (n) for the nth pulse is the force applied filter 22 given by the equation (24).
- the adaptive filter 22 also filters the kth sampling data at the time of pulse transmission and the sampling data force before and after that.
- the MSN filter is a FIR (Finite Impulse Response) filter that ignores the influence of the filter output value on pulses other than the nth pulse in calculating the filter value of the nth pulse.
- the coefficients a, a,..., A of W (n ⁇ 1) – W (n ⁇ p) appearing on the right side of Equation (24) are considered to be zero.
- Equation (27) the output data vector of the receiver 15 at the time of the k-th sampling of the n-th pulse.
- the correlation is based on the data vector of the reference interval
- the mean of the matrix R is estimated as follows:
- Equation (28) H represents the complex conjugate transpose of the matrix, and ⁇ *> represents the average operation in the reference interval.
- V (m) is as follows.
- the adaptive filter coefficient is R-m
- the adaptive filter output W (m) for the m-th order frequency component is
- an adaptive filter can be calculated to perform a plurality of filterings that divide the required band, similarly to the coefficients in the FFT.
- the output of the adaptive filter 22 is classified into CFC and BSC in the band selection processor 19, and the distance, speed, and stationary target of the external target moving in the distance 'speed detector 20 are set. The distance is calculated.
- Non-Patent Document 1 an adaptive filter is applied between FMCW sweeps.
- the FMCW continuous wave is pulsed, and then pulse direction sampling in each sweep is performed. There is a difference that an adaptive filter is applied to the data.
- FIG. 9 is a block diagram showing a detailed configuration of the signal processor 16 of the radar apparatus according to Embodiment 5 of the present invention.
- the form of implementation A novel part compared with state 3 is that a super-resolution spectrum estimator 23 is provided in place of the frequency analyzer 18. Since other components are the same as those in the third embodiment, description thereof is omitted.
- the super-resolution spectrum estimator 23 uses MUS IC (Multiple signal and lassincation nom ⁇ iiiisPRnXEstimation of the super-resolution spectrum estimation method between each pulse for the sampling data when k times are sampled after each pulse transmission signal Parameters via Rotational Invariance Technique) ⁇
- a circuit or element that performs likelihood A circuit or element that performs likelihood.
- the super-resolution spectrum estimator 23 calculates the correlation matrix of the data vector W by the equation (32).
- the resolution spectrum estimator 23 calculates the noise eigenspace E by Equation (34).
- the MUSIC spectrum is calculated by the evaluation function represented by Expression (35) using the steering vector V and the noise eigenspace E.
- the super-resolution spectrum estimator 23 searches the peak of the evaluation function of Equation (35) to obtain the frequency.
- a spectrum can be obtained by MUSIC as well as FFT. Therefore, the output result of the super-resolution spectrum estimator 23 is classified into CFC and BSC in the band selection processor 19 and the frequency value force that becomes the peak of the absolute value is also moved in the distance / speed detector 20. Calculate the distance and speed of the target, as well as the distance of the stationary external target.
- the bandwidth selection processor 19 can perform the processing! What will change! /
- the band selection processor 19 determines whether the frequency value that is the output result of the super-resolution spectrum estimator 23 is included in the difference between CFC and BSC. Try to sort.
- the clutter composed of many reflected waves is suppressed in advance. Yes.
- the wave number is limited to the number of moving targets existing within the pulse width, and the effect of facilitating the application of the super-resolution spectrum estimation method is produced. Therefore, with these super-resolution spectrum estimation methods, it is possible to estimate the spectrum with higher resolution than the spectrum estimation by FFT, that is, when the same sweep band B is used, the target distance The resolution of speed is improved and the adjacent targets can be separated.
- the present invention can be applied to a radar apparatus that separates and measures the positions and velocities of a plurality of targets such as an on-vehicle radar apparatus.
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Application Number | Priority Date | Filing Date | Title |
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US11/658,997 US7671788B2 (en) | 2004-08-02 | 2004-08-02 | Apparatus and method for suppression of unnecessary signals in a radar system |
EP04748188A EP1777548A4 (en) | 2004-08-02 | 2004-08-02 | RADAR |
JP2006531051A JP4668198B2 (ja) | 2004-08-02 | 2004-08-02 | レーダ装置 |
PCT/JP2004/011055 WO2006013614A1 (ja) | 2004-08-02 | 2004-08-02 | レーダ装置 |
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PCT/JP2004/011055 WO2006013614A1 (ja) | 2004-08-02 | 2004-08-02 | レーダ装置 |
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EP (1) | EP1777548A4 (ja) |
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JP2009109417A (ja) * | 2007-10-31 | 2009-05-21 | Toshiba Corp | レーダシステムとレーダ搭載移動体装置 |
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JPWO2019224880A1 (ja) * | 2018-05-21 | 2020-10-01 | 三菱電機株式会社 | レーダ装置 |
Also Published As
Publication number | Publication date |
---|---|
JP4668198B2 (ja) | 2011-04-13 |
EP1777548A4 (en) | 2010-07-21 |
US20090009381A1 (en) | 2009-01-08 |
US7671788B2 (en) | 2010-03-02 |
EP1777548A1 (en) | 2007-04-25 |
JPWO2006013614A1 (ja) | 2008-05-01 |
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