A system includes a high energy laser (HEL) configured to transmit a HEL beam aimed at a first location on an airborne target. The system also includes a beacon illuminator laser (BIL) configured to transmit a BIL beam aimed at a second location on the target, wherein the second location is offset from the first location. The system also includes at least one fast steering mirror (FSM) configured to steer the BIL beam to be spatially and angularly offset from the HEL beam. The system also includes at least one Coudé path FSM configured to simultaneously receive both the HEL beam and the BIL beam and steer the HEL beam and the BIL beam to correct for atmospheric jitter of the HEL beam and the BIL beam while maintaining the offset of the BIL beam from the HEL beam.

A system for disabling or destroying an unmanned aerial vehicle (UAV) is provided. The system comprises an anti-UAV system and an anti-UAV computing platform. The anti-UAV system comprises: a plurality of laser devices configured to generate a plurality of laser beams at a plurality of different wavelengths; a coarse wavelength division multiplexing (CWDM) combiner configured to combine the plurality of laser beams from the plurality of laser devices into a combined laser beam; and a tracking device configured to detect a UAV. The anti-UAV computing platform is configured to: detect, using the tracking device, an object within range of the tracking device; and based on detecting the object, direct, using the anti-UAV system, the combined laser beam from the CWDM combiner onto the detected object.

A DE energy weapon and tracking system includes a passive millimeter wave (PmmW) imaging receiver on a common gimbaled telescope to sense natural electromagnetic radiation from a mmW scene. The PmmW imaging receiver operates in a portion of the electromagnetic spectrum distinct from the IR bands associated with thermal blooming or the HEL laser. In the case of a HPM source, the reflected energy is either in a different RF band and/or of diminished amplitude such as to not interfere with operation of the PmmW imaging receiver. Although lower resolution than traditional optical imaging, PmmW imaging provides a viable alternative for target tracking when the DE weapon is actively prosecuting the target and provides additional tracking information when the DE weapon is not engaged.

A system includes a target illumination laser (TIL) configured to illuminate an airborne target with a TIL beam. The system also includes a beacon illuminator (BIL) configured to transmit a spot of illumination to an expected location on the target, wherein the spot of illumination is more focused than the TIL beam. The system also includes a camera configured to receive an image of the spot reflected off the target. The system also includes a controller configured to determine an actual location of the spot on the target based on the received image. The controller is also configured to estimate a spot motion by correlating the actual location of the spot on the target with the expected location on the target. The controller is also configured to predict uplink jitter of a high energy laser (HEL) beam generated by a HEL based on the BIL spot motion, the uplink jitter caused by atmospheric optical turbulence.

A device (800) for protecting an aircraft against missiles, includes a Short-Wave InfraRed based (SWIR-based) Missile Tracking Unit, having a SWIR-based optical imager that associated with an optical SWIR band filter. The device (800) further includes a SWIR signals processor; it analyzes the captured SWIR optical signals; and it performs a SWIR-based missile acquisition process, which is also based on raw angular position data of a missile as received from a Missile Approach Warning System (MAWS); and it performs a SWIR-based missile tracking process, which continuously and dynamically determines a precise angular position of the missile based on the captured SWIR optical signals. The device (800) includes a laser-based missile-jamming unit, having an internal laser emitter; and optionally also being operably associated with an external high-power laser emitter; to disrupt the missile, or to disrupt a guiding station of the missile.

The present disclosure concerns a method and plasma burst application system for applying a plasma burst to a target object at a target location, the system comprising a terawatt femtosecond pulsed laser for emitting femtosecond laser pulses; a distance obtaining unit configured to obtain a target distance to the target location; and one or more controllers configured to receive the obtained target distance; set one or more laser control parameters of the terawatt femtosecond pulsed laser according to the obtained target distance such that, when a laser pulse is emitted by the terawatt femtosecond pulsed laser, the laser pulse collapses at a selected laser pulse propagation distance substantially equal to the obtained target distance, and control the emission of at least one laser pulse towards the target location such that the laser pulse collapses at substantially the target location in order to apply the plasma burst at the target location.

A power switch component configured to power a laser apparatus. A data storage component configured to store laser apparatus information and a settings and display circuit in communication with data storage. A display configured to read a current setting and configured to display this setting. A trigger component allowing an activation of the laser apparatus so as to energize the laser apparatus to create a laser beam. A firing circuit configured to receive an electrical activation signal from a trigger and generate a firing signal. A power transfer circuit configured to receive the firing signal. The power transfer circuit component transfers power to a laser beam generation component. A power source configured to provide power to the laser beam generation component for generating a laser beam. Output optics are configured to receive the generated laser beam.

Apparatus for a Directed-Energy Weapon An apparatus for a directed-energy weapon comprises: an assessment system arranged to, during an assessment phase, perform an assessment of a target environment, wherein the target environment comprises a target, and the assessment comprises determining a possible engagement efficiency of the target by the directed-energy weapon; and a controller arranged to, during an engaging phase, control the directed-energy weapon to direct energy towards the target environment conditionally upon the possible engagement efficiency.

A system includes a high energy laser (HEL) configured to transmit a HEL beam and a beacon illumination laser (BIL) configured to transmit a BIL beam. The system also includes at least one fast steering mirror (FSM) configured to steer the BIL beam to be offset from the HEL beam. The system further includes at least one Coudé path FSM configured to correct for atmospheric jitter of the HEL beam and the BIL beam while maintaining the offset of the BIL beam from the HEL beam.

A localized laser-based interceptor for kites balloons and UAVs comprises a laser and a large aperture optical beam delivery system with adjustable focal distance and spot size. The spot-size is adjusted for optimal damage performance on plastic targets, as a function of the distance from the target, its velocity across the laser beam spot and where the extent of the danger zone for personnel and equipment is limited by the fast expansion of the illuminating laser beams. The optical design ensures diverging beam to minimize the hazardous range of the system.