Abstract: An apparatus, and a method performed by the apparatus, are disclosed wherein the apparatus can be mounted on an unmanned vehicle and arranged to act upon a payload. The payload can be mounted on the unmanned vehicle and, under an action of the apparatus, is able to be activated. The method can include receiving an activation instruction from an entity remote from the unmanned vehicle; determining whether or not the received activation instruction is valid by performing a validation process; and in response to determining that the received activation instruction is valid, activating the payload. In response to determining that the received activation instruction is not valid, activation of the payload may be prevented or opposed.

Abstract: An electro-optic system, e.g., mounted to a weapon, measures down range winds and a range-to-target for compensating the ballistic hit point. The system may include an optical light source, collimated to generate a laser spot on the target. The system may include a wind measurement receiver that captures laser light scattered from the target. The captured light may be modulated by atmospheric scintillation eddies, producing optical patterns which change in time and move with the crosswind. These patterns may be analyzed by a processor using covariance techniques to determine path-integrated crosswinds and associated errors. Ranging is done by measuring the time of flight of the laser pulse to the target collecting the scattered signal from the target. Compensated ballistic hit point, measurement errors and other data may be displayed on a micro-display digital eyepiece, overlaid on the real-time image of the target.

Abstract: An apparatus including a body portion, a plurality of missiles attached to the body portion in a manner which allows the plurality of missiles to detach from the body portion, a net having a plurality of locations, wherein each missile is attached to the net at a different location of the plurality of locations, and means for controlling a flight direction and a flight speed of each of the plurality of missiles. The means for controlling the flight direction and the flight speed of each of the plurality of missiles may include a computer processor attached to each of the plurality of missiles. A majority of the net may lie inside of an inner chamber inside of the body portion, and the at least a majority of the net may be configured to come out of the inner chamber in response to a command from a control device.

Abstract: An electronic weapon with an installed deployment unit, from which wire-tethered electrodes are launched, provides a stimulus current through a target to inhibit locomotion by the target. A canister of compressed gas propels the electrodes. The canister is located in the deployment unit in a manner that facilitates the design and manufacture of a relatively narrow deployment unit.

Abstract: A loaded weapon detection system is presented including a mobile device handled by a first user and a weapon handled by a second user, the weapon configured to receive at least one projectile, where either the weapon or the projectile has an electronic beacon associated therewith, the electronic beacon transmitting at least one signal detected by the mobile device when the first user handling the mobile device is within a predefined radius of the electronic beacon associated with the weapon or the projectile. The mobile device issues at least one loaded weapon notification to the first user handling the mobile device while a positional relationship is maintained between the electronic beacon and the mobile device handled by the first user.

Abstract: A counter-flying object system comprising a sensor array including at least one active sensor configured to detect and track the flying object, and a missile launcher configured to launch an interceptor to intercept the flying object, wherein upon launching of the interceptor, the sensor array is configured to determine the location of the interceptor and send said object and interceptor locations to a control system, the control system being configured to provide mission data to the interceptor based on said object and interceptor locations for guiding the interceptor toward the flying object and activating a fragmentation warhead on or in the vicinity of said flying object when a lethality criteria is met.

Abstract: The invention relates to a method for decision support of a combat object (1) in a combat situation comprising the steps of: a) detecting (3) an enemy object (2) such that a plurality of characteristic parameters of the enemy object (2) is determined, b) calculating (4) at least one quality factor for at least one combat sensor of the combat object (1), wherein each quality factor is adapted for indicating identification ability of a combat sensor, and calculating (4) at least one signature factor for at least one enemy sensor of the enemy object (2) based on a predetermined model, wherein each signature factor is adapted for indicating identification ability of an enemy sensor, c) allocating (5) each quality factor calculated in the previous step b) to each combat sensor and allocating (5) each signature factor calculated in the previous step b) to each enemy sensor, and d) controlling (6) each combat sensor against the enemy object (2) based on the result of the previous step c).

