Abstract:
A heat sensing system and method for dynamic heat sensing may be implemented in a flight vehicle having a main antenna configured for sending and/or receipt of signals. The system includes an auxiliary antenna system that is arranged within a radome of the flight vehicle for detecting temperatures around the exterior surface of the radome. The auxiliary antenna is configured for receiving and measuring infrared or optical energy. Using the measured energy, the system is configured to determine whether the detected temperature exceeds a predetermined temperature and rotating the vehicle to equalize heat around the vehicle when the current temperature exceeds the predetermined temperature.
Abstract:
A compact, wideband antenna system includes first and second monopole radiating elements positioned near an edge of a common ground plane. The first and second monopole radiating elements may be located on opposite sides of the ground plane. Additional monopole elements may also be provided. In some embodiments, the ground plane includes an opening in a central region thereof to accommodate an optical system. In some embodiments, an additional antenna (e.g., an array antenna) may be provided over the same ground plane in a region between the monopole elements.
Abstract:
An ultra wideband (UWB) feed circuit is provided from an optical substrate disposed over a multi-layer dielectric substrate with each layer being provided from a material having a relatively low relative dielectric constant. Conductor layers are disposed between at least a pair of the dielectric substrates which make up the multi-layer dielectric substrate. The multi-layer dielectric substrate is, in turn, disposed over a suspended air stripline (SAS) signal path comprised of a substrate having a conductor disposed thereover. The optical substrate, multi-layer dielectric substrate and SAS are disposed in a radio frequency (RF) waveguide.
Abstract:
A compact transducer system includes both an antenna subsystem and an optical transducer subsystem. The antenna subsystem may include multiple radio frequency (RF) radiating elements disposed adjacent to a ground plane. The ground plane may also serve as an optical reflector within an optical path of the optical transducer subsystem. A secondary reflector may also be provided within the optical path of the optical transducer subsystem. The secondary reflector may be formed of dielectric material (e.g., meta-material) in some embodiments to prevent undesired coupling with RF circuitry.