Abstract: A method of determining position and orientation of an object using a profilometer. A measurement body has a predetermined polyhedral basic form and a defined spatial relationship with the object. The profilometer captures rectilinear coordinates of at least three measurement points lying on a profile line defined by a profilometer scan-line. Using the coordinates and measurement body geometric values, rotations of the measurement body are calculated about a measurement body z-axis, an intermediate y-axis resulting from the z-axis rotation, and about a profilometer-defined x-axis. Next, three translation displacements of the measurement body relative to the three profilometer-defined axes are calculated using the coordinates, the geometric values of the measurement body, and the above-calculated rotations. The position and an orientation of the object is determined by then applying the defined spatial relationship of the measurement body to the object.

Abstract: A system for deploying a first object for capturing, immobilising or disabling a second object is provided. The system comprises the first object, a projectile for carrying the first object therein, and a launcher for launching the projectile towards the second object, wherein the projectile is configured for deploying the first object in the vicinity of the second object for capturing, immobilising or disabling the second object.

Abstract: Methods aim to reduce and/or eliminate the need for shims in manufacturing assemblies, such as in manufacturing of aircraft wings. Exemplary methods include predicting a set of predicted manufacturing dimensions within a range of predetermined allowances for a first part, manufacturing the first part, scanning the first part to determine a set of actual manufacturing dimensions for the first part, and at least beginning manufacturing a second part before the scanning the first part is completed. The second part may be manufactured based on the set of predicted manufacturing dimensions for the first part. Once the scan of the first part is completed, the set of predicted manufacturing dimensions may be compared to a set of actual manufacturing dimensions to check for any non-compliant deviances between the predicted and actual manufacturing dimensions. Repairs and local re-scans may be performed in the areas of the non-compliant deviances, which may streamline manufacturing.

Abstract: Embodiments of an airborne synthetic phased antenna array include a plurality of airborne antennas and phase shifters for the antennas. The antennas are operated coherently, and constant phase shifts between the antennas are maintained. In addition, methods for providing wireless communication services include providing a plurality of airborne platforms, providing RF antennas for wireless communication services and phase shifters for the RF antennas on at least two airborne platforms, and operating the phase shifters to maintain synchronous operation of the RF antennas.

Abstract: A method for providing a display on a head-worn display includes receiving imagery from one or more sensors configured to capture details of an environment surrounding an aircraft, receiving a current gaze of a user of the head-worn display, and processing the imagery. Processing the imagery comprises identifying one or more attributes of the imagery. The method further includes identifying at least two layers of the imagery. At least one of the at least two layers has a different resolution than another layer. The method further includes determining a priority of each of the at least two layers based on the one or more attributes and the current gaze of the user. The method further includes transmitting one or more of the at least two layers to the head-worn display based on the determined priority of the layers.

Abstract: An imaging apparatus performs control to display first region information indicating a first region that is a region gazed at by a user and second region information indicating a second region that is a region of a main object within a region of a shot image region so as to be distinguishably superimposed on the shot image. In the above control, the imaging apparatus displays the first region information and the second region information based on the information on the identical position before the first instruction means is operated, and after the first instruction means is operated, the first region information and the second region information are displayed based on information of different positions corresponding to each region.

Abstract: A target designator for a guided weapon is disclosed. The designator has a sight arranged to display, in operation, a reticule superimposed upon a field of view. The reticule is moveable within the field of view. The designator further comprises an eye tracker operable to track the gaze of the operator whilst the operator uses the sight. The eye tracker communicates with the sight such that the reticule moves so as to be aligned with the direction of the gaze of the operator.

Abstract: Provided is a data processing method for determining rotation by a marker device of a medical tracking system about its mount. The data processing method includes acquiring a first marker device position dataset which represents a position of the marker device before a movement of the marker device. A second marker device position dataset is acquired which represents the position of the marker device after a movement of the marker device. A marker device displacement dataset is calculated, which represents the displacement of the marker device, from the first and second marker device position datasets. At least one axis of rotation of the marker device displacement dataset is calculated. A determination is made whether or not the marker device is rotated about its mount from the position of the at least one axis of rotation relative to the marker device.