Abstract: A method for combining power of separate directed energy beams each associated with a separate firing unit, on a common spot on target. The firing units are coordination and synchronization unit (FUSU) tracks a target and assigns a master firing unit and slave firing units. The master firing unit sends a guide beam to the target, forming a local coordinate system on said target, while the slave firing units track the target and track at least one spot of EM (electromagnetic) radiation on the target. The slave units calculate a direction vector, and fire a power beam at the target, together with the master unit.

Abstract: A military standard-1760 (MIL-STD-1760) interface bridge for storing mission planning data can include a housing, a translator device, a ground support equipment (GSE) connector, and non-volatile memory. The housing can include a MIL-STD-1760 connector on a first end and a weapon side connector on a second end. The translator device can translate a MIL-STD-1553 remote terminal (RT) protocol to a weapon side signaling protocol and translate the weapon side signaling protocol to the MIL-STD-1553 RT protocol. The GSE connector can be coupled to the housing and translator device for downloading mission planning data for a weapon. The non-volatile memory can be configured to store the mission planning data.

Abstract: A weapon system which includes an intermodal shipping container, an unmanned weapons unit, configured to fit substantially within said intermodal shipping container, an energy source capable of providing power to said weapon system, a computing processing unit, wherein computing processing unit is capable of controlling said weapon system, a lifting system, wherein said lifting system is capable of raising said unmanned weapons unit, and a camera system, wherein camera system is capable of capturing images and communicating said images to said computing processing unit.

Abstract: A method for autonomous weapon effects planning includes receiving the desired lethality and collateral effects information on a target and autonomously selecting at least one weapon and fuze setting from an inventory of weapons based on the received lethality and collateral effects information. The method further includes autonomously; determining which weapon with fuze setting and terminal elevation and heading angles satisfies the desired lethality and collateral effects; shaping weapon trajectory to satisfy weapon maneuverability, terrain clobber avoidance and guidance requirements and planning weapon launch conditions for the one or more autonomously selected weapons. The weapon launch conditions include at least a launch point or a launch corridor.

Abstract: A device for the aerial release of mosquitoes includes an unmanned aerial vehicle operable by remote control. It carries a container holding a central processing unit and a mosquito breeding bin, which is a self-contained volume housing mosquitoes and a mosquito food having a toxin suitable to be transmitted by mosquito bite after the mosquito consumes the mosquito food. A release tube is connected to the mosquito breeding bin and sized to release mosquitoes from the mosquito breeding bin. A valve is connected to the release tube and is operable by remote control so that when opened, the mosquitoes have an open pathway out of the container through the release tube.

Abstract: Multiple embodiments of a system are disclosed for defeating enemy missiles and rockets by the use of a non-lethal cloud of pellets that collide with the missile a certain distance away from the target causing premature detonation of the missile, and/or possible severe damage to the missile, and/or deflection of the missile, and/or a deformation to the ogive cones to cause a short in the fuze circuit, and/or deposition of conductive material to cause a short in the fuze circuit.

Abstract: A gun is presented including a frame; a barrel connected to the frame; and a magazine mechanically cooperating with the frame, the magazine having at least one projectile stored therein. The gun further includes an electronic beacon non-removably incorporated within the gun, the electronic beacon configured to emit at least one signal to be received by at least one electronic device located within a pre-established vicinity of the gun. The electronic device provides a notification indicating proximity of the gun. The electronic beacon may be a radio transceiver operating at least one of a plurality of frequencies.

Abstract: An anti-fratricide responsive ordnance system that uses the power of a friendly radio frequency signal to detect and identify a friendly force. Upon identification, an electronic safe and arm device disarms the munition when it enters a kill radius of the friendly force emitting the friendly radio signal.

Abstract: A weapon-locating ladar system estimates a backward trajectory of an airborne target by using flow field measurements to follow the wake turbulence trailing the airborne target from a position at which the target is detected backwards until the wake is no longer observable. The system may use the backward trajectory to estimate the point-of-origin of the target. The system may also use the flow field measurements along the backward trajectory to classify the target. Target classification may be used to refine the point-of-origin estimate, to influence counter-fire or to adapt the flow field measurements.

