Abstract: A semiconductor package device includes: (1) a die having an active surface, a back surface opposite to the active surface and a lateral surface extending between the active surface and the back surface; (2) a first conductive pillar disposed on the active surface of the die and electrically connected to the die, the first conductive pillar having a top surface facing away from the die and a lateral surface substantially perpendicular to the top surface of the first conductive pillar; (3) a dielectric layer disposed on the active surface of the die and fully covering the lateral surface of the first conductive pillar; and (4) a package body encapsulating the back surface and the lateral surface of the die.

Abstract: An apparatus includes a communications interface configured to receive, at a first aircraft, data related to a radiofrequency (RF) survey of a particular location. The RF survey is based on RF samples from at least a second aircraft. The apparatus further includes a radio, an onboard network system (ONS) configured to determine that the first aircraft is approaching the particular location, and a radio controller coupled to the radio. The radio controller is configured to automatically adjust, based on the RF survey and responsive to determining that the first aircraft is approaching the particular location, a parameter of the radio.

Abstract: An apparatus includes a cross-link phased array and a communication-link phased array. The cross-link phased array and the communication-link phased array are integrated into a single array. The cross-link phased array and communication-link phased array comprise a multi-beam phased array. The cross-link phased array provides communication between multiple space vehicles and the communication-link phased array provides communication between the satellite and the ground GPS system.

Abstract: A vehicle environment detection system (2) that includes at least one radar sensor arrangement (3) and at least one processing unit (4), where the radar sensor arrangement (3) is arranged to detect at least two radar detections (9, 10, 11) during at least two radar cycles. For each radar cycle, the processing unit (4) generates a detection list ({Dit}t=t0, . . . ,t0?N) including range (ri), azimuth angle (?i) and Doppler velocity (vi) for each of the radar detections (9, 10, 11). The processing unit (4) is further arranged to aggregate and store detection lists ({Dit}t=t0, . . . ,t0?N) from the radar cycles in a detection memory (12), and then to group the radar detections (9, 10, 11) in the detection lists ({Dit}t=t0, . . . ,t0?N) into consistently moving motion subsets (40, 41, 42) in a segmentation procedure. Each motion subset (40, 41, 42) corresponds to a certain target object (6, 7, 8).

Abstract: An RF receiver may include antenna elements to receive RF signals, and electro-optic modulators to generate corresponding upconverted optical signals by mixing an RF signal with an optical carrier beam. The RF receiver may include a transmission array having a first bundle of optical waveguides that receive and transmit upconverted optical signals from their ends. The ends may be arranged in a first pattern. The RF receiver may include an interference space to receive the upconverted optical signals to form a composite beam, and an array of single mode optical fibers that have lenses positioned in a detection plane to receive a portion of the composite beam. The first pattern of the ends generates an RF emitter interference pattern at the detection plane, and the single mode optical fiber lenses have a geometric arrangement that corresponds to the first RF emitter interference pattern.

Abstract: A method for determining a model of an electron distribution in the Earth's atmosphere in order to correct time-of-flight measurements of signals that are transmitted by earth satellites for position determinations with signal receivers includes determining local electron density data of provision sites and determining a local resolution accuracy as a function of the electron density data of the provision sites. The method further includes determining functions for interpolation of a distribution of the determined electron density data of the provision sites as a function of the determined resolution accuracy and compiling the model of the electron density distribution with the determined electron density data of the provision sites and the determined functions for interpolation.

Abstract: Implementations described and claimed herein provide systems and methods for obstacle detection. In one implementation, a beam is transmitted at an elevation orientation from a transmit array system. The transmit array system includes transmit antenna arrays each having one or more transmit antennas. Target scatter is received at a receive array system including one or more receive channels. A virtual array is synthesized for the elevation orientation from an incidence of the target scatter on each of the one or more receive channels for each of the one or more transmit antennas. The virtual array has a size corresponding to the one or more transmit antenna arrays convolved with the receive array system. Four dimensional space information is generated from the virtual array, and any obstacles along a travel path are detected from the four dimensional space information.

Abstract: A method for setting up a reference coordinate system including: providing an object with sensors having a geometrical cavity with a pick up terminal configured to provide an output that varies with orientation of the sensors with respect to a direction of an incoming polarized RF plane of polarization; using polarized RF reference sources each having two polarization planes offset from each other and different from polarization fields of other references sources; amplitude modulating the two polarization planes for each of the reference sources to define a time varying linear polarization vector for each of the reference sources; and determining, for each of the reference sources, the position and orientation of the object relative to the reference coordinate system based on a measured amplitude of the time varying linear polarization vector at the sensors, a predetermined mapping function and a predetermined scanning pattern of the time varying linear polarization vector.

Abstract: Iterative methods for direction of arrival estimation of a signal at a receiver with a plurality of spatially separated sensor elements are described. A quantized estimate of the angle of arrival is obtained from a compressive sensing solution of a set of equations. The estimate is refined in a subsequent iteration by a computed error based a quantized estimate of the direction of arrival in relation to quantization points offset from the quantization points for the first quantized estimate of the angle of arrival. The iterations converge on an estimated direction of arrival.

Abstract: A phase rotation amount of each of subcarriers is calculated by calculating a difference between the first phase difference and the second phase difference between consecutive subcarriers included in radio signals, and performing phase addition processing based on the difference. A characteristic coefficient regarding a change rate of the phase rotation amount of each of the subcarriers with respect to a frequency is calculated by performing a linear regression analysis of the relationship between a frequency and the phase rotation amount, and a distance is estimated based on the characteristic coefficient.

