Method, antenna array, radar system and vehicle
US-9910150-B2 · Mar 6, 2018 · US
US10145936B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10145936-B2 |
| Application number | US-201615066679-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 10, 2016 |
| Priority date | Mar 25, 2015 |
| Publication date | Dec 4, 2018 |
| Grant date | Dec 4, 2018 |
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Nt transmitting antennas include Nt1 (Nt>Nt1) transmitting antennas arranged on a first straight line at a first spacing, and (Nt+1−Nt1) transmitting antennas arranged on a second straight line at a second spacing in a direction orthogonal to the Nt1 transmitting antennas, where Nt1 is a value that maximizes Nt1×(Nt+1−Nt1). Na receiving antennas include Na1 (Na>Na1) receiving antennas arranged on the first straight line at a third spacing, and (Na+1−Na1) receiving antennas arranged on the second straight line at a fourth spacing in a direction orthogonal to the Na1 receiving antennas, where Na1 is a value that maximizes Na1×(Na+1−Na1).
Opening claim text (preview).
What is claimed is: 1. A radar device comprising: radar transmission circuitry which, in operation, transmits Nt radar signals through Nt transmitting antennas at each predetermined transmission period, wherein Nt is an integer that is three or greater than three; and radar reception circuitry which, in operation, receives, through Na receiving antennas, and performs Doppler frequency analysis processing on at least one reflected wave signal which is of the Nt radar signals transmitted and reflected by an object, wherein Na is an integer that is three or greater than three, wherein: the Nt transmitting antennas include: Nt1 transmitting antennas arranged on a first straight line with a first spacing therebetween, and (Nt+1−Nt1) transmitting antennas arranged on a second straight line with a second spacing therebetween, the second straight line being orthogonal to the first straight line, wherein Nt1 is an integer that satisfies Nt>Nt1; at least one transmitting antenna of the Nt transmitting antennas is arranged simultaneously on the first straight line and on the second straight line; the integer Nt1 maximizes Nt1×(Nt+1−Nt1); the Na receiving antennas include: Na1 receiving antennas arranged on the first straight line with a third spacing therebetween, wherein Na1 is an integer that satisfies Na>Na1, and (Na+1−Na1) receiving antennas arranged on the second straight line with a fourth spacing therebetween; at least one receiving antenna of the Na receiving antennas is arranged simultaneously on the first straight line and on the second straight line; and the integer Na1 maximizes Na1×(Na+1−Na1). 2. The radar device according to claim 1 , wherein the third spacing is larger than the fourth spacing when (Nt1×Na1)<(Nt+1−Nt1)×(Na+1−Na1) is satisfied, and the third spacing is smaller than the fourth spacing when (Nt1×Na1)>(Nt+1−Nt1)×(Na+1−Na1) is satisfied. 3. The radar device according to claim 1 , wherein the third spacing and the fourth spacing are shorter than a wavelength of the radar signal. 4. The radar device according to claim 1 , wherein the radar reception circuitry includes: first direction component extraction circuitry which, in operation, extracts components of Nt1×Na1 virtual antenna elements arranged on the first straight line in a virtual receiving array of Nt×Na virtual antenna elements from an output of the Doppler frequency analysis processing; second direction component extraction circuitry which, in operation, extracts components of (Nt+1−Nt1)×(Na+1−Na1) virtual antenna elements arranged on the second straight line in the virtual receiving array of the Nt×Na virtual antenna elements from the output of the Doppler frequency analysis processing; azimuth estimation circuitry which, in operation, estimates a predetermined number of arrival direction candidates in an azimuth direction based on the components of the Nt1×Na1 virtual antenna elements; elevation estimation circuitry which, in operation, estimates a predetermined number of arrival direction candidates in an elevation direction based on the components of the (Nt+1−Nt1)×(Na+1−Na1) virtual antenna elements; and integration processing circuitry which, in operation, calculates a likelihood value for each combination of pairs of the arrival direction candidates in the azimuth direction and the arrival direction candidates in the elevation direction and outputs an arrival direction estimation value of the reflected wave signal in the azimuth direction and the elevation direction based on the likelihood value.
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