Abstract: The disclosure relates to a doppler division multiplexing (DDM) multiple input multiple output (MIMO) radar system. Example embodiments include a DDM MIMO radar system (400) comprising: a transmitter (401) connected to a plurality of transmitter antennas (4021-N) via a corresponding plurality of signal paths (4031-N) of different electrical lengths (L1-N) such that a phase of a signal transmitted by the transmitter (401) is different at each of the plurality of transmitter antennas (4021-N).

Abstract: The disclosure relates to a radar system comprising multiple synchronized transceivers.

Abstract: The disclosure relates to patch antennas for radar or communications applications. Example embodiments include an antenna comprising: a substrate; a ground plane on a first face of the substrate; and a patch antenna on an opposing second face of the substrate, the patch antenna having a lead extending along a central axis and connected to a rectangular radiating element, wherein the rectangular radiating element comprises two slots on opposing sides of the central axis such that the patch antenna has two resonant frequencies within an operating frequency range of the antenna.

Abstract: The disclosure relates to a doppler division multiplexing MIMO radar system. Example embodiments include a doppler division multiplexing, DDM, multiple input multiple output, MIMO, radar system (400) comprising: a transmitter (401) connected to a plurality of transmitter antennas (4021?N) via a corresponding plurality of signal paths (4031?N) of different electrical lengths (L1?N) such that a phase of a signal transmitted by the transmitter (401) is different at each of the plurality of transmitter antennas (4021?N).

Abstract: The disclosure relates to a radar system comprising multiple synchronized transceivers.

Abstract: A method (400) of detecting an object using a radar system is disclosed. The method comprises transmitting (401) a first radar beam having a first frequency and first radiation pattern (301) from an antenna (500), the first radiation pattern comprising a peak at zero azimuth angle, and detecting (402) a first signal from the object due to a reflection of the first radar beam. A second radar beam having a second frequency and second radiation pattern (302) is transmitted (403) from the antenna (500), the second radiation pattern comprising a peak at a non-zero azimuth angle. A second signal due to a reflection of the second radar beam from the object is detected (404), and the first signal and the second signal compared (405) to determine an angular location of the object relative to the zero azimuth angle.

Abstract: A radar module (100; 200) comprises a low temperature co-fired ceramic, LTCC, substrate (101; 201), with a radar chip (102; 202) attached to a first surface (101a; 201a) of the LTCC substrate (101; 201) and a transmitting antenna (105, 106) for transmitting the radar signal attached to a second surface (101b; 201b) of the LTCC substrate (101; 201). The radar chip (102; 202) is configured to generate a radar signal for transmission. The transmitting antenna (105, 106) is configured to communicate with the radar chip (102; 202) through the LTCC substrate (101; 201). The radar module (100; 200) further comprises a beam steering element (205) configured to introduce a phase delay to the radar signal in order to adjust a first component of a direction of transmission of the radar signal.

Abstract: A wireless communication unit (100) is described that comprises: at least one receiver configured to receive a radio frequency signal on at least one receiver channel (262, 264, 266, 268) and comprising a plurality of receiver circuits; at least one interference detection circuit (244, 248, 252) coupled to an output of at least one of the plurality of receiver circuits and configured to detect a saturation event of a signal output from the at least one of the plurality of receiver circuits; and a controller (114) configured to identify interference in a received signal.

Abstract: A system for register error detection is described, the system comprising: a plurality of addressable registers comprising sets of registers, the registers in each set having contiguous addresses; a cyclic redundancy check generator coupled to the addressable registers and configured to determine a cyclic-redundancy-check result for each set of registers from the values of each of the respective set of registers; a controller coupled to the registers and the cyclic-redundancy-check generator.

Abstract: A radar module (100; 200) comprises a low temperature co-fired ceramic, LTCC, substrate (101; 201), with a radar chip (102; 202) attached to a first surface (101a; 201a) of the LTCC substrate (101; 201) and a transmitting antenna (105, 106) for transmitting the radar signal attached to a second surface (101b; 201b) of the LTCC substrate (101; 201). The radar chip (102; 202) is configured to generate a radar signal for transmission. The transmitting antenna (105, 106) is configured to communicate with the radar chip (102; 202) through the LTCC substrate (101; 201). The radar module (100; 200) further comprises a beam steering element (205) configured to introduce a phase delay to the radar signal in order to adjust a first component of a direction of transmission of the radar signal.

Abstract: A method (400) of detecting an object using a radar system is disclosed. The method comprises transmitting (401) a first radar beam having a first frequency and first radiation pattern (301) from an antenna (500), the first radiation pattern comprising a peak at zero azimuth angle, and detecting (402) a first signal from the object due to a reflection of the first radar beam. A second radar beam having a second frequency and second radiation pattern (302) is transmitted (403) from the antenna (500), the second radiation pattern comprising a peak at a non-zero azimuth angle. A second signal due to a reflection of the second radar beam from the object is detected (404), and the first signal and the second signal compared (405) to determine an angular location of the object relative to the zero azimuth angle.

Abstract: A wireless communication unit (100) is described that comprises: at least one receiver configured to receive a radio frequency signal on at least one receiver channel (262, 264, 266, 268) and comprising a plurality of receiver circuits; at least one interference detection circuit (244, 248, 252) coupled to an output of at least one of the plurality of receiver circuits and configured to detect a saturation event of a signal output from the at least one of the plurality of receiver circuits; and a controller (114) configured to identify interference in a received signal.

Abstract: The disclosure relates to patch antennas for radar or communications applications. Example embodiments include an antenna comprising: a substrate; a ground plane on a first face of the substrate; and a patch antenna on an opposing second face of the substrate, the patch antenna having a lead extending along a central axis and connected to a rectangular radiating element, wherein the rectangular radiating element comprises two slots on opposing sides of the central axis such that the patch antenna has two resonant frequencies within an operating frequency range of the antenna.

Abstract: A system for register error detection is described, the system comprising: a plurality of addressable registers comprising sets of registers, the registers in each set having contiguous addresses; a cyclic redundancy check generator coupled to the addressable registers and configured to determine a cyclic-redundancy-check result for each set of registers from the values of each of the respective set of registers; a controller coupled to the registers and the cyclic-redundancy-check generator.