Abstract: Apparatus and a method for intercepting a rocket body during boost phase. A sensor is arranged to detect thermal emission in a range that is characteristic of a firing rocket body. The image detected by the sensor is applied to an analog-to-digital converter for digitization and application to a computer that includes a routine for separating the modulated photon energy of the detected image from the substantially unmodulated photon energy that characterizes rocket body emissions. The unmodulated photon energy, signature of the rocket body, may be utilized by a fire control system for tracking, targeting and aiming munitions at the firing rocket body.

Abstract: The invention relates to a method for decision support of a combat object (1) in a combat situation comprising the steps of: a) detecting (3) an enemy object (2) such that a plurality of characteristic parameters of the enemy object (2) is determined, b) calculating (4) at least one quality factor for at least one combat sensor of the combat object (1), wherein each quality factor is adapted for indicating identification ability of a combat sensor, and calculating (4) at least one signature factor for at least one enemy sensor of the enemy object (2) based on a predetermined model, wherein each signature factor is adapted for indicating identification ability of an enemy sensor, c) allocating (5) each quality factor calculated in the previous step b) to each combat sensor and allocating (5) each signature factor calculated in the previous step b) to each enemy sensor, and d) controlling (6) each combat sensor against the enemy object (2) based on the result of the previous step c).

Abstract: A directed-energy irradiating apparatus includes an FEL apparatus and an HPM apparatus. The FEL apparatus accelerates free electrons by using a microwave supplied from a microwave source to irradiate an FEL beam and outputs a remaining microwave. The HPM apparatus irradiates an HPM beam generated based on the remaining microwave outputted from the FEL apparatus. It is possible to destroy a target even in a situation that a destruction effect by the FEL beam cannot expected, while maintaining the destruction ability of the FEL beam.

Abstract: The subject munitions deployment platform for an Anti-Personnel Obstacle Breaching System munitions set provides prepositioned compartments to receive the ALICE packs of the munitions set to ensure that they are positioned and aligned for proper deployment. The pre-positioned compartments ensure that when the APOBS is deployed, the front edge of the rear ALICE pack properly engages the rear edge of the front ALICE pack providing a fulcrum aiding rotation of the rear pack allowing it to clear the engaging elements to lift the rear pack off the platform and into the air where it further functions as a drogue to assist in extending the charge line over the chosen target line. Combining the subject platform with a vehicle, or with a towed wagon, allows a Soldier to remain in a safe location while remotely positioning the munitions set to clear a minefield or other anti-personnel obstacle.

Abstract: A tear gas-based enhancement to a fluid bed security system implemented for the purpose of inhibiting unauthorized entry or access and to provide additional time for threatened individuals to evacuate or escape a hostile assembly at the perimeter of a secured area. The system provides for the reliable and controlled application of a specified concentration of tear gas emitted in conjunction with fluidizing gas distributed through a fluid bed configuration comprising a gas distribution piping array and a plurality of fluidizable granular solids in a surrounding relationship to the gas distribution piping array.

Abstract: A method for detecting an object, comprising the steps of defining expected characteristics of scattered electromagnetic radiation to be received at a receiver; attenuating at least a portion of electromagnetic radiation received at the receiver by a presence of an object within a path of electromagnetic information; and detecting the attenuation to indicate a presence of the object. The object may be a low radar profile object, such as a stealth aircraft. The electromagnetic radiation is preferably microwave, but may also be radio frequency or infrared. By using triangulation and other geometric techniques, distance and position of the object may be computed.

