Abstract: A camera-based mixed reality glass apparatus, includes: a smart glass unit including: a band-type flexible display disposed in an eye direction of a user, a head engaging band mounting the band-type flexible display and formed along a head of the user and a plurality of cameras mounted on an opposite direction to the eye of the user in the band-type flexible display and disposed along the head of the user, a real image processor for generating and transmitting a peripheral image of the user through the plurality of cameras, a virtual image processor for generating a direct or indirect virtual image according to a control of the user, and a mixed reality image processor for overlaying the virtual image on the peripheral image of the user and displaying the virtual image on the band-type flexible display.

Abstract: A point of aim shows where a weapon is aimed on a target. An electronic device determines an impact location on the target of a projectile fired from the weapon, determines a distance from the point of aim to the impact location, and moves the point of aim in order to sight the weapon to the target.

Abstract: A rifle scope includes a housing configured to mount to a rifle. The rifle scope further includes a network transceiver within the housing and configured to communicate bi-directionally with at least one of a network and an electronic device configurable to communicate with to the network.

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: A method includes determining a shot count within an optical device coupled to a firearm. The shot count corresponds to a number of shots taken using the firearm. The method further includes determining a muzzle velocity parameter from a life-cycle profile of the firearm based on the shot count as an input into a ballistics solution.

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: A method includes receiving location data corresponding to a physical location of a user at a computing device and receiving prey data corresponding to a relative position of an animal at the computing device from a gun scope. The method further includes determining a location of the animal relative to the computing device based on the location data and the prey data.

Abstract: Disclosed embodiments, as well as features and aspects thereof, are directed towards providing a system, device and method for calculating comprehensive ballistic solutions, or portions thereof, via a varying magnification optical range determining and ballistic trajectory calculating apparatus referred to as a ballistic solutions device. Advantageously, embodiments of a ballistic solutions device may drastically reduce marksman error in milling targets by employing a measurement component configured to measure angular movement of a projectile launching device, such as a rifle, thus delivering consistently accurate distance to target estimations. Additionally, embodiments of a ballistic solutions device may also comprise features and aspects that enable a user to leverage available real-time field data such that error associated with the measurement of those variables is minimized prior to calculating and rendering a comprehensive ballistic solution derived from stored DOPE.

Abstract: A method includes determining a shot count within an optical device coupled to a firearm. The shot count corresponds to a number of shots taken using the firearm. The method further includes determining a muzzle velocity parameter from a life-cycle profile of the firearm based on the shot count as an input into a ballistics solution.

Abstract: Technology for predicting and correcting a trajectory is described. The technology can create a model to predict a position of the reusable launch vehicle at a time in the future; observe a wind condition during ascent of the reusable launch vehicle; store the observed wind condition in a wind map; predict during ascent a position and a terminal lateral velocity of the reusable launch vehicle at a terminal altitude; and correct a flight trajectory of the reusable launch vehicle based on the wind map.

Abstract: Systems, apparatus, and methods are provided which: (a) receive wired or wireless transmission of information regarding an orientation of a weapon; (b) receive wired or wireless transmission of information regarding an orientation of a viewing area of a head-mounted display apparatus; (c) process ballistic information of ammunition to be fired by the weapon and the information regarding the orientations of the weapon and the viewing area to obtain a calculated endpoint of the ammunition to be fired by the weapon; and (d) display an icon (e.g., a crosshair) representative of the endpoint of the ammunition in the viewing area of the head-mounted display apparatus.

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: An analog ballistic system calculator for long range shooting is constructed of a pair of rugged, waterproof rotatable transparent discs superimposed over a base member on one side and a single transparent rotatable disc on the opposite side of the base. The hand held calculator device provides a wind speed and direction and air temperature adjusted calculator device for long distance rifles.

Abstract: A ranging system for use with a projectile launching device is provided. The ranging system includes an alignment marker visible with an optical sight device. The position of the alignment marker is adjusted based at least on a determined range to a target.

Abstract: An advanced weapon scope system, particularly for 21st century nighttime tactical situations is disclosed herein. A preferred embodiment includes multiple sensors coupled to a thermal scope to provide input to a ballistics computer also provided to the scope. The device is further programmable and can record nighttime tactical events as desired by a user. Other features include automatic recognition of a living target based on a temperature threshold and automatic identification of weapon based on RFID scanning. Another preferred embodiment provides for command center remote monitoring via a wireless module such as Wi-Fi.

