Various embodiments relate to an antenna design enabling beam-steering antenna arrays for communication in a high radio frequency spectrum. A device may comprise a first layer of resonance structures; a second layer of resonance structures, wherein the resonance structures of the first layer are configured to be electromagnetically coupled with the resonance structures of the second layer; a feeding element configured to electromagnetically excite the first and the second layer of the electromagnetically coupled resonance structures, wherein the first and the second layers are stacked with the feeding element substantially symmetrically with respect to an axis perpendicular to a plane defined by the feeding element, and wherein distances of geometric centers of the resonance structures of the second layer from the axis differ from distances of geometric centers of the resonance structures of the first layer from the axis. A device and a method of fabricating the device are disclosed.

Methods, apparatus, and systems are provided for controlling a payload of a gimbal stabilisation system for an aircraft during testing an antenna under test (AUT). The gimbal stabilisation system including a payload control assembly coupled via a yaw motor to a gimbal assembly. The gimbal assembling including the payload comprising a first section with a transceiver for use in testing the AUT and a second section rotatably coupled to the gimbal assembly. The payload control assembly including a controller configured to operate the yaw motor and gimbal assembly by: receiving an in-flight position of the aircraft during testing of the AUT; receiving a position of the AUT in relation to the aircraft; and controlling the gimbal assembly by: calculating a pointing direction and alignment of the first section of the payload relative to the AUT based on the received position of the aircraft and the received position of the AUT; and maintaining pointing and alignment of the first section of the payload towards the AUT based on the calculated pointing direction and alignment of the first section of the payload.

Systems, methods, apparatuses, and computer program products for initialization and operation of intelligent reflecting surface. The method may include transmitting a synchronization signal block burst to a reflection surface device. The method may also include receiving a first measurement report of the synchronization signal block burst received at the reflection surface device. The method may further include determining a transmit beam for a subsequent synchronization signal block burst based on a highest strength of signals in the synchronization signal block burst. In addition, the method may include receiving a second measurement report of the subsequent synchronization signal block burst. Further, the method may include determining an arrival angle of the subsequent synchronization signal block burst at the reflection surface device. The method may also include establishing a connection with the reflection surface device based on the transmit beam and the arrival angle.

Multi-RET actuators include a plurality of shafts that have respective axially-drivable members mounted thereon. Each of axially-drivable member is mechanically linked to a respective one of a plurality of phase shifters. The multi-RET actuator further includes a motor having a drive shaft and a gear system that is configured to selectively couple the motor to the respective shafts. The gear system is configured so that rotation of the drive shaft in a first direction creates a mechanical linkage between the motor and a first of the shafts, and rotation of the drive shaft in a second direction that is opposite the first direction rotates the first of the shafts.

An interface matrix arrangement for multi-beam, multi-port antenna is described.

An apparatus including a body and a wireless communication system. The body partially encloses a camera. The wireless communication system is integrated within or coupled to the body of the apparatus. The wireless communication system includes: a sensor, an antenna, a switching unit, a wireless communication circuit, and a controller. The sensor is configured to determine an orientation of the wireless communication system. The antenna is configured to transmit or receive wireless signals and configured to have an antenna gain and polarization. The switching unit is configured to change a configuration of the antenna gain and polarization. The wireless communication circuit is electrically coupled to the antenna to transmit or receive the wireless signals. The sensor determines the orientation of the wireless communication system related to an external wireless communication system and the switching unit changes the configuration of the antenna gain and polarization.

An apparatus including a body and a wireless communication system. The body partially encloses a camera. The wireless communication system is integrated within or coupled to the body of the apparatus. The wireless communication system includes: a sensor, an antenna, a switching unit, a wireless communication circuit, and a controller. The sensor is configured to determine an orientation of the wireless communication system. The antenna is configured to transmit or receive wireless signals and configured to have an antenna gain and polarization. The switching unit is configured to change a configuration of the antenna gain and polarization. The wireless communication circuit is electrically coupled to the antenna to transmit or receive the wireless signals. The sensor determines the orientation of the wireless communication system related to an external wireless communication system and the switching unit changes the configuration of the antenna gain and polarization.

The present disclosure provides a linkage structure including an upper bracket and a lower bracket, wherein said upper bracket includes a first linkage unit, a second linkage unit, a middle piece and two sets of adjusting pieces, one end of said middle piece is connected to said first linkage unit and the other end is connected to said second linkage unit; wherein at least one adjusting piece in each set of adjusting pieces is connected rotatably to said first linkage unit or said second linkage unit. According to the linkage structure of the present disclosure, mechanical tilt can be achieved by driving two sets of adjusting pieces to move in coordination, it can ensure the accuracy of mechanical tilt, realize mechanical tilt at any angle, and the operation process is friendly and safe.

A satellite television antenna system can include a self-pointing satellite antenna and a power inserter coupled to the self-pointing satellite antenna. The power inserter can include an enclosure body and a circuit board disposed inside of the enclosure body. The circuit board includes a microprocessor. The microprocessor can be configured via software code to determine whether a first type of communication protocol is being received from a set top box (STB) coupled to the power inserter, determine a configuration for a first constellation of spacecraft if the first type of communication protocol is being received from the STB, and determine a configuration for a second constellation of spacecraft if the first type of communication protocol is not being received from the STB. The first constellation of spacecraft is different than the second constellation of spacecraft.

The disclosure concerns an antenna subsystem that can be used in various repeater systems to optimize gain of the repeater by increasing isolation between donor and server antennas, wherein at least one of the donor and server antennas is an active multi-mode antenna.