Radar system

Patent metadata

Field	Value
Publication number	US-11782148-B2
Application number	US-201916363719-A
Country	US
Kind code	B2
Filing date	Mar 25, 2019
Priority date	Mar 25, 2019
Publication date	Oct 10, 2023
Grant date	Oct 10, 2023

Abstract

Aspects of the present disclosure provide for a radar system including a radar IC including a timing engine, a local oscillator, and a modulator. The timing engine is configured to generate one or more chirp control signals. The local oscillator is configured to receive the one or more chirp control signals and generate a frame including a first sequence of chirps according to the one or more chirp control signals. The modulator is configured to modulate the first sequence of chirps to generate a second sequence of chirps so the frame includes the first sequence of chirps and the second sequence of chirps offset by a first frequency value.

First claim

What is claimed is:

1. A radar system, comprising:
a radar transceiver integrated circuit (IC), comprising:
a local oscillator configured to generate a frame including a first sequence of chirps; and
a modulator coupled to the local oscillator, the modulator configured to modulate the first sequence of chirps to generate a second sequence of chirps such that the frame includes the first sequence of chirps and the second sequence of chirps offset by a first frequency value; and a processing element configured to:
compute a first velocity estimate for an object within a field of view of the radar system based on a range-Doppler array;
compute a second velocity estimate for the object based on a difference between a phase of at least one peak in a first range-Doppler array for the first sequence of chirps and a phase of at least one peak in a second range-Doppler array for the second sequence of chirps; and
compute a final velocity estimate for the object based on the first velocity estimate and the second velocity estimate.

2. The radar system of claim 1 , further comprising a timing engine configured to generate one or more chirp control signals,
wherein the local oscillator is configured to generate the frame according to the one or more chirp control signals, and
wherein the radar transceiver IC further comprises a control module coupled to the timing engine and to the modulator, and wherein the control module is configured to:
transmit one or more parameter values to the timing engine to at least partially control generation of the chirp control signals; and
transmit one or more signals to the modulator to at least partially control the modulation of the first sequence of chirps.

3. The radar system of claim 1 , wherein the radar transceiver IC is configured to:
receive a frame of reflected chirps, the reflected chirps comprising the first sequence of chirps and the second sequence of chirps reflected by the object;
generate a digital intermediate frequency (IF) signal corresponding to the frame of reflected chirps; and
demodulate the digital IF signal to obtain a first demodulated digital IF signal corresponding to the first sequence of chirps and a second demodulated digital IF signal corresponding to the second sequence of chirps, wherein before demodulation the first sequence of chirps is offset in the digital IF signal from the second sequence of chirps by the first frequency value.

4. The radar system of claim 3 , wherein the range-Doppler array on which computation of the first velocity estimate is based is one of the first range-Doppler array, the second range-Doppler array, and a relationship between the first and second range-Doppler array, and wherein the processing element is configured to:
perform a range fast Fourier transform (FFT) on the first demodulated digital IF signal and on the second demodulated digital IF signal to generate a first range array for the first demodulated digital IF signal and a second range array for the second demodulated digital IF signal; and
perform Doppler FFTs on the first range array and on the second range array to generate the first range-Doppler array corresponding to the first range array and the second range-Doppler array corresponding to the second range array.

5. The radar system of claim 4 , wherein to compute the second velocity estimate, the processing element is configured to subtract a phase of a first peak of the first range-Doppler array from a phase of a second peak of the second range-Doppler array.

6. The radar system of claim 1 ,
wherein the frame while containing the first sequence of chirps is associated with a first maximum measurable velocity, and
wherein the frame while containing the first sequence of chirps and the second sequence of chirps is associated with a second maximum measurable velocity greater than the first maximum measurable velocity.

7. The radar system of claim 1 ,
wherein the radar system is configured to operate in a calibration mode to determine a systematic phase offset between receive channels of the radar transceiver IC, and
wherein the processing element is configured to determine the final velocity estimate of the object based on the systematic phase offset.

8. The radar system of claim 1 , wherein the first sequence of chirps and the second sequence of chirps are described by 1+e j2πΔft , wherein Δf the first frequency value, and wherein t is representative of time.

9. The radar system of claim 1 , wherein the first sequence of chirps and the second sequence of chirps are transmitted using a same antenna of the radar system.

10. The radar system of claim 1 , further comprising an antenna, wherein the radar transceiver IC is configured to cause the antenna to:
transmit the first sequence of chirps; and
transmit the second sequence of chirps at a same time as the antenna transmits the first sequence of chirps.

11. A method for determining an approximate velocity in a radar system, the method comprising:
initiating transmission, via a transmission channel, of a frame of chirps having a first sequence of chirps and a second sequence of chirps offset from the first sequence of chirps by a frequency (Δf), wherein initiating transmission of the frame of chirps having the first sequence of chirps and the second sequence of chirps offset from the first sequence of chirps by Δf comprises:
generating one or more chirp control signals according to chirp parameter values;
generating a frame including the first sequence of chirps according to the one or more chirp control signals, the frame including the first sequence of chirps and being associated with a first maximum measurable velocity; and
modulating the first sequence of chirps to generate a second sequence of chirps such that the frame contains the first sequence of chirps and the second sequence of chirps offset by the Δf, the frame including the first sequence of chirps and the second sequence of chirps and being associated with a second maximum measurable velocity greater than the first maximum measurable velocity;

receiving, via a receive channel, a frame of reflected chirps, the reflected chirps comprising the first sequence of chirps and the second sequence of chirps reflected by an object within a field of view of the radar system;
generating, via the receive channel, a digital intermediate frequency (IF) signal corresponding to the frame of reflected chirps; demodulating, via a processor, the digital IF signal to form a first demodulated IF signal corresponding to the first sequence of chirps and a second demodulated IF signal corresponding to the second sequence of chirps; and
determining, via the processor, the approximate velocity at least partially according to the first demodulated IF signal and the second demodulated IF signal.

12. The method of claim 11 , wherein determining the approximate velocity for an object in a field of view of the radar system at least partially according to the first demodulated IF signal and the second demodulated IF signal comprises:
performing a range fast Fourier transform (FFT) on the first demodulated IF signal and the second demodulated IF signal to generate a first range array corresponding to the first demodulated IF signal and a second range array corresponding to the second demodulated IF signal; and
performing Doppler FFTs on the first range array and the second range array to generate a first range-Doppler array and a second range-Doppler array.

13. The method of claim 12 , further comprising determining the approximate velocity of the object within the field of view of the radar system using at least one of the first range-Dopp

Assignees

• Texas Instruments Inc

Inventors

• Subburaj Karthik
• Rao Sandeep
• Murali Sriram
• Ramasubramanian Karthik

Classifications

• G01S13/584 Primary

  adapted for simultaneous range and velocity measurements · CPC title

• G01S7/352

  Receivers · CPC title

• G01S7/356

  involving particularities of FFT processing · CPC title

• G01S13/343

  using sawtooth modulation · CPC title

• G01S13/345

  using triangular modulation · CPC title