Abstract: According to one embodiment, a system for protecting a vehicle from projectiles includes a detection component, a selection component, and an ignition component. In one embodiment, the detection component detects one or more projectiles having a first trajectory that is incident to a first location on the vehicle. In one embodiment, the selection component automatically selects two or more rockets mounted on the vehicle that, when ignited, produce a plurality of exhaust streams configured to deflect the one or more projectiles to a second trajectory. In one embodiment, the second trajectory is not incident to the first location on the vehicle. In one embodiment, the ignition component ignites the selected two or more rockets.

Abstract: There is proposed a system for managing fire of snipers, including a central station (CS) and a plurality of N individual kits (IK), each operated by one sniper. Preferably, the IK includes: --a rifle, --an optical sight (OS) mounted on the rifle with a mechanism for correction of the OS, --equipment including devices activating the rifle's firing pin; --a laser target designator having an axis coinciding with the OS axis, satellite navigation receiver (SNR), video-camera, symbol generator, adding device summarizing output signals, readiness sensor installed on the rifle's trigger, command decoder; zoom-lens actuator; electronic switches controlling the zoom-lens actuator, laser rangefinder; commutator receiving output signals from the laser rangefinder and SNR, and radio-modem module (IK-RM) provided with a two-way communication with the CS furnished with certain devices specified therein.

Abstract: A projectile and associated method are provided for seeking a target that has been laser designated even though the projectile does not include a laser receiver. A projectile includes an aerodynamic body and a GPS receiver configured to receive GPS signals indicative of a location of the aerodynamic body. The projectile also includes a radio receiver configured to receive radio signals from an offboard laser receiver that provide information relating to a location of the target based upon laser designation of the target. Further, the projectile includes a processor configured to direct flight of the aerodynamic body toward the target based upon the location of the aerodynamic body as determined from the GPS signals and the location of the target based upon the information provided by the offboard laser receiver.

Abstract: A method and system to detect an improvised explosive device is disclosed. In a particular embodiment, the method includes dispersing a mixture containing a fluorescent material uniformly over a ground cover, illuminating the ground cover with wavelengths of visible light or ultraviolet (UV) light causing the fluorescent material to fluoresce in a visible light spectrum, and detecting where the mixture has been disturbed on the ground cover by visually observing inconsistencies in the fluorescent material on the ground cover that is fluorescing to indicate a location of the improvised explosive device. The method also includes that the mixture is adapted to cling to a person, clothes, or any combination thereof, upon contact.

Abstract: Textile armor (2) comprising at least one textile section (4) and corresponding supporting means (6), wherein the arrangement is such that the or each textile section is fully extended.

Abstract: The invention relates to a method of guiding a salvo of guided projectiles to a target. The method comprises the steps of generating a beam defining a common reference coordinate system, determining the position of each projectile relative to the beam, and providing to each projectile: position information of other projectiles. Further, the method includes the step of associating dispersion parameters to the salvo of guided projectiles. In addition, the method comprises the step of determining numerical values of the dispersion parameters based on accuracy uncertainty. Also, the method includes the step of controlling the projectiles to an optimal dispersion by using a swarming technique based on the position information of the projectiles and on the numerical values of the dispersion parameters.

Abstract: Systems and methods for coordinating fields of view are provided. Sensor data may be generated regarding movement in one or more planes and used as boundaries for the field of view. A geographic location may also be associated with the field of view. Fields of view from two or more geographic locations may be aggregated to determine a collective field of view. The collective field of view may be provided to an electronic display. In some cases, the field of view may be a field of fire associated with a ballistic weapon.

Abstract: A weapon system includes a number of WAN components, each WAN component includes a warhead, a launch mechanism for launching the warhead, an aiming mechanism for aiming the launch mechanism to launch the warhead in a desired direction, and a controller that, upon receipt of a command to aim and launch the warhead, operates the aiming mechanism to aim the warhead in the desired direction and then operates the launch mechanism to launch the warhead. The weapon system also includes a WAN component deployment mechanism for deploying the plurality of WAN components in a defended area; and a command center for instructing the controller of one or more of the WAN components to aim and launch the warhead of the each WAN component at a target that has been detected in the defended area.

