Patent classifications
F41G7/224
SEARCH SUPPORT APPARATUS, SEARCH SUPPORT METHOD, AND COMPUTER-READABLE RECORDING MEDIUM
A search support apparatus includes: a search sensor unit 2; an environment sensor unit 3 configured to generate environment information; a search effective range estimation unit 4 configured to estimate the search effective range of the search sensor unit 2 using the environment information and performance information that indicates the performance of the search sensor unit; a threat effective range estimation unit 5 configured to estimate the search effective range of a sensor possessed by a target that is a threat using the environment information and performance information that indicates the performance of the sensor possessed by the target; and a route calculation unit 6 configured to calculate a search route to the object, based on the search effective range of the search sensor unit 2, the search effective range of the sensor possessed by the target, and a distribution of existence probabilities of the target that is a threat.
Unauthorized electro-optics (EO) device detection and response system
A system is disclosed to identify authorized EO devices and unauthorized EO devices within a scene. The system responds with a variety of response actions including sending warning messages of the unauthorized EO devices, recording images and position of the unauthorized EO device. The system can further be configured to hamper the operation of the unauthorized EO devices detected within the scene.
COUNTER DRONE SYSTEM
The system comprises a plurality of sensor systems, a counter drone, and a processor. A sensor system of the plurality of sensor systems comprises one or more sensors that are connected to a network. The counter drone is connected to the network. The processor is configured to receive an indication of a potential target from the plurality of sensor systems; generate a fused data set for the potential target, determine whether the potential target comprises the threat drone based at least in part on the fused data set; and in response to determining that the potential target comprises the threat drone, provide counter drone instructions to the counter drone.
Towed, autonomous, or remotely controlled airborne mobile system including a plurality of reflection structure sections and shapes adapted for attracting attention of search systems configured for sensing pattern recognition based electromagnetic or visual reflections from the structures and shapes and related methods
Methods and structures associated with a towed, autonomous, or remotely controlled airborne mobile system including a plurality of reflection structure sections and shapes adapted for attracting attention of search systems configured for sensing pattern recognition based electromagnetic or visual reflections from the structures and shapes and related methods.
Flight-path determination device and flight-path determination method
A flight-path determination device for determining a flight path of a flying object has a position determination apparatus to detect a position of the flying object, an alignment apparatus that to verify whether the position of the flying object is within one specified approach path of a number of specified approach paths, and a path determination apparatus to output the relevant approach path as the flight path of the flying object if the position of the flying object is within one of the specified approach paths.
System and method for detecting multiple fragments in a target missile
A system and method is provided for detecting the trajectory of multiple fragments through a conic or cylindrical section, such as the body of a missile. Three or more sensors are placed on the on the body of the object. Each of the sensors is constructed and arranged to measure signals to the sensor at from impacts on one or more locations on the body. The sensor then transmits a signal commiserate with the impact of a fragment thereon. A computer system is also provided to perform necessary calculations and, potentially, record the impact times and locations. When the body of the object is hit by fragments or shrapnel, a signal from one or more of the sensors is sent to the computer system. This operation is performed and constantly updated for all locations where a fragment is detected by one or more of the sensors. Waveforms of the impacts are recorded, but because multiple hits can occur, there can be superposition (or destruction) of the resulting waveform sent to the computer system. The computer system can interpret which superposition or destruction is indicative of another fragment strike, and filter out those additions or subtractions to the waveforms that could not possibly be from another fragment.
Method and device for providing a dummy target for protecting a vehicle and/or an object from radar-guided seeker heads
A method and a device for providing a dummy target via decoy chaffs for protecting a vehicle and/or an object from radar-guided missiles. After identification of the radar-guided missile and calculation of a decoy chaff pattern, the decoy chaff pattern is presented in the form of polar coordinates in accordance with the firing of shots, a cut-off distance for the determination of a defence radius is then found in these polar coordinates. A minimum distance between the disassembly or detonation points within the defence radius is set. The dummy target is then optimized on the basis of the cut-off distance and the minimum distance between the disassembly or detonation points. As a result of this calculation, the only decoy chaffs that are deloyed are those that meet the conditions, i.e. that have a minimum distance between the disassembly or detonation points within the defence radius in the optimized dummy target.
METHODS AND APPARATUSES FOR AERIAL INTERCEPTION OF AERIAL THREATS
Embodiments include active protection systems and methods for an aerial platform. An onboard system includes radar modules, detects aerial vehicles within a threat range of the aerial platform, and determines if any of the aerial vehicles are an aerial threat. The onboard system also determines an intercept vector to the aerial threat, communicates the intercept vector to an eject vehicle, and causes the eject vehicle to be ejected from the aerial platform to intercept the aerial threat. The eject vehicle includes alignment thrusters to rotate a longitudinal axis of the eject vehicle to substantially align with the intercept vector, a rocket motor to accelerate the eject vehicle along an intercept vector, divert thrusters to divert the eject vehicle in a direction substantially perpendicular to the intercept vector, and attitude control thrusters to make adjustments to the attitude of the eject vehicle.
THREAT WARNING SYSTEM
The present disclosure provides a threat warning system that utilizes an image sensor and an active radar to determine whether a muzzle flash is the source of a threat to a platform carrying the threat warning system. The threat warning system may be a new operation of existing or legacy components on a platform that are implemented as a software update to accomplish the new objectives of the present disclosure. Alternatively, the components described herein may be provide as a newly constructed group of components networked together to accomplish the intended functions of the present disclosure.
System for deploying a first object for capturing, inhibiting, immobilising or disabling a second object
A system for inhibiting the electronic system of a target object is provided. The system comprises an Electronic Counter Measure (ECM) unit, and a projectile for carrying the ECM unit towards the target object.