Abstract: An angle-of-arrival identification device receives a reception signal including a plurality of subcarriers, using a plurality of antenna elements, and identifies an angle of arrival of the reception signal. The angle-of-arrival identification device includes signal processing units that extract predefined specific subcarriers (pilot carriers) from the reception signals received by each of the plurality of antenna elements, and an angle identification unit that identifies the angle of arrival on the basis of a phase difference between the specific subcarriers extracted by each of the signal processing units. The signal processing unit includes a frequency adjustment unit that adjusts a deviation, from a defined value, of a frequency of the reception signal received by the antenna element, and a filter unit that extracts the specific subcarrier by performing bandpass filter processing on the reception signal whose frequency has been adjusted.

Abstract: In an embodiment, a downlight includes: a plurality of light emitting diodes (LEDs) disposed in a housing of the downlight, and a millimeter-wave radar. The millimeter-wave radar includes: an antenna disposed in the housing, a controller configured to: detect a presence of a human in a field-of-view of the millimeter-wave radar, determine a direction of movement of the detected human, and produce log data based on the direction of movement of the detected human, and a wireless module configured to transmit the log data to a wireless server.

Abstract: A phased array system includes an antenna system includes multiple antennas configured to transmit or receive signals and a power supply circuit configured to generate a supply power and provide the supply power to a plurality of distributed power supply circuits. The phased array system includes distributed power supply circuits, each of the plurality of distributed power supply circuits configured to receive the supply power from the power supply circuit and generate radio frequency supply powers for one multiple radio frequency circuits. The phased array system includes radio frequency circuits, each of the radio frequency circuits configured to cause one of the antennas to transmit or receive the signals based on the plurality of radio frequency supply powers.

Abstract: A semiconductor device includes a base substrate, a first transistor disposed on the base substrate, the first transistor including a first input electrode, a first output electrode, a first control electrode, and a first semiconductor pattern including a crystalline semiconductor, a second transistor disposed on the base substrate, the second transistor including a second input electrode, a second output electrode, a second control electrode, and a second semiconductor pattern including an oxide semiconductor, a plurality of insulating layers disposed on the base substrate, and an upper electrode disposed on the first control electrode with at least one insulating layer of the plurality of insulating layers interposed between the upper electrode and the first control electrode. The upper electrode overlaps the first control electrode and forms a capacitor with the first control electrode.

Abstract: Systems and method for determining an angle of arrival of a radio frequency (RF) signal are disclosed. A radio frequency receiving system as disclosed herein can include a plurality of antenna or receiving elements formed on a common plane. A spacing between the receiving elements can be arbitrary. In response to receiving a radio frequency signal, a difference in an integer number of wavelengths that have passed and a difference in a phase of the received signal is determined between each of a plurality of pairs of antenna elements. More particularly, a residual error is calculated for each possible difference in the number of integer wavelengths that can occur as the received signal travels to the elements in each pair of elements. A solution with a minimum residual value is taken as the difference in the actual integer number of wavelengths that have been traversed by the received signal. That integer value and the detected phase difference is applied to determine the angle of arrival.

Abstract: Methods and apparatuses for reducing roughness using integrated atomic layer deposition (ALD) and etch processes are described herein. In some implementations, after a mask is provided on a substrate, methods include depositing a conformal layer on the mask by ALD to reduce roughness and etching a layer underlying the mask to form patterned features having a reduced roughness. In some implementations, after a substrate is etched to a first depth to form features at the first depth in the substrate, methods include depositing a conformal layer by ALD on sidewalls of the features to protect sidewalls and reduce roughness during a subsequent etch process. The ALD and etch processes may be performed in a plasma chamber.

Abstract: A radar module includes a printed circuit board (PCB) and a semiconductor package mounted on the PCB. The semiconductor package comprises an integrated circuit die and a substrate for electrically connecting the integrated circuit die to the PCB. The substrate comprises an antenna layer integrated into the semiconductor package and electrically connected to the integrated circuit die for at least one of transmitting and receiving radar signals. A discrete pattern-shaping device is mounted on the PCB and is configured to shape a radiation pattern of the radar signals.

Abstract: Radar radiation redirecting tapes (1, 2) include a first plurality of individual radar-reflecting directional antennae (5, 11). Each directional antenna comprises at least three elongate, unevenly spaced antenna conductors (10, 20, 30), arranged with their long extensions parallel to each other in the plane of the tape, such that the directional antenna is operable to reflect incoming radar radiation predominantly in a direction (80) which is orthogonal to the long extension of the antenna conductors and parallel to the plane of the tape.

Abstract: An interface device that enables a GNSS-based precision approach through the Ground Base Augmentation System (GBAS) function known as the GNSS Landing System (GLS) and/or through Satellite Based Augmentation Systems (SBAS) based Localizer Performance with Vertical Guidance (LPV). The GLS interface device allows a GLS-capable multi-mode receiver to be used on a non-GLS-capable airplane without extensive changes to other airplane systems. The GLS interface device works by intercepting information to and from the multi-mode receiver and modifying the information to make the interface compatible with an airplane that uses ILS guidance. Similarly, the information modifications will make the airplane appear to the multi-mode receiver as if it were a GLS-capable airplane.

Abstract: Described embodiments provide systems and methods for detecting and tracking a possible threat object using a multi-static frequency diverse waveform. An example method includes receiving an indication of a possible threat object and provisioning a multi-static cluster of sensors. A set of pulses are transmitted toward the object such that each pulse is transmitted on a unique frequency and at different time slots. A set of reflected pulses are processed to detect and track the object.