A blade antenna comprising: an upper blade element made of conductive, planar material having a profile that curves upwardly from a centrally-located feed point; and a lower blade element made of conductive, planar material having a profile that curves downwardly from the feed point, wherein the lower blade element is configured to be connected to a ground and has a thickness that is at least three times a thickness of the upper blade element, and wherein the curved profiles of the upper and lower blade elements are disposed with respect to one another so as to form a tapered slot on each side of the feed point.

A precision guided munition (PGM) system is disclosed. The PGM system comprises a body including a nose portion. The nose portion includes an aperture. A window is attached, secured, or adhered to the body at the nose portion. One or more antenna substrates is attached, secured, or adhered to the window. A plurality of radiating elements is attached, secured, or adhered to the one or more antenna substrates. An image sensor configured to capture an image in front of the body. The image sensor is behind the aperture and is configured to focus at an infinity focus in front of the body. The one or more antenna substrates include unpopulated areas configured to let photons pass through the antenna substrates from the window to the image sensor. The photons are parallel or collimated and the captured image does not include features of the antenna substrates.

A radio-frequency (RF) antenna and method for using the same are disclosed. In some embodiments, an antenna includes an array of RF radiating antenna elements, a plurality of RF antenna element driving circuits coupled to the array of RF radiating antenna elements to supply tuning voltages to the RF radiating antenna elements, and one or more metal power planes, each of the one or more metal power planes coupled to supply a common voltage to two or more of the plurality of RF antenna driving circuits.

An antenna system for a moving vehicle, the antenna system comprising: a main antenna to generate a main beam; a measurement antenna to generate a measurement beam; and control circuitry to perform an adjustment process by: rotating the main beam to an initial bearing angle; rotating the measurement beam independently of the main beam to receive signals at positions to either side of the initial bearing angle; comparing at least one metric measured for the signals received by the measurement antenna at the positions to either side of the initial bearing angle to generate a comparison output; and determining, based on the comparison output, a correction to be applied to the initial bearing angle of the main beam.

Modular RF assemblies are described for radio networks. The modular RF assemblies include a number of replaceable elements for simplified maintenance and upgradability. In particular, the modular RF assemblies include a control assembly which includes electronics, an RF antenna assembly that includes one or more RF antennas, and a mounting plate. The RF antenna assembly is removably mounted to the control assembly, and the control assembly is removably mounted to the mounting plate. During a maintenance operation and/or an upgrade operation, the control assembly and/or the RF antenna assembly may be replaced to resolve a defective component, to modify the orientation or type of the one or more RF antennas, to change the type of wireless spectrum used for the radio network, etc.

Modular RF assemblies are described for radio networks. The modular RF assemblies include a number of replaceable elements for simplified maintenance and upgradability. In particular, the modular RF assemblies include a control assembly which includes electronics, an RF antenna assembly that includes one or more RF antennas, and a mounting plate. The RF antenna assembly is removably mounted to the control assembly, and the control assembly is removably mounted to the mounting plate. During a maintenance operation and/or an upgrade operation, the control assembly and/or the RF antenna assembly may be replaced to resolve a defective component, to modify the orientation or type of the one or more RF antennas, to change the type of wireless spectrum used for the radio network, etc.

An example autonomous or remotely piloted aircraft includes a virtual aperture radar system including a plurality of antennas relationally positioned on one or more surfaces of the aircraft such that individual beams from each of the plurality of antennas scan respective volumes around the aircraft and the respective volumes together substantially form an ellipsoidal field of regard around the aircraft, and a computing device having one or more processors configured to execute instructions stored in memory for performing functions of: combining the respective volumes together to form an image representative of the ellipsoidal field of regard around the aircraft, and identifying one or more objects within the image.

An electromagnetic phased array (100) is disclosed comprising a plurality of antenna elements (102), each antenna element (102) comprising at least three constituent antennae (104). A drive circuit (106) generates about an axis of each element (102) a radiation pattern that has a defined minima at or close to a null in at least one direction. The drive circuit (106) effects electronic steering of this minima through a range of angles around the axis of each antenna element (102) of the array (100) by appropriate setting of the vector currents associated with its constituent antennae (104). The axes of each of the antenna elements (102) are aligned in parallel with a central axis of the array (100) and at least a sub-set of the elements (102) lie substantially on a common helical surface. The elements (102) are spaced on this surface such that the array (100) has a substantially constant aperture.

An electromagnetic phased array (100) is disclosed comprising a plurality of antenna elements (102), each antenna element (102) comprising at least three constituent antennae (104). A drive circuit (106) generates about an axis of each element (102) a radiation pattern that has a defined minima at or close to a null in at least one direction. The drive circuit (106) effects electronic steering of this minima through a range of angles around the axis of each antenna element (102) of the array (100) by appropriate setting of the vector currents associated with its constituent antennae (104). The axes of each of the antenna elements (102) are aligned in parallel with a central axis of the array (100) and at least a sub-set of the elements (102) lie substantially on a common helical surface. The elements (102) are spaced on this surface such that the array (100) has a substantially constant aperture.

A vehicle communication system includes a controller configured to be communicatively coupled to one or more antennas. The controller is also configured to adjust a beam during a period of time to be oriented at a plurality of pointing angles, and detect a plurality of sets of signal data for a received signal, where each set of signal data is detected at a different one of the pointing angles. The controller is further configured to identify a particular pointing angle based on the plurality of sets of signal data, reorient another beam from the given pointing angle to the particular pointing angle, and transmit or receive data, via the other beam while the other beam is oriented at the particular pointing angle, between a particular external node and at least one internal node.