The present disclosure describes methods and systems for measuring crosswind speed by optical measurement of laser scintillation. One method includes projecting radiation into a medium, receiving, over time, with a photodetector receiver, a plurality of scintillation patterns of scattered radiation, comparing cumulative a radiation intensity for each received scintillation pattern of the received plurality of scintillation patterns, and measuring a cumulative weighted average cross-movement within the medium using the compared cumulative radiation intensities.

A device that causes a weapon to fire upon a target when the weapon is enabled by an operator, and when the weapon point of impact passes through a target or in a proximity thereto and when the target satisfies certain criteria as determined by one or more sensors/designations. This invention represents a significant paradigm shift. Some prior art (large scale) weapons automatically acquire/track/prioritize/target/fire upon targets without operator intervention (i.e. Phalanx). Most prior art weapons, especially but not limited to small arms, are manually aimed, and fire immediately upon an input (trigger pull, or equivalent) from the operator. The current invention is a novel approach which triggers the release of a round, multi-round burst, rocket, missile, or other projectile(s) when enabled by the operator, and when the target passes through the point of impact (or desired/computed proximity thereto), relieving the operator of the split second judgment in timing the release and/or cessation of such fire. The results intended include a reduction in off-target rounds fired, increased hit rate, conservation of ammunition, more effective targeting for non-motion-stabilized weapons (in particular small/medium arms), and the introduction of a backup mode for nominally motion-stabilized weapons which may allow effective operations when primary stabilization systems fail or are overwhelmed by dynamics. This invention is applicable (in embodiments of varying complexity) to weapons ranging from handheld pistols to the main (artillery) gun of a tank, a ship, or the cannon aboard an aircraft.

A device that causes a weapon to fire upon a target when the weapon is enabled by an operator, and when the weapon point of impact passes through a target or in a proximity thereto and when the target satisfies certain criteria as determined by one or more sensors/designations. This invention represents a significant paradigm shift. Some prior art (large scale) weapons automatically acquire/track/prioritize/target/fire upon targets without operator intervention (i.e. Phalanx). Most prior art weapons, especially but not limited to small arms, are manually aimed, and fire immediately upon an input (trigger pull, or equivalent) from the operator. The current invention is a novel approach which triggers the release of a round, multi-round burst, rocket, missile, or other projectile(s) when enabled by the operator, and when the target passes through the point of impact (or desired/computed proximity thereto), relieving the operator of the split second judgment in timing the release and/or cessation of such fire. The results intended include a reduction in off-target rounds fired, increased hit rate, conservation of ammunition, more effective targeting for non-motion-stabilized weapons (in particular small/medium arms), and the introduction of a backup mode for nominally motion-stabilized weapons which may allow effective operations when primary stabilization systems fail or are overwhelmed by dynamics. This invention is applicable (in embodiments of varying complexity) to weapons ranging from handheld pistols to the main (artillery) gun of a tank, a ship, or the cannon aboard an aircraft.

The disclosure relates to a viewing optic. In one embodiment, the disclosure relates to a viewing optic having an integrated display system. In one embodiment, the disclosure relates to a viewing optic having an integrated display system for generating images that are projected into the first focal plane of an optical system.

Systems and methods of calculating a ballistic solution for a projectile are provided. A ballistic system may include an airborne device, a ballistic computer, a data interface, and a flight module, or any combination thereof. The airborne device (e.g., a drone) may be operable to gather wind data along or adjacent to a flight path of a projectile to a target. The ballistic computer may be in data communication with the airborne device to receive the wind data. The ballistic computer may be configured to calculate a ballistic solution for the projectile based on the wind data. The data interface may be in data communication with the ballistic computer to output the ballistic solution to a user. The flight module may be configured to calibrate a flight path of the airborne device.

The present disclosure relates to a shooting device, sighting apparatus, imaging rangefinder and adjusting method thereof. The imaging rangefinder capable of being adjustably mount on a sighting telescope, comprising a power supply, a control module electrically connected to the power supply, an imaging module electrically connected to the control module, a ranging imaging module electrically connected to the control module, and a display module electrically connected to the control module, and an eyepiece system showing an image shown by the display module, wherein an image from the sighting telescope is transmitted to the control module via the imaging module, the image shown by the display module comprises the image from the sighting telescope, an image from the ranging imaging module, and ranging information and ranging aiming point from the ranging imaging module.

The present disclosure relates to a shooting device, sighting apparatus, imaging rangefinder and adjusting method thereof. The imaging rangefinder capable of being adjustably mount on a sighting telescope, comprising a power supply, a control module electrically connected to the power supply, an imaging module electrically connected to the control module, a ranging imaging module electrically connected to the control module, and a display module electrically connected to the control module, and an eyepiece system showing an image shown by the display module, wherein an image from the sighting telescope is transmitted to the control module via the imaging module, the image shown by the display module comprises the image from the sighting telescope, an image from the ranging imaging module, and ranging information and ranging aiming point from the ranging imaging module.

A rifle includes a magazine well, a barrel detachably coupled to the magazine well, and a suppressor detachably coupled to the barrel. The barrel includes a forward barrel portion on an end of the barrel opposite the magazine well. The forward barrel portion includes a muzzle locking mechanism. The suppressor is configured to be retractable.

The application relates to a target acquisition system according to one embodiment for an indirect-fire weapon. The system includes a terminal device, a sensor unit for the terminal device, an unmanned aircraft and a control device for the aircraft. The terminal device is adapted to receive, from the control device-controlled aircraft, location data (LD, PW, DT, LT) related to a target's location (LT). The sensor unit is adapted to monitor the weapon's position. The terminal device is adapted to present, with a user interface unit, the target's location on the basis of the received location data and a calculated hit point (LH) for the weapon's projectile on the basis of the weapon's position. The terminal device is adapted to indicate, with the user interface unit, when the weapon has been aimed in such a way that, on the basis of its position, the projectile's calculated hit point is in alignment with the target's location, whereby, when the weapon is discharged, its projectile strikes the designated target

The present disclosure describes a single aperture laser range finder (SALRF). In an implementation, the single aperture laser range finder includes a beam extender including an aperture and an input aperture lens. A matching lens collimates light emitted from an emitter element associated with a single aperture optical circulator and received by the beam extender, respectively. A single aperture optical circulator has an emitter channel associated with the emitter element and a detector channel associated with a detector element. The emitter channel and the detector channel merge together at an input/output aperture. A light gating mechanism is configured to permit received light to enter the detector channel and to prevent the received light from entering the emitter channel. The SALRF has an electronics end cap.