Abstract: A waveguide antenna (200) is disclosed, comprising: a first plurality (220) of slots (222,224), for producing a beam having a first radiation pattern (301) at a first resonant frequency (f1); and a second plurality (230) of slots (232, 234), for producing a beam having a second radiation pattern (302) at a second resonant frequency (f2).

Abstract: A waveguide antenna (200) is disclosed, comprising: a first plurality (220) of slots (222,224), for producing a beam having a first radiation pattern (301) at a first resonant frequency (f1); and a second plurality (230) of slots (232, 234), for producing a beam having a second radiation pattern (302) at a second resonant frequency (f2).

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 waveguide antenna is disclosed, comprising: a first plurality of slots, for producing a beam having a first radiation pattern at a first resonant frequency; and a second plurality of slots, for producing a beam having a second radiation pattern at a second resonant frequency. A method of operation of the waveguide antenna is also disclosed, comprising: operating the transceiver at a first frequency to detect objects in a first field of view; and operating the transceiver at a second frequency to detect objects in a second field of view.

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 system (200, 200a) and a method of operating a radar system are described, the radar system (200, 200a) comprising: a plurality of ICs (210, 220), each IC (210, 220) comprising: a respective LO output (212, 222) for selectively outputting a respective LO signal, and a respective LO input (214, 224); and a coupling device (230, 330), the coupling device (230, 330) comprising: a plurality of inputs (232, 234; 341, 342, 351, 352), each input being coupled to the LO output (212, 222) of a respective IC (200, 200a), and a plurality of outputs (236, 238; 363, 364, 373, 374), each output being coupled to the LO input (212, 222) of a respective IC (214, 224); wherein the coupling device (230, 330) is configured such that a LO signal arriving at any one of said plurality of inputs (232, 234; 341, 342, 351, 352) is distributed to each of said plurality of outputs (236, 238; 363, 364, 373, 374). The coupling device (230, 330) may comprise at least one directional coupler.

Abstract: Embodiments are provided herein for a radar system and a method for determining true velocity, which includes: obtaining a radial velocity component that corresponds to a target object, based on sensor data detected by a radar sensor on a vehicle; obtaining a true velocity magnitude of the target object from a communication protocol; and calculating a true velocity angle of direction of the target object based on a trigonometric relationship established between the radial velocity component and the true velocity vector.

Abstract: A transmission line coupling arrangement comprising: a substrate comprising: a plurality of transmission lines each having a terminal radiating end for providing an electromagnetic wave as a result of a signal provided to the transmission line; and a footprint region extending over a portion of the substrate, wherein each of the terminal radiating ends of each of the plurality of transmission lines extend to a respective point within the footprint region; and the footprint region configured to receive a single transition housing thereover, the transition housing having at least one waveguide for receipt of the electromagnetic wave from one of the terminal radiating ends for coupling the at least one of the plurality of transmission lines to one of an output waveguide and an output antenna.

Abstract: An apparatus configured to provide for detection and ranging of a remote object, the apparatus configured to perform the following: based on a first reflected signal comprising a reflection from the remote object of a first frequency varying detection signal that varies in frequency over a first bandwidth; and based on a second reflected signal comprising a reflection from the remote object of a second frequency varying detection signal that varies in frequency over a different second bandwidth; determine a first estimated range based on a first beat frequency signal comprising the first reflected signal mixed with the first frequency varying detection signal; determine a second estimated range based on a second beat frequency signal comprising the second reflected signal mixed with the second frequency varying detection signal; determine a range of the remote object as a function of the first estimated range and the second estimated range.

Abstract: A method of tuning inductive and/or capacitive components within an integrated circuit device. The method comprises measuring bare-die mounted performance of such a component formed within a semiconductor die, determining a package distribution layer pattern for the at least one component for achieving a desired performance for the at least one component based at least partly on the measured bare-die mounted performance, and packaging the semiconductor die with the determined package distribution layer pattern for the at least one component.

Abstract: A device is disclosed. The device includes a wire board including metallic wiring and a first microchip connected to the metallic wiring. The first microchip includes a first radiating element configured to operate a first frequency. The device further includes a second microchip connect to the metallic wiring. The second microchip includes a second radiating element configured to operate at the first frequency. A main radiating element is also included. The main radiating element is configured to operate at a second radio frequency. The first microchip and the second microchip are physically placed such that the first radiating element faces the second radiating element.