Abstract: The invention relates to a single system that can simultaneously protects a plurality of assets, such as soldiers, vehicles and structures in a given perimeter. The assets are, for example, vehicles and structures that could not otherwise be protected due to tactical and mechanical limitations.

Abstract: A method includes sampling a first intensity of light with a first array of photo detectors of a digital camera. A second intensity of light is sampled with a second array of photo detectors of the digital camera. A first channel processor coupled to the first array of photo detectors generates a first image using first array data which is representative of the first intensity of light sampled by the first array of photo detectors. A second channel processor coupled to the second array of photo detectors generates a second image using second array data which is representative of the second intensity of light sampled by the second array of photo detectors. The first array of photo detectors, the second array of photo detectors, the first channel processor, and the second channel processor are integrated on or in a semiconductor substrate.

Abstract: 1. An embodiment of an attention monitoring eye-view image and attention recording apparatus includes an eyeglass frame, at least one first optical unit disposed on the eyeglass frame for capturing an image corresponding to a field of view of a user, and at least one second optical unit disposed on the eyeglass frame for tracking movement of at least one eye of the user to determine a direction within the field of view to which the at least one eye is directed. The eye-view image recording apparatus further includes at least one accelerometer to track the head movement of the user and at least one processor to determine the user's mental attention level and the direction within the field of view to which the at least one eye is directed, and generating a subset of the captured image based on the determination.

Abstract: A method of tracking objects of a scene is disclosed. The method determines two or more tracks which have merged. Each track is associated with at least one of the objects and having a corresponding graph structure. Each graph structure comprising at least one node representing the corresponding track. A new node representing the merged tracks is created. The graph structures are added as children nodes of the new node to create a merged graph structure. A split between the objects associated with one of the tracks represented by the nodes of the merged graph structure is determined. Similarity between one or more of the nodes in the merged graph structure and foreground areas corresponding to split objects is determined. One of the nodes in the merged graph structure is selected based on the determined similarity. A new graph structure for tracking the objects is created, the new graph structure having the selected node at the root of the new graph structure.

Abstract: Introduced herein are various techniques for displaying virtual and augmented reality content via a head-mounted display (HMD). The techniques can be used to improve the effectiveness of the HMD, as well as the general experience and comfort of users of the HMD. An HMD may increase and/or decrease the resolution of certain areas in digital content that is being viewed to more accurately mimic a user's high resolution and low resolution fields of view. For example, the HMD may monitor the user's eye movement to identify a focal point of the user's gaze, and then increase the resolution in an area surrounding the focal point, decrease the resolution elsewhere, or both. Predictive algorithms could also be employed to identify which areas are likely to be the subject of the user's gaze in the future, which allows the HMD to present the regionally-focused content in real-time.

Abstract: The invention comprises using a photodetector that it sensitive in the MWIR band, performing image differencing on two successive images at a time, and defining thresholds for said differences in order to extract only those exceeding the threshold used.

Abstract: A method for determining geo-position of a target by an aircraft includes: receiving navigation data related to the aircraft including aircraft attitude information; receiving multilateration information related to the target including an angle to the target; calculating an axis for a cone fixed to the aircraft, based on the received aircraft attitude information; calculating a central angle for the cone from the received angle to the target; generating two vectors orthogonal to the cone axis; calculating a cone model from the axis, the central angle and the two vectors; and intersecting the cone model with an earth model to obtain a LEP curve, wherein the LEP curve is used to determine the geo position of the target.

Abstract: An aircraft control device determines, on the basis of relative positional relations between an individual aircraft and a target aircraft, a role of the individual aircraft with respect to the target aircraft, and a trajectory of the individual aircraft based on control operations determined according to the role of the individual aircraft. As an example, the aircraft control device represents the role of the individual aircraft with respect to the target aircraft as a numerical value and changes the role of the individual aircraft a plurality of times by changing the numerical value. Every time the role of the individual aircraft is changed, a minimum distance to target is calculated for the individual aircraft, and the role of the individual aircraft having the largest minimum distance to target is determined as the role of the individual aircraft.

