Radar imaging apparatus, imaging method, and program thereof
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G01S-013/42
G01S-013/64
출원번호
US-0478323
(2012-05-23)
등록번호
US-8686894
(2014-04-01)
우선권정보
JP-2010-178959 (2010-08-09)
발명자
/ 주소
Fukuda, Takeshi
Inoue, Kenichi
Sato, Toru
Sakamoto, Takuya
Saho, Kenshi
출원인 / 주소
Panasonic Corporation
대리인 / 주소
Wenderoth, Lind & Ponack, L.L.P.
인용정보
피인용 횟수 :
27인용 특허 :
6
초록▼
A radar imaging apparatus includes: (i) a delay code generation unit which repeats, for M scan periods, scan processing of generating, using a transmission code, N delay codes in a scan period for scanning N range gates having mutually different distances from the radar imaging apparatus; (ii) a sig
A radar imaging apparatus includes: (i) a delay code generation unit which repeats, for M scan periods, scan processing of generating, using a transmission code, N delay codes in a scan period for scanning N range gates having mutually different distances from the radar imaging apparatus; (ii) a signal storage unit which stores, in association with a range gate and a scan period, a baseband signal; (iii) a memory control unit which repeatedly writes, in the signal storage unit, for the M scan periods, N demodulated signals corresponding to a single scan period, and reads out a group of M demodulated signals corresponding to mutually different scan periods; (iv) a Doppler frequency discrimination unit which performs frequency analysis on demodulated signals having the same range gate; and (v) a direction of arrival calculation unit which estimates a direction of a target.
대표청구항▼
1. A radar imaging apparatus, comprising: a transmission unit configured to generate a transmission signal by spreading carrier waves using a transmission spreading code;a transmission antenna which radiates the transmission signal as radiation waves;a plurality of receiving antennas each of which r
1. A radar imaging apparatus, comprising: a transmission unit configured to generate a transmission signal by spreading carrier waves using a transmission spreading code;a transmission antenna which radiates the transmission signal as radiation waves;a plurality of receiving antennas each of which receives reflected waves which are the radiation waves reflected from an object;a delay code generation unit configured to repeat, for M scan periods, scan processing of sequentially generating N delay codes in a scan period for scanning N range gates having mutually different distances from the radar imaging apparatus, the N delay codes being the same as the transmission spreading code and corresponding to the distances, M being an integer equal to or greater than two, and N being an integer equal to or greater than two;a plurality of despreading units corresponding to the respective receiving antennas and each configured to despread, by sequentially using the N delay codes, the reflected waves received by a corresponding one of the receiving antennas;a plurality of demodulators corresponding to said respective despreading units and each configured to perform, using the carrier waves, quadrature demodulation of the reflected waves despread by a corresponding one of said despreading units, and generate demodulated signals Rij corresponding to the reflected waves received by a corresponding one of said receiving antennas, i being an integer from one to N, and j being an integer from one to M;a storage unit configured to store, in association with a delay time in said delay code generation unit and a scan period, the demodulated signals Rij generated by each of said demodulators;a memory control unit configured to (i) repeatedly write, in said storage unit, for the M scan periods, the N demodulated signals R1j to RNj corresponding to the mutually different distances corresponding to the N delay codes in said delay code generation unit and a single scan period, and (ii) sequentially read out, from said storage unit, a group of the M demodulated signals Ri1 to RiM corresponding to same distances and mutually different scan periods;a Doppler frequency detection unit configured to detect, for each of said demodulators, a Doppler frequency component, a phase, and an intensity by performing frequency analysis on the M demodulated signals Ri1 to RiM read out by said memory control unit and corresponding to the same distances, the Doppler frequency component being a frequency component representing a difference between the reflected waves and the carrier waves in each of the range gates, and the phase and the intensity corresponding to the Doppler frequency component; anda direction estimation unit configured to estimate a direction of the object by (i) calculating, from the detected phase corresponding to each of said demodulators, a phase difference between said demodulators and (ii) detecting, from the calculated phase difference, a direction of arrival of the reflected waves in each of the range gates. 