Abstract: The disclosed technology is a vehicle object detection radar system incorporating an inertial measurement unit (IMU). The IMU may obtain input signals of, or relating to, for example, relative motion, acceleration, object detection angle, sway and vibration of the vehicle and/or any towed trailer, and process them for relay to the vehicle operator as operating information and possibly alarms. Also, the obtained IMU signals may be relayed directly to the vehicle's object detection radar systems and central control for automatic adjustment and control thereof.

Abstract: An illuminated reflex optical sighting system integrated directly into a firearm includes a lighting module comprising an illumination source mounted to a body of the firearm at a discrete first mounting location, an optical lens assembly mounted to the body of the firearm at a discrete second location spatially distanced from the first location, and a power source operably coupled to the illumination source. The illumination source is configured and operable to project a reticle onto a lens of the lens assembly for use in aiming the firearm. The illumination source and lens assembly are separately mounted to and independently removable from the body of the firearm thereby providing a low profile sighting system which substantially retains the aspects of the original firearm. The illumination source, power source, and lighting control circuitry may be housed inside the metal rear sight of the firearm in one embodiment.

Abstract: An inertial measurement unit (IMU) may be used to align a plurality of radar units coupled to a vehicle via a plurality of mounting structures. The IMU may be placed at a reference location and reference-location data may be captured. The IMU may be coupled to each of the mounting structures and, at each mounting structure, respective mounting-location inertial measurement data may be captured using the IMU. For each mounting structure, a measured roll angle, measured elevational angle, and measured azimuthal angle is determined based on at least the mounting-location inertial measurement obtained at the mounting structure and the reference inertial measurement. Further, for each mounting structure, offsets are determined for the measured roll angle, the measured elevational angle, and the measured azimuthal angle. One or more of the mounting structures and/or radar units are adjusted based on one or more of the offsets.

Abstract: The present disclosure relates to a method and system for providing and enhanced navigation solution of a device within a platform (such as for example person, vehicle, or vessel of any type), wherein the device is within the platform and may be strapped or non-strapped to the platform, wherein in case of non-strapped the mobility of the device may be constrained or unconstrained within the platform, wherein the enhancement of the navigation solution is through multiple sensor assemblies, wherein the multiple sensors assemblies are not necessarily all on the device, and wherein the multiple sensors assemblies are within the platform. This method works for a navigation solution utilizing measurements from sensors (such as for example, accelerometers, gyroscopes, magnetometers etc.) whether in the presence or in the absence of absolute navigational information (such as, for example, GNSS or WiFi positioning).

Abstract: An inertial measurement unit (IMU) may be used to align a plurality of radar units coupled to a vehicle via a plurality of mounting structures. The IMU may be placed at a reference location and reference-location data may be captured. The IMU may be coupled to each of the mounting structures and, at each mounting structure, respective mounting-location inertial measurement data may be captured using the IMU. For each mounting structure, a measured roll angle, measured elevational angle, and measured azimuthal angle is determined based on at least the mounting-location inertial measurement obtained at the mounting structure and the reference inertial measurement. Further, for each mounting structure, offsets are determined for the measured roll angle, the measured elevational angle, and the measured azimuthal angle. One or more of the mounting structures and/or radar units are adjusted based on one or more of the offsets.

Abstract: A system and method for aiming and alignment of a shell firing weapon includes a portable aiming unit that may be located in close proximity to the weapon that includes a reference head for emitting and/or receiving at least one energy ray. The portable aiming unit can be aligned to a reference azimuth, either absolute or relative. A sighting unit is also included in the system and removably mounted to the weapon. The sighting unit includes a reference head that is complementary to the reference head of the portable aiming unit. The at least one energy ray established between the portable aiming unit and the sighting unit provides an accurate relative reference of directing the weapons fire and monitoring linear and angular displacement of the weapon as it is fired so that corrections can be made in aiming the weapon in response thereto.

Abstract: Multiple independently gimbaled devices, such as an electro-optical sensor and machine gun, are mounted to a rotating platform on a vehicle. The platform can rotate to prevent one device from blocking the other while aiming at an off-board location. A control system can harmonize the rotation of the device gimbals and rotating platform so that they remain pointed at the same location. The platform can be rotated to place a firing weapon downwind of a sensor or otherwise compensate for effects of one on the other.

Abstract: A rifle scope includes an image sensor configured to capture visual data corresponding to a view area, a display, and a controller coupled to the display and the image sensor. The controller is configured to apply a first stabilization parameter to at least a portion of the visual data to produce a stabilized view, to provide the stabilized view and a reticle to the display, and to apply a second stabilization parameter to stabilize the reticle relative to the stabilized view in response to motion.