Abstract: A ball joint gimbal imaging system includes on-gimbal optics that reimage a front optical aperture to a smaller back optical aperture that moves with the rotation of the inner ball. Relay optics are configured to relay the back optical aperture to an electro-optic component mounted on the platform, off-gimbal. Relay optics includes a first two-axis steering element (on or off-gimbal) that is positioned and sized to cover the range of motion of the beam from the back optical aperture across the range of gimbal motion. The first two-axis steering element is controlled to steer the optical beam passing through the back optical aperture into a second off-gimbal two-axis steering element that is controlled to tilt the optical beam to align light along the central axis of the electro-optic element with the central axis of the front optical aperture on the inner ball, which is coincident with the gimbal pointing axis.

Abstract: A system and methods are disclosed for providing integrated software development environment for the design, verification and validation of advanced automotive safety systems. The system allows automotive software to be developed on a host computer using a collection of computer programs running simultaneously as processes and synchronized by a central process. The software disclosed uses separate synchronized processes, permitting signals from disparate sources to be generated by a simulation running on the host computer or from actual sensors and data bus signals coming from and going to actual vehicle hardware which is connected to their bus counterparts in the host computer on a real-time basis. The methods provide a data model that first extends the capabilities of the physical data model and then translates, gates, optimizes, fuses, filters and manages the physical representation of the logical model into a state estimation of the situation around the vehicle.

Abstract: Wireless tracking systems and devices to detect the status of aircraft cargo containers. The system uses a sensor array to deactivate and activate the tracking devices as needed to comply with FAA regulations. The tracking systems use an array of machine vision sensors and/or inertia (motion) sensors to determine when to activate and deactivate the device. The tracking systems can feature LTE communication devices with a global roaming SIM card to realize true global operation to support GSM, CDMA and other mobile environments seamlessly.

Abstract: An optical device includes a housing containing a plurality of lenses. At least one of those lenses includes a reticle. An optical device and a processor are also located in the housing. A wind speed sensor is mounted to the housing and configured to send a wind speed signal corresponding to a wind speed to the processor. The processor calculates a wind speed based at least in part on the wind speed signal, and wherein the processor sends an output signal corresponding to the calculated wind speed to the output device.

Abstract: A method for tracking an object using radar includes detecting a wideband radio frequency (“RF”) energy at a first radar sensor tracking the object and determining in a computer process if a booster is propelling the object based on the wideband RF energy. The object is tracked in a computer process based on a ballistic trajectory if the booster is not propelling the object, and the object is tracked in a computer process based on a non-ballistic trajectory if the booster is propelling the object.

Abstract: According to one embodiment, a target tracking apparatus calculates N-dimensional predicted values from a respective stored (N+1)-dimensional tracks for each of the targets, determines whether or not the N-dimensional predicted value for each of the targets is correlated with the received N-dimensional angle observed value for the target, if the N-dimensional predicted value is not correlated, generates a new (N+1)-dimensional track for the target based on the N-dimensional track corresponding to the N-dimensional angle observed value and if the N-dimensional predicted value is correlated, updates and stores the (N+1)-dimensional track using the N-dimensional angle observed value.

Abstract: A sight and methods of operation thereof are provided. In some embodiments, an image is captured via an image capture unit, and a center position is calculated according to the positions of at least three impact points in the image, and a predefined view center of a display unit is set to the center position. In some embodiments, an angle of dip of the sight to a plane is detected via a dip angle detector. A predictive impact point is calculated according to the angle of dip and at least one calculation parameter, and an impact point indication is accordingly displayed in the display unit. When the angle of dip is changed, the predictive impact point is recalculated according to the new angle of dip, and the corresponding impact point indication is displayed.