2. The radar imaging apparatus according to claim 1, wherein said direction estimation unit is configured to estimate that a direction of arrival of the reflected waves including a Doppler frequency component is the direction of the object, the Doppler frequency component having an intensity equal to or greater than a predetermined first threshold value, and the intensity being detected by said Doppler frequency detection unit. 3. The radar imaging apparatus according to claim 2, further comprising a distance estimation unit configured to estimate that the distance of one of the range gates in which the Doppler frequency component is detected is a distance from said radar imaging apparatus to the object, the Doppler frequency component having an intensity equal to or greater than the first threshold value, and the intensity being detected by said Doppler frequency detection unit. 4. The radar imaging apparatus according to claim 2, wherein said direction estimation unit is further configured to estimate, from the Doppler frequency component, a radial velocity which is a velocity of the object as viewed from said radar imaging apparatus, the Doppler frequency component having the intensity equal to or greater than the first threshold value, and the intensity being detected by said Doppler frequency detection unit. 5. The radar imaging apparatus according to claim 1, wherein each of the N delay codes has a delay time which is mutually different with respect to the transmission spreading code, andthe delay time is an integer multiple of a bit time which is a time for providing one bit of the transmission spreading code. 6. The radar imaging apparatus according to claim 5, wherein said distance estimation unit is configured to:identify a peak intensity from an intensity distribution of the Doppler frequency component corresponding to the delay time for each Doppler frequency component, the peak intensity being a local maximum intensity, and the Doppler frequency component being detected by said Doppler frequency detection unit; andestimate a distance from said radar imaging apparatus to the object by performing interpolation processing with use of the identified peak intensity, a pre-peak intensity, and a post-peak intensity, the distance being estimated with, as a resolution, a distance shorter than a distance corresponding to the bit time, the pre-peak intensity being an intensity corresponding to a delay time shorter by the bit time than the delay time corresponding to the identified peak intensity, and the post-peak intensity being an intensity corresponding to a delay time longer by the bit time than the delay time corresponding to the identified peak intensity. 7. The radar imaging apparatus according to claim 1, wherein, a chip rate CR of the transmission spreading code and the delay code satisfies:CR≦2×f0×vres/vmax where a frequency of the carrier waves is f0, an estimated maximum value of a radial velocity which is a velocity of the object as viewed from said radar imaging apparatus is vmax, and a resolution at which the radial velocity can be detect is vres. 8. The radar imaging apparatus according to claim 1, further comprising a control unit configured to control (i) a first operation mode in which said delay code generation unit repeats the scan processing M times and (ii) a second operation mode in which said delay code generation unit repeatedly generates the same delay code,wherein said control unit is configured to determine, in the first operation mode, whether or not there is a Doppler frequency component having an intensity equal to or greater than a predetermined second threshold value, and switch to the second operation mode when it is determined that there is the Doppler frequency component having the intensity equal to or greater than the predetermined second threshold value, the intensity being detected by said Doppler frequency detection unit, andsaid delay code generation unit is configured to repeatedly generate, in the second operation mode, the delay code corresponding to a range gate in which the Doppler frequency component equal to or greater than the predetermined second threshold value is detected,said storage unit is configured to avoid storing a demodulated signal which is despread using the delay code corresponding to the range gate, and demodulated, andsaid Doppler frequency detection unit is configured to detect again, by (i) sampling, in a cycle shorter than the scan period, the demodulated signal avoided being stored by said storage unit and (ii) performing frequency analysis on the sampled demodulated signal, a phase and an intensity of the Doppler frequency component in a range gate in which the Doppler frequency component equal to or greater than the predetermined second threshold value is detected. 9. The radar imaging apparatus according to claim 8, wherein, in the second operation mode, an observation time of the demodulated signal necessary for said Doppler frequency detection unit to perform the frequency analysis is equal to a time necessary to repeat the scan period M times. 10. The radar imaging apparatus according to claim 8, wherein the predetermined second threshold value is a value in which the number of the range gates is N−2 or less, each of the range gates being determined to have the intensity equal to or greater than the predetermined second threshold value.
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