A firearm stabilization device is described that can be attached to a firearm to improve, increase, or maintain the stability of a firearm. The firearm stabilization device may include an electric motor configured to rotate a flywheel about an axis of rotation and a power source powering the electric motor. The electric motor, the flywheel, and the power source may be positioned within a housing. The fire arm stabilization device may include an engagement structure positioned on an outer surface of the housing for attaching (releasably or permanently) the firearm stabilization device to a firearm.

The present invention relates to a rocket launching module comprising a base frame (1) comprising at least one rail (2a); a sliding table (3) configured to slide substantially vertically on said rail (2a) when driven by at least one electric linear actuator (11), and a targeting device (4) comprising a turntable (5) on which a pivotable body (6) is mounted, supporting a rocket support portion (7). The sliding table (3) comprises a platform (8) configured to receive the turntable (5) of the targeting device (4).

The present invention relates to a rocket launching module comprising a base frame (1) comprising at least one rail (2a); a sliding table (3) configured to slide substantially vertically on said rail (2a) when driven by at least one electric linear actuator (11), and a targeting device (4) comprising a turntable (5) on which a pivotable body (6) is mounted, supporting a rocket support portion (7). The sliding table (3) comprises a platform (8) configured to receive the turntable (5) of the targeting device (4).

An attachment mechanism is provided for connecting a trunnion shaft to a pivoting platform. The mechanism includes a bracket, a block, a polygonal terminus attached to the trunnion shaft, a pair of bolts and fasteners. The bracket has a center recess and flanking surfaces parallel to the pivoting platform. The block has a cutout notch. The polygonal terminus inserts into a gap formed between the recess and the notch. The pair of bolts extends through the bracket and the terminus, and inserts into the block. The plurality of fasteners attaches the bracket at the facing surfaces to the pivoting platform.

An attachment mechanism is provided for connecting a trunnion shaft to a pivoting platform. The mechanism includes a bracket, a block, a polygonal terminus attached to the trunnion shaft, a pair of bolts and fasteners. The bracket has a center recess and flanking surfaces parallel to the pivoting platform. The block has a cutout notch. The polygonal terminus inserts into a gap formed between the recess and the notch. The pair of bolts extends through the bracket and the terminus, and inserts into the block. The plurality of fasteners attaches the bracket at the facing surfaces to the pivoting platform.

The present invention relates to a rocket launching module comprising a base frame (1) comprising at least one rail (2a); a sliding table (3) configured to slide substantially vertically on said rail (2a) when driven by at least one electric linear actuator (11), and a targeting device (4) comprising a turntable (5) on which a pivotable body (6) is mounted, supporting a rocket support portion (7). The sliding table (3) comprises a platform (8) configured to receive the turntable (5) of the targeting device (4).

The present invention relates to a rocket launching module comprising a base frame (1) comprising at least one rail (2a); a sliding table (3) configured to slide substantially vertically on said rail (2a) when driven by at least one electric linear actuator (11), and a targeting device (4) comprising a turntable (5) on which a pivotable body (6) is mounted, supporting a rocket support portion (7). The sliding table (3) comprises a platform (8) configured to receive the turntable (5) of the targeting device (4).

A weapon mount for controlling targeting of a weapon includes a base, an arm that extends from the base, and an attachment component that is rotatably coupled with the arm. The base is attachable to a platform and is rotatable to control a yaw of the weapon relative to the platform. The attachment component is configured to couple with the weapon and is rotatable to control a pitch of the weapon relative to the platform. The arm is positioned relative to the base so that a recoil vector of the weapon is within 0.5 inches radially of an axis of rotation of the base.

An automated weapons system is comprised of a plurality of weapon subsystems each comprising at least one human transported weapon subsystem. Each of the plurality of weapon subsystems is comprises a barrel, a targeting subsystem, a computational subsystem, positioning means, and a firing subsystem. The barrel is utilized for propelling a munition from each of the plurality of weapon subsystems aimed towards an area of sighting. The targeting subsystem identifies a chosen target for each of said plurality of weapon subsystems in the area of sighting. The computational subsystem, responsive to the targeting subsystem, determines where the chosen target is for each weapon subsystem (out of plurality) and where the respective barrel needs to be aimed for each weapon subsystem (out of plurality) so that the munitions will strike the chosen target. The positioning means adjusts the aim of the munitions for each weapon subsystem, responsive to the computational subsystem, out of plurality of weapons subsystems. The firing subsystem, fires the munitions from at least one to each of said plurality of weapon subsystems at the chosen target for one of the weapons subsystems, responsive to the positioning means from at least one of the plurality of the weapons subsystems.

Techniques are disclosed for systems and methods for nested gimbal assemblies. A gimbal system may include a base, a yoke, and a gimbal assembly rotatably connecting the yoke to the base. The gimbal assembly may include a motor, a bearing, and a ferrofluid seal. The motor may be configured to rotate the yoke relative to the base about a rotational axis. The bearing may be seated within the base and permit rotation of the yoke relative to the base about the rotational axis. The ferrofluid seal may be positioned to seal an interface between the yoke and the base. The motor may be positioned within an inner diameter of the bearing. The bearing may be positioned within an inner diameter of the ferrofluid seal.