Abstract: System and methods for managing targets of a vehicle is provided. In some aspects, a system may include a boundary check module configured to receive boundary information from a flight safety system. The boundary information comprises a selected termination boundary of a plurality of termination boundaries confining navigation of the vehicle. Each of the plurality of termination boundaries is associated with a target of a plurality of targets of the vehicle. The system may further include a target modification module configured to select the target associated with the selected termination boundary, and a target guidance module configured to provide the selected target to a guidance and control system of the vehicle.

Abstract: A sighting apparatus for a firearm includes a video camera capable of capturing and tracking the path of a projectile The captured images are taken generally concurrently with the firing of the first projectile, and with the projectile reaching the target. A video display includes a reticle positioned at the center of the display to permit the user to aim the firearm by positioning the reticle over the target. A processor receives captured images from the camera. An output interface delivers information to the video display to enable the video display to display images of the target area. Software and a processor determine the flight path of the projectile and the point where the projectile impacts or passes by the intended target and adjusts for the variance between the two points by moving the image on the display.

Abstract: Systems and methods based on firing table fitting allow interception of a small low-altitude low-velocity target. A system includes: a target detecting system, a directing control system, a launch control system, an interception execution system, a communication bus a, a communication bus b and a communication bus c. Firing table data under a standard working condition and fitting parameters under different working conditions are pre-stored in the system. Based on target flight data and environment condition parameters, a lead aiming point is predicted, a time sequence of each stage of a fight flow is controlled, and firing data are output to execute an interception by the launch control system. An interception operation is simplified, a ground control of a non-controlled bomb fight flow is realized, a single shot success probability of an interception system is increased, and an interception cost is reduced.

Abstract: An example method includes receiving output voltage data from an array of at least four thermopiles placed around the circumference of a projectile such that for any rotation of the projectile during flight thereof, at least a pair of the thermopile having upwardly-facing fields of view referenced to the earth-fixed coordinate system. The method includes determining the pair of upwardly-facing thermopiles based on the output voltage data from the array, with the respective pair of thermopiles including a thermopile p and next adjacent thermopile p+1. The method includes determining a ratio of the output voltage data from thermopiles p and p+1, and applying the ratio to a function associating, for any pair of thermopiles n and n+1, a ratio of output voltage data from thermopiles n and n+1, and a roll angle ?n of thermopile n referenced to the earth-fixed coordinate system.

Abstract: An apparatus and system for allowing accurate navigation to a target regardless of GPS jamming levels. An apparatus and system can be used to update the navigation solution based upon seeker measurements in at least one of three electromagnetic frequency domains: infrared, visible, and radio frequency (RF).

Abstract: Systems and methods allow for intercepting a small, low-altitude and low-velocity target. A system includes a detecting apparatus, a directing control apparatus, an aiming control apparatus, a launch control apparatus, a launching device, and an intercepting device. A method includes: searching and tracking a target by the detecting apparatus in a networking mode, or by the aiming control apparatus in a single-soldier mode; sending target information to the launch control apparatus; performing a trajectory calculation by the launch control apparatus; and launching the intercepting device by the launching device to intercept the target. A low-cost system with a short response time can thus be realized. The target falls with the net at a low velocity under a parachute, and this is desirable in a city environment.

Abstract: A system and method calculate a range and velocity of an object in image data. The range calculation includes detecting a contour of the object from the image data, forming a template from the image data based on the contour; and calculating a range to the object using pixel resolution and dimension statistics of the object. A three-dimensional velocity of the object is determined by calculating a radial component and an angular component of the velocity. The radial velocity component is calculated by determining the range of the object in two or more image frames, determining a time differential between the two or more image frames, and calculating the radial velocity as a function of the range of the object in the two or more image frames and the time differential between the two or more image frames. The angular component is calculated using spatial-temporal derivatives as a function of a motion constraint equation.

