Systems, devices, and methods for determining a predicted impact point of a selected weapon and associated round based on stored ballistic information, provided elevation data, provided azimuth data, and provided position data.

Systems, devices, and methods for determining a predicted impact point of a selected weapon and associated round based on stored ballistic information, provided elevation data, provided azimuth data, and provided position data.

Apparatus and associated methods relate to a motor-less cartridge ring gear engagement module (CRGEM) for a turret-rotating system that includes a main drive gear configured to rotate in a rotation plane, a manual input shaft that extends substantially orthogonal relative to the rotation plane, and a drive shaft that extends substantially orthogonal relative to the rotation plane, where the drive shaft and the manual input shaft extend substantially parallel to one another. In an illustrative example, both the main drive gear and a hand crank may be located on a top surface of the CRGEM. In some embodiments, a manual drive cap may be hingedly coupled to the gearbox and configured to rotate in a vertical plane that is substantially orthogonal to the rotation plane. At least some examples may provide for a hand-operated, manual traverse unit that advantageously does not require electrical power to operate.

Apparatus and associated methods relate to a motor-less cartridge ring gear engagement module (CRGEM) for a turret-rotating system that includes a main drive gear configured to rotate in a rotation plane, a manual input shaft that extends substantially orthogonal relative to the rotation plane, and a drive shaft that extends substantially orthogonal relative to the rotation plane, where the drive shaft and the manual input shaft extend substantially parallel to one another. In an illustrative example, both the main drive gear and a hand crank may be located on a top surface of the CRGEM. In some embodiments, a manual drive cap may be hingedly coupled to the gearbox and configured to rotate in a vertical plane that is substantially orthogonal to the rotation plane. At least some examples may provide for a hand-operated, manual traverse unit that advantageously does not require electrical power to operate.

Provided is an apparatus for controlling a striking device. The apparatus for controlling the striking device equipped with a weapon to strike a target includes: a display unit which displays an image captured by a camera mounted on the striking device; a control unit which controls firing of the weapon; and a manipulation unit which transmits a fire signal to the control unit, wherein the control unit calculates the number of rounds of ammunition left in the striking device, calculates an accuracy rate which is a probability that the striking device will hit the target, and determines whether the target can be neutralized by considering the calculated number of rounds of ammunition left and the calculated accuracy rate for the target.

Provided is an apparatus for controlling a striking device. The apparatus for controlling the striking device equipped with a weapon to strike a target includes: a display unit which displays an image captured by a camera mounted on the striking device; a control unit which controls firing of the weapon; and a manipulation unit which transmits a fire signal to the control unit, wherein the control unit calculates the number of rounds of ammunition left in the striking device, calculates an accuracy rate which is a probability that the striking device will hit the target, and determines whether the target can be neutralized by considering the calculated number of rounds of ammunition left and the calculated accuracy rate for the target.

A controllable firing pattern firearm system is described herein. The controllable firing pattern firearm system includes a firearm, one or more actuators for adjusting at least one of a position and orientation of the firearm, and a controller controlling the actuators to produce a designated firing pattern on a target as the firearm is fired. The controller receives several user inputs to generate the commands for the actuators to produce the designated firing pattern, where the designated firing pattern may be a spiral firing pattern. The user provides input through a control panel having several control input mechanisms. The user inputs include a firing pattern size or target diameter, projectile firing density, and a distance of a target from the firearm, among other inputs. A method is also described herein for firing a spiral firing pattern on a target with the controllable firing pattern firearm system.

A method and apparatus for generating, in an aircraft in flight, a feasibility display indicative of the feasibility of a weapon, the method comprising: providing a performance envelope for the weapon; determining, using the performance envelope, configuration data for configuring a generic algorithm; uploading the configuration data to the aircraft; generating feasibility data indicative of the feasibility of a weapon carried on the aircraft successfully engaging a target and/or the feasibility of a weapon carried on the target successfully engaging the aircraft; determining, on board the aircraft, using the same generic algorithm and the uploaded configuration data, one or more test criteria; performing, on board the aircraft, an assessment process including determining whether or not the feasibility data satisfies the one or more test criteria; and, based the assessment, using the feasibility data, generating the feasibility display.

A method and apparatus for generating, in an aircraft in flight, a feasibility display indicative of the feasibility of a weapon, the method comprising: providing a performance envelope for the weapon; determining, using the performance envelope, configuration data for configuring a generic algorithm; uploading the configuration data to the aircraft; generating feasibility data indicative of the feasibility of a weapon carried on the aircraft successfully engaging a target and/or the feasibility of a weapon carried on the target successfully engaging the aircraft; determining, on board the aircraft, using the same generic algorithm and the uploaded configuration data, one or more test criteria; performing, on board the aircraft, an assessment process including determining whether or not the feasibility data satisfies the one or more test criteria; and, based the assessment, using the feasibility data, generating the feasibility display.

Systems, devices, and methods for determining a predicted impact point of a selected weapon and associated round based on stored ballistic information, provided elevation data, provided azimuth data, and provided position data.