Abstract: An interdiction device that includes a net for trapping and containing a target swimmer, diver or water-borne vessel. The net is deployed from the interdiction device that is either initially submerged in a body of water or floating on the surface of the body of water. The net is deployed either below the surface of the water in one embodiment or on the surface of the water depending on the desired function.

Abstract: A weapon system which includes an intermodal shipping container, an unmanned weapons unit, configured to fit substantially within said intermodal shipping container, an energy source capable of providing power to said weapon system, a computing processing unit, wherein computing processing unit is capable of controlling said weapon system, a lifting system, wherein said lifting system is capable of raising said unmanned weapons unit, and a camera system, wherein camera system is capable of capturing images and communicating said images to said computing processing unit.

Abstract: Multiple embodiments of a system are disclosed for defeating enemy missiles and rockets by the use of a non-lethal cloud of pellets that collide with the missile a certain distance away from the target causing premature detonation of the missile, and/or possible severe damage to the missile, and/or deflection of the missile, and/or a deformation to the ogive cones to cause a short in the fuze circuit, and/or deposition of conductive material to cause a short in the fuze circuit.

Abstract: An emitting structure for simulating an irradiance signature of a missile is provided. The emitting structure includes one or more radiation sources, each of which includes at least one ultraviolet radiation source and at least one infrared radiation source. The emitting structure also includes a spherical shell and a mechanism for positioning the radiation source(s) along a three dimensional boundary of the spherical shell. The emitting structure can locate and operate one of the radiation sources to simulate the irradiance signature of the missile.

Abstract: A method for guiding a gun-fired or mortared round towards an intended target. The method including: capturing image data from an image pick-up device during a descent of the round; transmitting the image data to a control platform remotely located from the round; transmitting guidance information to the round from the remote platform based on the captured image data; varying a flight path of the round based on the guidance information to guide the round towards its intended target.

Abstract: According to one embodiment, a system for protecting a vehicle from projectiles includes a detection component, an ignition component, and an adjustment component. In one embodiment, the detection component detects one or more projectiles having a first trajectory that is incident to a first location on the vehicle. In one embodiment, the ignition component ignites one or more rockets mounted on the vehicle to produce one or more exhaust streams. In one embodiment, the adjustment component adjusts the one or more exhaust streams to deflect the one or more projectiles to a second trajectory that is not incident to the first location on the vehicle.

Abstract: A self propelled flying vehicle (1) adapted to emulate a hostile firing action comprises an ultraviolet light source (5) in communication with a driving means (7) for driving the ultraviolet light source. The driving means (7) stores information indicative of an ultraviolet profile of a hostile firing action and, in use, communicates the ultraviolet profile to the ultraviolet light source (5).

Abstract: There is disclosed a collar (100) which may be attached to a munition in order to control the trajectory of the munition. The collar (100) has a collar body (10); a surface (12) for capturing the projectile as it leaves the barrel; a sill (14) for supporting the surface (12) at the muzzle of the barrel; and a guidance means (20a, 20b, 21a, 21b) for altering the flow of air around the collar (100). The collar (100) supports itself at the muzzle and may attach to the projectile at the surface (12) to integrate with the projectile as the projectile is fired. The collar (100) is particularly suited for attachment to mortar rounds. Such a collar (100) gives a weapon operator the option of increasing the precision of a munition without having to carry a plurality of munition types.

Abstract: An exo-atmospheric intercepting method for intercepting in space multiple objects, including acquiring and tracking multiple inflated objects which fly towards a protected territory. The method further includes launching an interceptor missile accommodating a plurality of kill vehicles each hosting a plurality of punching objects and classifying the multiple objects into clusters. In respect of each cluster of objects, determining an ejection condition responsive to meeting of which a kill vehicle is ejected from the interceptor missile towards the cluster of objects and thereafter releasing from the kill vehicle a plurality of punching objects such that every inflated object in the cluster is likely, with a high degree of certainty, to be punched by one or more punching objects.