Abstract: A method including detecting a threat incoming to a vehicle, the vehicle having a plurality of countermeasures including a primary armament and an active protection system, communicating the detected threat to a controller, activating, with the controller, a first sensor in response to the detecting, the first sensor tracking the incoming threat and generating tracking data, routing, with the controller, the tracking data to a plurality of fire control processors, each of the plurality of fire control processors being associated with a respective one of the plurality of countermeasures, and the plurality of fire control processors simultaneously computing respective firing solutions using the tracking data, and determining, with the controller, a preferred countermeasure out of the plurality of countermeasures with which to counter the incoming threat.

Abstract: This invention relates to a method, system and computer program product that calculates a real-time, accurate, firing solution for man carried weapon system; specifically a transparent display to be located in-line with a weapon mounted optic and a device to adjust the aim point through real-time data collection, analysis and real-time visual feedback to the operator. A firing solution system mounted on a projectile weapon comprising: A Sensor and CPU Unit (SCU) and a Sight Adjusted Reticule (SAR) and a PC Dongle which configured to facilitate communication between the SCU and a personal computer (PC), or similar computing device, enabling management of the SCU configuration and offloading of sensor obtained and system determined data values.

Abstract: Apparatus and methods for an airborne biota monitoring and control system are disclosed. Radar and laser/optical sensors are used to detect insects, with detection zones being over water in some embodiments to reduce backscatter clutter. A pest control laser or small autonomous or radio controlled aircraft under automated or human control may be used to disable a targeted flying insect. One embodiment includes use of a head-mounted display for displaying insect targeting information superimposed on a real landscape view. Technologies such as adaptive lens, holographic optical elements, polarized radar and/or laser beams, light amplifiers and light guides, thin disk, spinning disk, or vertical cavity surface emitting lasers enhance performance of the apparatus or reduce cost of the apparatus. Also disclosed are methods of discrimination of insect types using spectral information and dynamic relative variation of spectral intensities at different wavelengths reflected from an insect in flight.

Abstract: Embodiments of automated structural interpretation are described. In some embodiments, a method includes identifying one or more object points belonging to an object to be tracked; tracking a trajectory of the one or more object points, including: calculating a plurality of etalons around at least one of the one or more object points using one or more different angular parameters; selecting one or more candidate points for evaluation; extracting one or more samples from around the one or more candidate points; and evaluating a next trajectory location of the one or more object points based at least partially on the one or more samples and one or more of the plurality of etalons.

Abstract: A passive electro-optical tracker uses a two-band IR intensity ratio to discriminate high-speed projectiles and obtain a speed estimate from their temperature, as well as determining the trajectory back to the source of fire. In an omnidirectional system a hemispheric imager with an MWIR spectrum splitter forms two CCD images of the environment. Three methods are given to determine the azimuth and range of a projectile, one for clear atmospheric conditions and two for nonhomogeneous atmospheric conditions. The first approach uses the relative intensity of the image of the projectile on the pixels of a CCD camera to determine the azimuthal angle of trajectory with respect to the ground, and its range. The second calculates this angle using a different algorithm. The third uses a least squares optimization over multiple frames based on a triangle representation of the smeared image to yield a real-time trajectory estimate.

Abstract: In order to target and intercept a desired object within a number of objects detected in an environment, detection data is received from two different sensors, where the detection data includes spatial coordinates. A set of four-point subsets (tetrahedra) are selected from each set of spatial coordinates. A number of correlation maps are determined between the first set of spatial coordinates and the second set of spatial coordinates based on the plurality of four-point subsets. The mean sphericity for each corresponding plurality of four-point subsets in the plurality of correlation maps is determined, and a threat object map based on the correlation map having the greatest mean sphericity is created. The desired object is targeted based on the correlation map.