Abstract: A photoluminescent capsule illuminator for a sighting device. The photoluminescent illuminator includes an elongated phosphor housing having sidewalls and a base. The photoluminescent illuminator includes phosphors in a granular form disposed inside the phosphor housing. The photoluminescent illuminator includes a cap sealing the phosphors in the phosphor housing. The phosphor housing is disposed in relation to a body of the sighting device such that photoluminescent light emitted from the phosphors exits the phosphor housing and identifies a location of a sight on the sighting device.

Abstract: A dot-sighting device includes a light source, a beam splitter and a reflective element. The light source emits light. The beam splitter includes a surface that reflects at least a portion of a first light component of the light and transmits at least a portion of a second light component. The reflective element reflects at least a portion of the first light component reflected by the surface of the beam splitter toward the beam splitter. The light reflected by the reflective element includes the second light component.

Abstract: A method for acquiring the coordinates of a trigger point of a projectile above a plot of land on which a target is located, said method being characterized in that it includes the following steps: performing a three-dimensional acquisition of the plot of land using a laser observation means, constructing by calculation, and then displaying an image of the plot of land from a bird's eye view observation direction, and recovering the coordinates of the trigger point desired for the projectile after the positioning said area on the image of the land. The invention also relates to a fire control implementing such a method.

Abstract: Multiple independently gimbaled devices, such as an electro-optical sensor and machine gun, are mounted to a rotating platform on a vehicle. The platform can rotate to prevent one device from blocking the other while aiming at an off-board location. A control system can harmonize the rotation of the device gimbals and rotating platform so that they remain pointed at the same location. The platform can be rotated to place a firing weapon downwind of a sensor or otherwise compensate for effects of one on the other.

Abstract: A dot-sighting device includes a light source, a beam splitter and a reflective element. The light source emits light. The beam splitter includes a surface that reflects at least a portion of a first light component of the light and transmits at least a portion of a second light component. The reflective element reflects at least a portion of the first light component reflected by the surface of the beam splitter toward the beam splitter. The light reflected by the reflective element includes the second light component.

Abstract: A boresight verification device (BVD) comprised of a circular housing with a rear portion of smaller diameter and a front portion of larger diameter. The front portion securely holds a level. The circular housing also contains a plurality of spring plungers which grip the inside of a muzzle when BVD is inserted into a muzzle for use. A tooling ball provides a stable reference point.

Abstract: A firearm laser sight alignment assembly includes a laser module for emitting a beam along an optical axis, the laser module having an outer seat. The alignment assembly encompasses a resilient grommet mechanically engaging the outer seat in a first adhesive free interference fit. The grommet includes an external seat sized to form adhesive free interferences fits with a laser cover and the housing, as the laser cover engages the housing to retain the grommet with respect to the housing and the laser cover. Upon operable assembly, the interference fits substantially preclude axial and longitudinal movement between the grommet and the laser module as well as the grommet and the laser cover and housing, while allowing angular movement of the laser module to a desired alignment position.

Abstract: A light and accessory mount having a mounting bracket for attaching to a weapon mount, the mounting bracket having a proximal side and a distal side, the proximal side of the mounting bracket having one or more mounting holes for connecting the mounting bracket to the weapon mount with mounting fasteners and one or more lugs to engage bosses on the weapon mount; the distal side of the mounting bracket having one or more attachment holes and one of more bosses for attaching a channel assembly to the mounting bracket; the channel assembly including a proximal end and a distal end, the proximal end having one or more attachment points for attaching the channel assembly to the mounting bracket with one or more attachment fasteners and one or more lugs to engage bosses on the distal end of the mounting bracket; and the distal end of the channel assembly having one or more rails for attaching devices.

Abstract: The systems and methods described herein provide military personnel with a swift and accurate means to return fire at a detected shooter. In particular, the systems and methods described herein relate to an indicator for a weapon sight. In some embodiments, the indicator is electromechanical. In some embodiments, the indicator is configured to be moveable such that when the weapon sight is aligned with the indicator, the weapon points in the direction of the detected shooter. In some embodiments, the indicator is attached to the weapon itself, while in other embodiments, the indicator is attached to the weapon mount. The weapon may be located on a ground vehicle, aircraft, or may be portable. In some embodiments, the system includes a processor configured to receive a shooter's location, determine the position of the indicator based on the received shooter location, and control the indicator to move into the determined position.

Abstract: A weapon system comprises a first, second and third sensor and a range detecting means. The weapon system further comprises a weapons platform removably mounted to a moveable vehicle. The weapons platform includes a gun. The first sensor is mechanically attached to the gun for sensing an image. The second sensor senses a position of the gun, including at least an elevation and azimuth. The third sensor detects a rate and altitude of the moveable vehicle. The range detecting means detects a range of the gun to the target. The weapon system also comprises an image processor for processing the image from the first sensor, a display for displaying the processed image and a controller. The controller calculates an expected impact point for a round of fire based upon the sensed and detected data, and superimposes the expected impact point on the processed image on the display.

