Various aspects of the present disclosure generally relate to wireless communication. In some aspects, a wireless communication device may select, for communicating a signal, one or more active elements of a set of antenna elements based at least in part on positions of the one or more active elements of the set of antenna elements relative to a set of steering lenses of the wireless communication device; and communicate the signal based at least in part on emitting or receiving the signal using the one or more active elements, wherein the set of steering lenses of the wireless communication device steer the signal to or from the one or more active elements. Numerous other aspects are provided.

A multi-beam telecommunications antenna system with a focusing device including a two-dimensional radiator array generating a plurality of beams simultaneously by setting amplitude-time parameters of the signals for each radiator. The antenna includes: a focusing system having an amplifying lens; a radiating device, for irradiating the amplifying lens and having a two-dimensional radiator array, is disposed at a distance from the amplifying lens and covers a projection area of beams at this distance; and a beam forming system. At least one sub-array of the radiators provides a beam in a set direction. For each beam, the beam forming system provides, for each radiator in the corresponding sub-array, amplitude-time parameters of the signal being transmitted to form a non-planar wavefront, which is equidistant across the amplifying lens to a planar wavefront of the beam. The radiating surface of the radiator array is outside a region of self-intersection of the non-planar wavefronts.

A radar antenna for a flight vehicle that follows a flight path comprises a radio frequency (RF) reflector, and separated first arrays of first RF feed elements to form, with the reflector, respective first fixed radar beams that are directed at the Earth and positionally offset with respect to each other, such that when the radar antenna follows the flight path, the respective first fixed radar beams trace respective first subswaths on the Earth that are separated from each other by respective subswath gaps.

A semiconductor device comprises a substrate having a first surface and a second surface opposite the first surface, at least one connection element arranged on the first surface of the substrate to electrically and mechanically connect the substrate to a printed circuit board, and a radar semiconductor chip arranged on the first surface of the substrate.

An antenna device provided with a single reflecting mirror having multiple focal points, and multiple primary radiators provided at respective positions of the multiple focal points.

A radio frequency antenna array uses lenses and RF elements, to provide ground-based coverage for cellular communication. The antenna array can include two spherical lenses, where each spherical lens has at least two associated RF elements. Each of the RF elements associated with a given lens produces an output beam with an output area. Each lens is positioned with the other lenses in a staggered arrangement. The antenna includes a control mechanism configured to enable a user to move the RF elements along their respective tracks, and automatically phase compensate the output beams produced by the RF elements based on the relative distance between the RF elements.

Apparatus for Manufacture and In-Space Assembly of Antennas comprising: a prefabricated primary reflector center section; a trusselator truss assembler; a phased feed array; wherein said prefabricated reflector center section, trusselator, and phased feed array are fixedly connected to one another; a self-positioning and orienting tool; a truss extending from said trusselator; a secondary reflector attached to said truss; robotic arms; a nibbler end effector mounted on one of said robotic arms; a grapple end effector mounted on one of said robotic arms; a mold for casting a piece of a primary reflector; a power cube; a solar array providing power to said power cube; refabricator plus; and an ESPA ring.

The disclosure provides a wireless communications systems that uses a polybeam geometry. A polybeam communications network, a polybeam antenna, a method of communicating are disclosed. In one example, the polybeam communications network includes: (1) a first communications structure, (2) first transceivers, and (3) a first polybeam antenna attached to the first communications structure that transmits first communication beams driven by corresponding ones of the first transceivers, having arcs of less than twenty degrees each and defining overlapping territories of coverage.

According to the present disclosure there is provided a multiple-input-multiple-output (MIMO) transmitter for transmitting wireless communication signals over a communication channel to a receiver, the transmitter including a digital signal processor configured to perform pre-coding on a plurality N.sub.s of data streams; a plurality N.sub.RF of radio-frequency (RF) chains each configured to pass a pre-coded data stream from the digital signal processor to generate a signal representing that data stream; a lens antenna array comprising an array of N.sub.T antenna elements; and a selecting unit coupled between the plurality N.sub.RF of RF chains and the lens antenna array, the selecting unit including a plurality of separate coupling units each configured to couple a respective RF chain to a selective sub-array of N.sub.T.sup.B.sup.RF antenna elements concurrently for transmitting the signal representing the data stream passed through that RF chain.

The described features generally relate to adjusting a native antenna pattern of a satellite to adapt communications via the satellite. For example, a communications satellite may include an antenna having a feed array assembly, a reflector, and a linear actuator coupled between the feed array assembly and the reflector. The feed array assembly may have a plurality of feeds for communicating signals associated with a communications service, and the reflector may be configured to reflect the signals transmitted between the feed array assembly and one or more target devices. The linear actuator may have an adjustable length, or otherwise provide an adjustable position between the feed array assembly and the reflector. By adjusting the position of the feed array assembly relative to the reflector, the communications satellite may provide a communications service according to a plurality of native antenna patterns.