Abstract: A vehicle for launching from a gun such as a gas gun and having a housing; preferably incorporating a precessional attitude control system; and utilizing a flared base, fins, or active use of the attitude control system during passage through the atmosphere. Subtly canting the fins can produce desired spinning of the vehicle. The propulsion system can employ liquid, hybrid, or solid fuel. A removable aero-shell assists atmospheric flight with thermal protection being provided by anticipated ablation, an ablative aero-spike, or transpirational cooling. And a releasable sabot enhances the effectiveness of the launch.

Abstract: A miniature lightweight high-maneuverability missile (10) has a missile body (12) with three sets of at least two aerodynamic control surfaces (14, 16, 18) for independent control of roll, pitch and yaw of the missile. Each set of control surfaces (14, 16, 18) is independently controlled by a corresponding actuator (20) deployed within the missile body (12). Other preferred features include selection of an elevation angle of incidence at a target, and switching between explosive and kinetic modes of operation.

Abstract: An active denial apparatus for use in non-lethal weaponry includes at least one focusing element configured to focus millimeter-wave energy along an axis of propagation. The at least one focusing element includes an astigmatic or dual axis focusing system configured to direct a focused beam that allows the active denial apparatus to accurately immobilize targets at both close and long range within acceptable limits of intensity.

Abstract: The systems and methods of the invention modulate atmospheric gases to temporarily increase the amount of atmospheric particles in the path of the debris, in order to decelerate the debris and accelerate natural orbital decay to the point of atmospheric re-entry. In one aspect of the invention, clearing the space debris includes propelling a plume of atmospheric gases substantially orthogonal to the path of the debris such that the debris collides with the gaseous plume as it passes through the plume. Increased atmospheric drag from the gaseous particles of the plume in the path of the debris obstructs a forward propagation of the debris and gradually decelerates the debris, leading eventually to atmospheric recapture.

Abstract: An interdiction device that includes a net for trapping and containing a target swimmer, diver or water-borne vessel. The net is deployed from the interdiction device that is either initially submerged in a body of water or floating on the surface of the body of water. The net is deployed either below the surface of the water in one embodiment or on the surface of the water depending on the desired function.

Abstract: The technology can include a retractable rotary turret system. The system includes a base comprising two support arms. The system further includes a turret platform that is a truncated sphere having a substantially flat side and a substantially spherical side. The turret platform includes a turret support ring rotary coupled to the two support arms and a turret device isolatively coupled to the turret support ring. The turret platform is rotatable along a first dimension for deployment of the spherical side and is rotatable along the first dimension for deployment of the flat side.

Abstract: A semi-continuous duty, Green Technology 14, robotic vehicle providing protection and security from underground mines. A deflector blade 11 follows natural existing contours to maintain straight line paths, while simultaneously carrying a mine detector 10, a vertical reciprocating ram set 30, 32 and 33 that preloads soil while also creating forward motion, followed by an energy dissipation, reaction system and containment canopy system 22, 24, 26 & 29.

Abstract: A method and device for impeding the progress of a swimmer or a diver included a plurality of tendrils that can be launched into the path of a target and entangle the target.

Abstract: Systems and methods described herein provide for the protection of personnel within vehicles and structures from handheld grenades and other threats. According to one aspect of the disclosure provided herein, a countermeasure system includes an expandable countermeasure having a flexible body with a number of weighted projectiles attached around a perimeter of the body. A threat detection and launch control system detects incoming threats and, in response, triggers a launch of the expandable countermeasure from the launcher to intercept and neutralize the threat.

Abstract: An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile.

Abstract: An interceptor system and method for dispensing of multiple kill vehicles, including, a carrier vehicle having a central carrier vehicle axis and axial propulsion integrated into the carrier vehicle, a payload adapter associated with the carrier vehicle for connecting a payload to a boost vehicle, the payload adapter being located aft of the carrier vehicle, and multiple kill vehicles mounted to the carrier vehicle radially around a circumference of the carrier vehicle.