Abstract: The systems and methods described herein provide military personnel with a swift and accurate means to return fire at a detected shooter. In particular, the systems and methods described herein relate to an indicator for a weapon sight. In some embodiments, the indicator is electromechanical. In some embodiments, the indicator is configured to be moveable such that when the weapon sight is aligned with the indicator, the weapon points in the direction of the detected shooter. In some embodiments, the indicator is attached to the weapon itself, while in other embodiments, the indicator is attached to the weapon mount. The weapon may be located on a ground vehicle, aircraft, or may be portable. In some embodiments, the system includes a processor configured to receive a shooter's location, determine the position of the indicator based on the received shooter location, and control the indicator to move into the determined position.

Abstract: A method and system for improving precision and accuracy of weaponry according to which angular position information of the fire control device and optical location information of the optical signals emitted during the flight of a projectile are processed in a computer using software to calculate and provide a precise aim point for firing one or more subsequent projectiles.

Abstract: Disclosed are a sighting apparatus for a remote-control shooting system and a sighting alignment method using the same. The sighting apparatus for a remote-control shooting system including a firearm installed in a firearm platform rotatable in up, down, left and right directions, and an observation camera installed to be position-adjustable in at the firearm platform, the sighting apparatus includes: a sighting unit which is fastened to the firearm with a zeroing unit precisely up, down, left and right adjustable therebetween, and takes a first image as zeroed; and a controller which controls the firearm platform so that an sighting indicator (e.g., a line) of the first image taken by the sighting unit can be aligned with a target, and aims at the target.

Abstract: A ballistic vehicle-immobilization apparatus includes an optical module adapted to provide visual feedback to a user to aim at an object. The ballistic vehicle-immobilization apparatus further includes a firing mechanism adapted to fire a projectile towards the object and a housing containing the firing mechanism. The ballistic vehicle-immobilization apparatus is adapted to be mounted to a vehicle.

Abstract: A system and method for use of an enhanced aiming system which includes a marker displayed at a first position in an aiming scope, a user input of a start position and an ending position to measure a desired impact zone, a calculator for determining a range to the target based on the known dimension of the impact zone and the magnification value of the aiming scope, and a display in the aiming scope for showing an aiming point dot or bar to compensate for projectile drop at the calculated range, and optionally for windage and optionally for moving target hold-over.

Abstract: An improved telescopic gun sight includes a telescopic gun sight at least including an adjustable lens configuration for adjustably magnifying an external object to form an object image, an inverting tube for inverting the object image, an ocular lens array for presenting the object image for viewing, a primary reticule including sighting insignia imprinted thereon and a secondary reticule being movable both horizontally and vertically in the image plane. The secondary reticule includes a generally horizontal windage correction scale operative to provide instant windage correction target alignment. It includes instant windage correction target alignment values positioned at point-specific spaced-apart locations with specific instant windage correction target alignment values corresponding to selected distance amounts calculated for a selected bullet type and weight.

Abstract: An apparatus for measuring the azimuth of a tube having a bore axis includes a centering mandrel having a longitudinal axis; a flexible member for defining a bore axis projection of the bore axis; a tensioner fixed to one end of the flexible member, and a pair of adjusters connected to the tensioner, the adjusters for moving the tensioner along a respective pair of axes that are perpendicular to the bore axis projection, the axes of the adjusters being mutually perpendicular.

Abstract: The invention relates to an actuating element for setting the aim mark of a telescopic sight. According to the invention, the actuating element is rotatably located on the telescopic sight in the form of a rotary knob and the aim mark is displaced in a vertical and/or horizontal direction by means of a mechanical actuator, when the rotary knob is turned. In addition, the rotational area of the rotary knob is restricted in both rotational directions by at least one working region stop. The rotary knob is detachably coupled to the mechanical actuator. The working region stop(s) can be deactivated, allowing the rotary knob to be turned beyond the working region stop in both directions. The actuating element can be switched between at least three different modes. In mode A, the rotary knob is coupled to the mechanical actuator and the working region stop is inactive.

Abstract: The invention relates to an operating element for adjusting the cross-hairs of a telescopic sight. The operating element is in the form of a rotating knob, arranged to rotate on the telescopic sight, whereby a rotation of the rotating knob adjusts the cross-hairs by means of an adjuster mechanism. The rotating knob comprises one or several index marks, by means of which one or more positions of the cross-hairs may be indexed. The one or several index element(s) is/are arranged in one or several recess(es) and may be displaced therein in the circumferential direction of the rotating knob. The index elements are furthermore coupled to the rotating knob in the recesses such as to be rotated with the rotating knob on a rotation of the same.

