Abstract: A weapon safety system with a target and a weapon with an automated lock. Each target is associated with an emitter which transmits a clearance signal that encodes an identifier. The encoded identifier may release the automated lock when received by a receiver attached to the weapon. In order to restrict the positions and orientations from which the weapon can fire to those surrounding the desired targets, shooting is enabled and the automated lock is released, when the following conditions are met: the clearance signal is received by the receiver, so that the receiver is within a first enablement area generated by a first aperture in the emitter; a measured optical power is above a predefined threshold; and the encoded identifier is validated.

Abstract: The present invention provides an unmanned aerial vehicle with non-lethal neuromuscular incapacitation system comprising a body, a plurality of rotary assemblies secured to the body and configured to provide lift, a control system disposed within the body, and a telescoping stinger assembly mounted on the body. The telescoping stinger assembly comprises an elongated projectile having a barb at a first end thereof, a wire having a first end attached to a second end of the elongated projectile, a high voltage pulse power supply attached to a second end of the wire, and firing mechanism for launching the projectile from the telescoping stinger assembly toward a target. A protective cage may be attached to and surround the body of the UAV.

Abstract: Firing direction limitation device (15) for controlling the allowed launch angle range of a directable firing device (10) tiltable between at least two allowed maximum launch angles (MaxLA1, MaxLA2) defining a launch sector (4), wherein the firing direction limitation device (15) comprises a moveable limiting structure (16) configured to be arranged in connection to the directable firing device (10), where the limiting structure (16) is configured to be moveable between a first position (P1) and a second position (P2), wherein, when the limiting structure (16) is set in the first positon (P1), the directable firing device (10) is moveable within a first launch angle range (LARa1), and when the limiting structure (16) is set in the second positon (P2), the directable firing device (10) is moveable within a second launch angle range (LARa2), wherein the second launch angle range (LARa2) is limited in relation to the first launch angle range (LARa1), whereby the allowed launch angle of the directable firing devi

Abstract: Apparatus and associated methods relate to a toollessly interchangeable ring gear drive mount system for a rotatable turret including a ring gear, a ring gear drive module, a mount bracket, a pair of receiver members, and a pair of mount flanges. In an exemplary aspect, the mount bracket may extend in a plane perpendicular to an axis of rotation of the ring gear and be adapted for mounting to a platform arranged in a rotatable relationship to the ring gear. The pair of receiver members may extend from the mount bracket and define a pair of slide channels positioned substantially vertically and oriented substantially parallel to the axis of rotation. The pair of mount flanges may each be sized and shaped to be slidably inserted into a corresponding one of the pair of slide channels and adapted to support the ring gear drive module.

Abstract: The technology disclosed herein can include a motor unit having a motor with a motor gear to rotate a drive shaft and a drive gear. A manual input shaft can also be configured to transmit rotation to the drive shaft. The motor can have a central axis that forms an angle of less than 90 degrees with a plane substantially defined by an outer surface of a gear box coupled to the motor. A mounting bracket is configured to allow mechanical communication between the motor unit and an internal ring gear. The internal ring gear can be mounted to a vehicle and a turret can be pivotably disposed within the internal ring gear. A motor unit is mounted on the turret and a drive gear is rotatably mounted on the motor unit and in direct engagement with the internal ring gear.

Abstract: A remote weapon station (10) includes a firearm (12), which is able to fire ammunitions against a target. A remote control board or panel (14) is arranged at a distance from the firearm (12) and is configured to be activated by an operator, so as to control the firearm (12). An automatic target aiming system (32) is configured to provide the remote control board (14) with target aiming signals, which indicate the position of a target that has to be hit by the firearm (12). The remote control board (14) is assembled on a platform (18) which is adapted to be fitted to an aircraft. A support element (28) mounts on the platform (18) and supports the automatic target aiming system (32) and houses the adjustable firearm (12) in a controlled way by the remote control board (14) as a function of the target aiming signals.

Abstract: A firearm mount including a base that supports a movable cradle within which is positioned a firearm. Remotely controlled motors turn the cradle about horizontal and vertical axes. Remote operation of the motors is enhanced by a video camera secured to the firearm and connected to a transmitter that broadcasts an electronic video signal to the user stationed away from the mount. The trigger of the firearm in the cradle is moved to fire by a remotely controlled solenoid.

Abstract: A firearm mount including a base that supports a movable cradle within which is positioned a firearm. Remotely controlled motors turn the cradle about horizontal and vertical axes. Remote operation of the motors is enhanced by a video camera secured to the firearm and connected to a transmitter that broadcasts an electronic video signal to the user stationed away from the mount. The trigger of the firearm in the cradle is moved to fire by a remotely controlled solenoid.