Abstract: An aiming system for use with a weapon is provided and may include a processor, at least one sensor in communication with the processor, and a memory in communication with the processor. The aiming system may also include a display in communication with the processor that displays a corrected-aiming point based on at least one simulated bullet trajectory and at least one simulated bullet impact location determined by the processor.

Abstract: A computer-implemented method is provided for determining fratricide probability of projectile collision from a projectile launcher on a platform and an interception hazard that can be ejected or launched from a deployment position. The platform can represent a combat vessel, with the projectile launcher being a gun, the interception hazard being a missile, and the deployment position being a vertical launch cell. The projectile launcher operates within an angular area called the firing zone of the platform. The method includes determining the firing zone, calculating an angular firing area, quantifying a frontal area of the interception hazard, translating the resulting frontal area across a flight trajectory, sweeping the projectile launcher to produce a slew angle, combining the slew and trajectory, and dividing the combined interception area by the firing area. The firing and interception areas are calculated using spherical projection.

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: Disclosed embodiments, as well as features and aspects thereof, are directed towards providing a system, device and method for calculating comprehensive ballistic solutions, or portions thereof, via a varying magnification optical range determining and ballistic trajectory calculating apparatus referred to as a ballistic solutions device. Advantageously, embodiments of a ballistic solutions device may drastically reduce marksman error in milling targets by employing a measurement component configured to measure angular movement of a projectile launching device, such as a rifle, thus delivering consistently accurate distance to target estimations. Additionally, embodiments of a ballistic solutions device may also comprise features and aspects that enable a user to leverage available real-time field data such that error associated with the measurement of those variables is minimized prior to calculating and rendering a comprehensive ballistic solution derived from stored DOPE.

Abstract: The multi-target tracking and discrimination system (MOST) fuses with and augments existing BMDS sensor systems. Integrated devices include early warning radars, X-band radars, Lidar, DSP, and MOST which coordinates all the data received from all sources through a command center and deploys the GBI for successful interception of an object detected anywhere in space, for example, warheads. The MOST system integrates the optics for rapid detection and with the optical sensor array delivers high-speed, high accuracy positional information to radar systems and also identifies decoys. MOST incorporates space situational awareness, aero-optics, adaptive optics, and Lidar technologies. The components include telescopes or other optical systems, focal plane arrays including high-speed wavefront sensors or other focal plane detector arrays, wavefront sensor technology developed to mitigate aero-optic effects, distributed network of optical sensors, high-accuracy positional metrics, data fusion, and tracking mounts.

Abstract: An indirect artillery fire control system is shown, in which a plurality of indirect artillery systems are linked with a fire direction system such that a call for fire order is communicated as a fire command to a selected indirect artillery system, with that system being selected by reason of a characteristic of that indirect artillery system.

Abstract: A ballistics fire control system for a spin or fin stabilised projectile is provided with means which are operated such that the closest point of approach between a fired projectile and a target is taken to be at the instant the projectile velocity vector (6) is orthogonal to the position error vector (13) between the projectile and target in accordance with the relationship: Vp·(PP−PF)=0 where Vp is the projectile velocity vector, PP is the projectile trajectory or position vector, PF is the target future position vector, · is the vector dot product and (PP−PF) is the position error vector.

Abstract: In a device and method for predicting a future muzzle velocity of an indirect fire weapon 3, 7 means 9, 11 responsive to a measurement of muzzle velocity are adapted to implement an adaptive empirical prediction method to predict the future muzzle velocity. The invention also relates to an aiming system and method for an indirect-fire weapon 3, 7. The system comprises a muzzle velocity measuring device 5, and predictor means 9, 11 responsive to an output of the muzzle velocity measuring device 5 for determining a new elevation setting from the weapon. Preferably, the predictor means utilizes an adaptive empirical prediction method such as a Kalman Filter or neural network.

Abstract: A computerized instrument for displacing the aiming mark of a rifle or other small arm to compensate for ballistic trajectory, comprising a digital microcomputer, a triangulation rangefinder range data inputting system, a system for inputting data for a plurality of small arms ammo (9), other data inputting systems, an appropriate program including a small arms ballistic trajectory program, and an electric aiming mark displacement system with an aiming mark displacement data outputting receiver for acquiring cordless data transmission from a physically separate aiming mark displacement data outputting transmitter. The transmitter is physically integrated with a device comprising all subsystems of the instrument other than the cordless transmission slaved electric aiming mark displacement system with cordless transmission receiver. The small arms aiming mark displacement system and receiver may be in a telescopic sight or in an adjustable telescopic sight mount.