There is provided an anti-ballistic aerospace structure, said structure comprising a strike layer defining an outwardly facing surface and an opposing capture layer defining an inwardly facing surface and an intermediate structural layer arranged between the strike layer and capture layer, wherein the intermediate structural layer is spaced relative to the strike layer to define a space between the intermediate structural layer and the strike layer, said space comprising one or more reinforcement elements, and wherein the strike layer is formed of a fiber reinforced plastic laminate comprising at least one metallic layer.

Various countermeasure expendables and methods of using said countermeasure expendables are provided herein. The countermeasure expendable includes a container. The countermeasure expendable also includes a plurality of countermeasure payloads operably engaged inside the container, wherein one countermeasure payload of the plurality of countermeasure payloads is operably connected to a first Zener diode, and wherein another countermeasure packet of the plurality of countermeasure packets is operably connected to a second Zener diode. In addition, the first Zener diode has a first Zener voltage threshold and the second Zener diode has a second Zener voltage threshold greater than the first Zener voltage threshold.

Various countermeasure expendables and methods of using said countermeasure expendables are provided herein. The countermeasure expendable includes a container. The countermeasure expendable also includes a plurality of countermeasure payloads operably engaged inside the container, wherein one countermeasure payload of the plurality of countermeasure payloads is operably connected to a first Zener diode, and wherein another countermeasure packet of the plurality of countermeasure packets is operably connected to a second Zener diode. In addition, the first Zener diode has a first Zener voltage threshold and the second Zener diode has a second Zener voltage threshold greater than the first Zener voltage threshold.

The present invention relates to an armed unmanned aerial vehicle (“UAV”), an armed UAV control system, and methods of use thereof. In one form, the armed UAV includes: an elongate body, a pair opposed side rotor arm assemblies extending from the sides of the body, a tail rotor arm assembly extending from a rear end of the body, a weapons system including at least one firearm associated with the body, and a flight and targeting controller operatively associated with the side rotor arm assemblies and the tail rotor arm assembly. The controller configured to: determine at least a pitch angle and yaw angle required to strike a target with the weapons system, based on target information received; and selectively control operation of each rotor arm assembly for aiming the weapons system, based on at least the pitch angle and the yaw angle determined.

The present invention relates to an armed unmanned aerial vehicle (“UAV”), an armed UAV control system, and methods of use thereof. In one form, the armed UAV includes: an elongate body, a pair opposed side rotor arm assemblies extending from the sides of the body, a tail rotor arm assembly extending from a rear end of the body, a weapons system including at least one firearm associated with the body, and a flight and targeting controller operatively associated with the side rotor arm assemblies and the tail rotor arm assembly. The controller configured to: determine at least a pitch angle and yaw angle required to strike a target with the weapons system, based on target information received; and selectively control operation of each rotor arm assembly for aiming the weapons system, based on at least the pitch angle and the yaw angle determined.

The system comprises a plurality of sensor systems, a counter drone, and a processor. A sensor system of the plurality of sensor systems comprises one or more sensors that are connected to a network. The counter drone is connected to the network. The processor is configured to receive an indication of a potential target from the plurality of sensor systems; generate a fused data set for the potential target, determine whether the potential target comprises the threat drone based at least in part on the fused data set; and in response to determining that the potential target comprises the threat drone, provide counter drone instructions to the counter drone.

The system comprises a plurality of sensor systems, a counter drone, and a processor. A sensor system of the plurality of sensor systems comprises one or more sensors that are connected to a network. The counter drone is connected to the network. The processor is configured to receive an indication of a potential target from the plurality of sensor systems; generate a fused data set for the potential target, determine whether the potential target comprises the threat drone based at least in part on the fused data set; and in response to determining that the potential target comprises the threat drone, provide counter drone instructions to the counter drone.

Disclosed is a device and method to load stores on an aircraft. The device may include a controller configured to: assign one or more stores to the aircraft; and control at least one actuator to: control a position of the aircraft; load the one or more stores onto one or more corresponding lift portions; position the one or more stores relative to a position of the aircraft determined in accordance with sensor information from at least one sensor; and secure the one or more stores to the aircraft.

Disclosed is a device and method to load stores on an aircraft. The device may include a controller configured to: assign one or more stores to the aircraft; and control at least one actuator to: control a position of the aircraft; load the one or more stores onto one or more corresponding lift portions; position the one or more stores relative to a position of the aircraft determined in accordance with sensor information from at least one sensor; and secure the one or more stores to the aircraft.

A driving device includes a frame, a screw-nut system comprising a threaded rod and a first nut helicoidally connected to the threaded rod, the threaded rod being connected to the frame by a pivot connection that allows the threaded rod to rotate with respect to the frame about a longitudinal axis of the threaded rod, a first position sensor making it possible to detect a limit position of the first nut along the longitudinal axis, the first position sensor comprising a first part and a second part, the first position sensor being sensitive to a variation in a distance between the first part and the second part of the first position sensor along the axis, the first part being fixed to the first nut and the second part being connected to the threaded rod without passing via the pivot connection and in such a way that rotation of the threaded rod about the longitudinal axis leads to a variation in the distance between the first part and the second part of the first position sensor along the longitudinal axis.