Abstract: A waveguide antenna (200) is disclosed, comprising: a first plurality (220) of slots (222, 224), for producing a beam having a first radiation pattern (301) at a first resonant frequency (f1); and a second plurality (230) of slots (232, 234), for producing a beam having a second radiation pattern (302) at a second resonant frequency (f2).

Abstract: The embodiments described herein provide radar systems for use on unmanned vehicles. The radar systems can be applied to a wide variety of unmanned vehicles, including unmanned aerial vehicles and unmanned land vehicles. In general, the unmanned vehicle comprises a housing having at least one propulsion motor, a radar processing unit coupled to the body, and an antenna. In accordance with the embodiments described herein, the antenna includes an antenna body defining at least one transmitting waveguide and at least one receiving waveguide coupled to the radar processing unit. The antenna body is formed from plastic and includes metalized surface. In one embodiment, the antenna body is formed from 3-dimensional (3D) plastic printing.

Abstract: Embodiments are provided herein for a radar system and a method for determining true velocity, which includes: obtaining a first radial velocity component that corresponds to a target object, based on sensor data detected by a first radar sensor on a vehicle; obtaining a second radial velocity component that corresponds to the target object, based on sensor data detected by a second radar sensor on the vehicle; and calculating a true velocity vector of the target object based on a trigonometric relationship established between the first radial velocity component and the second radial velocity component.

Abstract: A radar system (200, 200a) and a method of operating a radar system are described, the radar system (200, 200a) comprising: a plurality of ICs (210, 220), each IC (210, 220) comprising: a respective LO output (212, 222) for selectively outputting a respective LO signal, and a respective LO input (214, 224); and a coupling device (230, 330), the coupling device (230, 330) comprising: a plurality of inputs (232, 234; 341, 342, 351, 352), each input being coupled to the LO output (212, 222) of a respective IC (200, 200a), and a plurality of outputs (236, 238; 363, 364, 373, 374), each output being coupled to the LO input (212, 222) of a respective IC (214, 224); wherein the coupling device (230, 330) is configured such that a LO signal arriving at any one of said plurality of inputs (232, 234; 341, 342, 351, 352) is distributed to each of said plurality of outputs (236, 238; 363, 364, 373, 374). The coupling device (230, 330) may comprise at least one directional coupler.

Abstract: Embodiments are provided herein for a radar system and a method for determining true velocity, which includes: obtaining a radial velocity component that corresponds to a target object, based on sensor data detected by a radar sensor on a vehicle; obtaining a true velocity magnitude of the target object from a communication protocol; and calculating a true velocity angle of direction of the target object based on a trigonometric relationship established between the radial velocity component and the true velocity vector.

Abstract: A transmission line coupling arrangement comprising: a substrate comprising: a plurality of transmission lines each having a terminal radiating end for providing an electromagnetic wave as a result of a signal provided to the transmission line; and a footprint region extending over a portion of the substrate, wherein each of the terminal radiating ends of each of the plurality of transmission lines extend to a respective point within the footprint region; and the footprint region configured to receive a single transition housing thereover, the transition housing having at least one waveguide for receipt of the electromagnetic wave from one of the terminal radiating ends for coupling the at least one of the plurality of transmission lines to one of an output waveguide and an output antenna.

Abstract: A radio frequency transmission structure couples a RF signal between a first and a second radiating elements arranged at a first and a second sides of a first dielectric substrate, respectively. The RF coupling structure comprises first and second coupling structures. Each coupling structure has a hole arranged through the first dielectric substrate, a first electrically conductive layer arranged on a first wall of the hole to electrically connect a first and a second signal terminals, a second electrically conductive layer arranged on a second wall of the hole opposite to the first wall to electrically connect a first and a second reference terminals. The first electrically conductive layer is separated from the second electrically conductive layer. The first and second coupling structures are symmetrically arranged with the first electrically conductive layers closer to each other than the second electrically conductive layers are to each other.

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 device is disclosed. The device includes a wire board including metallic wiring and a first microchip connected to the metallic wiring. The first microchip includes a first radiating element configured to operate a first frequency. The device further includes a second microchip connect to the metallic wiring. The second microchip includes a second radiating element configured to operate at the first frequency. A main radiating element is also included. The main radiating element is configured to operate at a second radio frequency. The first microchip and the second microchip are physically placed such that the first radiating element faces the second radiating element.