Abstract: A passive electro-optical tracker uses a two-band IR intensity ratio to discriminate high-speed projectiles and obtain a time-varying speed estimate from their time-varying temperature, as well as determining the trajectory back to the source of fire. In an omnidirectional system a hemispheric imager with an MWIR spectrum splitter forms two CCD images of the environment. Various methods are given to determine the azimuth and range of a projectile, both for clear atmospheric conditions and for nonhomogeneous atmospheric conditions. One approach uses the relative intensity of the image of the projectile on the pixels of a CCD camera to determine the azimuthal angle of trajectory with respect to the ground, and its range. A second uses a least squares optimization over multiple frames based on a triangle representation of the smeared image to yield a real-time trajectory estimate.

Abstract: A high-speed automatic fire net-based fire instruction control system for a short-range anti-aircraft gun is provided. More particular, the present invention relates to a system, in which when a short-range anti-aircraft gun gunner calibrates values indicated on equipment and follows instructions without personally viewing a flying object that has infiltrated at low altitude, a tracking and automatic fire net is constructed, and the gunner follows fire instructions, thus allowing gunners to easily cope with targets anywhere regardless of the location, such as an anti-aircraft defensive position or a contact area, as long as the targets appear on a detection radar even in unfavorable weather or at night which forbids the targets from being detected and identified with eyes.

Abstract: A method including detecting a threat incoming to a vehicle, the vehicle having a plurality of countermeasures including a primary armament and an active protection system, communicating the detected threat to a controller, activating, with the controller, a first sensor in response to the detecting, the first sensor tracking the incoming threat and generating tracking data, routing, with the controller, the tracking data to a plurality of fire control processors, each of the plurality of fire control processors being associated with a respective one of the plurality of countermeasures, and the plurality of fire control processors simultaneously computing respective firing solutions using the tracking data, and determining, with the controller, a preferred countermeasure out of the plurality of countermeasures with which to counter the incoming threat.

Abstract: A network-centric targeting system includes a prepare module to plan for targeting engagements and to identify a target; a sense module to locate targets of opportunity and targets generated by the prepare module to form targeting information; a refine module to enhance the targeting information from the sense module; a track module to maintain a location of a target, a state of the target and target activity, the track module being coupled to the refine module; a target module to select effects and to coordinate delivery of selected effects to the target, the target module being coupled to the track module, the refine module and the sense module; a deliver module to deliver effects to the target, the deliver module being coupled to the track module, the refine module, the target module and the sense module; and an assess module to assess effectiveness of the delivered effects on the target.

Abstract: A system and method for dual-band detection of incoming threats using an initial passive detection system and a selectively activated active detection system. Advantages include improved threat detection accuracy, reduction of false alarms, and reduced radiation emission from the active system, thereby making the active system more difficult to detect and reducing irradiation levels of users and bystanders. Variations include systems employing passive optical or electro-optical detectors, systems employing active RADAR or LADAR detectors, and systems connected to alarm signal/threat mitigation systems. The system may be configured for use on ground vehicles or small watercraft. Variations of the system may be specifically configured to detect incoming munitions launches.

Abstract: The present invention relates to a hierarchical system and method for task assignment (TA), coordination and communication of multiple Unmanned Aerial Vehicles (DAV's) engaging multiple attack targets and conceives an ad-hoc routing algorithm for synchronization of target lists utilizing a distributed computing topology. Assuming limited communication bandwidth and range, coordination of UAV motion is achieved by implementing a simple behavioral flocking algorithm utilizing a tree topology for target list routing. The TA algorithm is based on a graph-theoretic approach, in which a node locates all the detectable targets, identifies them and computes its distance to each target. The node then produces an attack plan that minimizes the sum of distances of the UAV's in the subtree of a given node to the targets.

Abstract: Methods and apparatus for launching an effector according to various aspects of the present invention may include a fire control system. The fire control system may be responsive to a sensor, such as a radar, and may be connected to the effector, such as via a launcher. The file control system may be adapted to generate a fire control solution according to the data from the sensor, initiate a launch of the effector, and provide the fire control solution to the effector after initiating the launch.