Abstract: Boresighting systems and methods are disclosed. In one embodiment, an assembly adapted for boresighting a launch system includes first and second elongated members adapted to be coupled to the launch system. First and second alignment members are coupled to and extend between the first and second elongated members and are adapted to position the elongated members in a substantially aligned, spaced-apart relationship. A mirror assembly is coupled to each elongated member, the mirror assemblies being adapted to provide an average angular position resulting in a single corrector value for the launch system. In a particular embodiment, each of the first and second elongated members is sized to simulate a Stinger missile.

Abstract: An improved aiming tube pivot assembly for use in a sighting and/or aiming apparatus which comprises an aiming tube axially mounted within an outer tube (or housing). A support ring supports the aiming tube within the outer tube in a gimbal-like arrangement by means of ball bearings and set screws. The ball bearings are secured intermediate the aiming tube and the support ring via apertures in the outer tube. The set screws are threadedly mounted in the support ring and engage the outer surface of the outer tube. A movable cover tube can be mounted on the outer tube and substantially encloses the end of the outer tube and the support ring.

Abstract: This invention concerns a device for a weapon sight. The device includes a deflecting element (15) disposed in an optical path through the sight and comprising an optical wedge (17), and means (16) arranged to control the positional setting of the optical wedge to produce a randomly altered sight image in the sight. The device is characterized in that the control means (16) are arranged to produce, before firing, the altered sight image and, during firing, to guide the wedge or wedges to a reference position in which the sight image is unaltered. The invention also concerns a method for optically simulating recoil in a weapon with a sight.

Abstract: A method for aiming a weapon barrel [B], wherein a target image [Z*] and a target marker [X] are displayed with the aid of an image visualization unit M. The rough aiming of the weapon barrel [B] is performed in a first phase, in a second phase, with the weapon barrel [B] stationary, sighting by sighting the target image [Z*] by means of the image visualization unit [V] is performed, wherein the target image [Z*] and the target marker [X] are brought into coincidence as closely as possible, and fine aiming of the weapon barrel [B] in a third phase. The device for executing the method comprises a device for setting an initial gun sight angle [?o] an image visualization unit [V], the latter displays a target image [Z*] and a target marker [X] representing the end of an imaginary projectile trajectory [p].

Abstract: A combat tank is converted into an artillery observation tank without requiring removal of the main gun. The combat tank is converted by integrating retrofitted equipment necessary for the artillery observation, especially the navigation system (12), into the vehicle turret (4) such that it does not collide with the main gun. The navigation system (12) is installed with an arbitrary orientation at an arbitrary location in the vehicle turret (4), and adjusted at this location, without requiring a complicated adjustment mechanism for the observation system, or attachment to the elevating mass. The necessary elevation values for the line of sight (21) are obtained through the evaluation of the angular values of a mirror in the mirror head, such as of a primary-target telescope (20), or through evaluation of gun-position angles.

Abstract: The invention relates to an elevation laying system for a weapon mounted on a vehicle. It comprises first positioning means for the weapon along a wide elevation range with respect to a first axis of rotation offset with respect to the center of gravity of the weapon, and second positioning means for the weapon connected to the first means along a narrow elevation range with respect to a second axis of rotation passing through the center of gravity of the weapon. The first axis of rotation is located to the rear of the weapon's center of gravity. The first positioning means are hinged with respect to a frame onto which the weapon is mounted around the first axis of rotation.

Abstract: The invention relates to an attachment device for observation and/or scrambling or other effect means at the end of the cannon of an armored vehicle. It incorporates a rigid substantially parallelepiped body, one face of which is shaped to fit the outer wall of the barrel, and constituting a reception cage, said body being connected to the barrel by removable linking means. The observation means are constituted by a day or night-vision camera. The reception cage of the body incorporates at least three cameras. Application to armored vehicles.

Abstract: An aiming system for a trajectory weapon such as a ground launcher, machine gun, mortar, or the like. The aiming system is attached to a conventional mount for the involved weapon. Also disclosed is a method of sighting in a weapon which employs the aiming system.

Abstract: An aiming system for a trajectory weapon such as a ground launcher, machine gun, mortar, or the like. The aiming system is attached to a conventional mount for the involved weapon. Also disclosed is a method of sighting in a weapon which employs the aiming system.

Abstract: An optical sighting system includes at least one optical channel with which there is associated at least one reticle. The reticle includes at least one mark which demarcates a blind spot, which is visible to an observer using the optical sighing system and which is centered approximately about a centering point that is situated substantially at a distance which is representative of a sighting angle of between 13° and 18°, with respect to a predetermined direction of observation along a first direction. This first direction is representative on the optical sighting system of the direction passing substantially by the centers of the eyes of an observer who is using the optical sighting system.