Abstract: A method, computer program product, and target tracking system for obtaining a first kinematic state measurement of a first projectile detection event from a first sensor. The first kinematic state measurement includes a first time measurement and a first state vector. A second kinematic state measurement of a second projectile detection event is obtained from a second sensor. The second kinematic state measurement includes a second time measurement and a second state vector. If it is determined that at least a portion of the first kinematic state measurement and at least a portion of the second kinematic state measurement define at least a portion of a flight trajectory orbital ellipse, the first projectile detection event and the second projectile detection event are defined as portions of a flight trajectory of a single ballistic projectile.

Abstract: A high-speed automatic fire net-based fire instruction control system for a short-range anti-aircraft gun is provided. More particular, the present invention relates to a system, in which when a short-range anti-aircraft gun gunner calibrates values indicated on equipment and follows instructions without personally viewing a flying object that has infiltrated at low altitude, a tracking and automatic fire net is constructed, and the gunner follows fire instructions, thus allowing gunners to easily cope with targets anywhere regardless of the location, such as an anti-aircraft defensive position or a contact area, as long as the targets appear on a detection radar even in unfavorable weather or at night which forbids the targets from being detected and identified with eyes.

Abstract: A computer-implemented method for estimating track error covariance of a sensor track data in a Link 16 tactical data link network from track quality involves receiving at a computer system the sensor track data on a ballistic target including the track quality and by estimating the track maturity, the position and velocity error covariance eigenvalues (?p, ?v), and the position and velocity error covariances (Cp, Cv), the track error covariance of the sensor track data is calculated. The resulting error covariance is provided to the weapons control systems for more accurate engagement of the ballistic targets.

Abstract: The present invention increases the survivability of a helicopter by prioritizing a threat engagement sequence for a laser-based countermeasure system based on the determined relative lethality of each detected visually trained threat (e.g., small arms fire). The system and method defines a plurality of threat effectiveness merit factors, or lethality factors, that are determinable from available helicopter navigation and sensor data, to quantify the danger associated with each detected threat. The system and method then combines the defined lethality factors using a mathematical function, such as a merit function, to numerically quantify the level of threat posed by each threat. The calculated threat values for each of the detected threats are compared to prioritize the threats for engagement by a laser-based countermeasure system, such as a Visual Acquisition Disrupter (VAD) system.

Abstract: A tracking device includes: an image sensor that obtains image information of an image present within an image plane formed via an optical system; a tracking unit that tracks a target within the image plane based upon the image information; a focus detection unit that detects a focus adjustment state of the optical system over at least one focus detection area set in the image plane; a focus adjustment unit that executes focus adjustment for the optical system based upon the focus adjustment state detected in the focus detection area corresponding to a position of the target; a decision-making unit that makes a decision as to whether or not the target is being tracked based upon results of tracking operation executed by the tracking unit; and a control unit that bans the focus adjustment based upon results of the decision made by the decision-making unit.

Abstract: A Reconfigurable Nose Control System (RNCS) is designed to adjust the flight path of spin-stabilized artillery projectiles. The RNCS uses the surface of a projectile nose cone as a trim tab. The nose cone may be despun by the action of aerodynamic surfaces, to zero spin relative to earth fixed coordinates using local air flow, and deflected by a simple rotary motion of a Divert Motor about the longitudinal axis of the projectile. A forward section of the nose cone having an ogive is mounted at an angle to the longitudinal axis of the projectile, forming an axial offset of an axis of the forward section with respect to the longitudinal axis of the projectile. Another section of the nose cone includes another motor, the Roll Generator Motor, that is rotationally decoupled from the forward section and rotates the deflected forward section so that its axis may be pointed in any direction within its range of motion.

Abstract: Methods and apparatus for countering a projectile according to various aspects of the present invention may operate in conjunction with a countermeasure system. The countermeasure system may comprise a beam source adapted to generate an electromagnetic beam. The countermeasure system may further include a beam control system adapted to aim the electromagnetic beam at the projectile according to a fire control solution. The beam heats at least a portion of the projectile to a disruption temperature to deflagrate the projectile.