Patent classifications
B64U2101/15
Autonomous and Automated Human Transported Weapon System with External Drone Subsystem
An automated weapons system is comprised of a human transported weapon having munitions for firing and a computational subsystem, responsive to a targeting subsystem for determining where the chosen target is located, positioning means, adjusting the aim when firing the munitions responsive to the computational subsystem; and, a firing subsystem. An external drone subsystem comprises a drone with a sensing subsystem that communicates to the targeting subsystem, the external drone subsystem located remotely to the human transported weapon subsystem and provides communications between the external drone subsystem and the human transported weapon subsystem. The targeting subsystem selects a chosen target from available targets. The computational subsystem is responsive to the targeting subsystem for determining where the chosen target is located, and then determines where to aim so that the munitions will strike the chosen target. Positioning means, adjusts the aim when firing the munitions responsive to the computational subsystem. A firing subsystem fires the munitions at the chosen target responsive to the positioning means.
Autonomous and Automatic Weapon Subsystem for Drones
A weapons system is comprised of a a human transported weapons subsystem, and a drone weapons subsystem. The human transported weapons subsystem is comprised of a targeting subsystem providing for selection of a selected target, a computational subsystem, and a communications subsystem. The drone weapons subsystem has munitions with positioning and firing capability thereupon, and has communications with the human transported weapons subsystem. The targeting subsystem utilizes communications with the drone weapons subsystem; and, the computational subsystem determines where the drone weapons subsystem is and where the selected target is and where the drone weapons subsystem needs to be located in order for the drone weapons subsystem to aim the munitions to strike the selected target. The human transported weapons subsystem communicates to the drone weapons subsystem to provide information on aim of the munitions from the drone weapons subsystem and communicates to provide activating positioning of the drone weapons subsystem and firing of the munitions from the drone weapons subsystem, responsive to the computational subsystem. The drone weapons subsystem, responsive to communications from the human transported weapons subsystem, fires the munitions from the drone weapons subsystem aimed at the selected target.
Anchored aerial countermeasures for rapid deployment and neutralizing of target aerial vehicles
A system for neutralization of a target aerial vehicle comprises one or more counter-attack unmanned aerial vehicles (UAVs) and an aerial vehicle capture countermeasure tethering the counter-attack UAV(s) to a structure or ground. The counter-attack UAV(s) are operable to capture and neutralize the target aerial vehicle with the aerial vehicle capture countermeasure (e.g., a net). The system can comprise an on-board aerial vehicle detection system, and/or an external aerial vehicle detection system each having at least one sensor configured to detect the target aerial vehicle while in flight. The counter-attack UAV(s) and the associated detection systems may be autonomously operated for detecting and neutralizing a target aerial vehicle. The aerial vehicle capture countermeasure can be moved from a stowed position to a deployed position in response to coordinated flight of the counter-attack UAV(s). Associated methods and systems are provided.
UNMANNED AERIAL VEHICLE
An unmanned aerial vehicle (UAV) adapted for transit in and deployment from a projectile casing is provided. The UAV includes a wing assembly coupled to the projectile casing and the wing assembly moveable between a closed position and a deployed position. The UAV further includes a propulsion system including at least one rotor disposed on the wing assembly to generate lift, wherein in the closed position, the wing assembly is substantially integral with the projectile casing and in the deployed position, the wing assembly is extended outwards from the projectile casing.
SYSTEM FOR NEUTRALISING A TARGET USING A DRONE AND A MISSILE
The neutralisation system (1) comprises a drone (2) configured to be able to fly close to a target and transmit at least position information concerning the position of the target, the neutralisation system (1) also comprising at least one missile (6) capable of being guided towards the target in order to neutralise it and at least one control station (8), the control station (8) comprising a receiving unit (9B) capable of receiving at least the position information transmitted by the drone (2) and a display unit (10A) capable of displaying this information to an operator, the missile (6) being configured to be able to be guided towards the target by means of the position information received by the control station (8).
TARGET MARKING DEVICE AND TARGET TRACKING AND PROCESSING SYSTEMS COMPRISING SUCH A DEVICE
The target marking device (1) comprises a drone (2) which is provided with at least one transmitter (4), the transmitter (4) comprising an activation element (10) for activating it so that it transmits at a given time a signal (S) which represents a position information item, the transmitter (4) being configured to transmit at least one of the following signals: an infrared signal, a light signal, a sound signal, a signal generated by a chemical substance, the target marking device (1) being part of a target tracking system (6) and/or a target processing system which is provided with movable machinery (7).
UNMANNED VEHICLE WITH MULTIPLE PAYLOAD PLATFORMS
An unmanned vehicle and a method of operating the vehicle are provided. The vehicle includes a fuselage and at least one thrust device coupled to the fuselage. A first payload module having an first attachment plate is fixedly coupled to the fuselage, the first payload module further having a first control module removably coupled to the first attachment plate and a first payload having a first energetic element. A second payload module having an second attachment plate is fixedly coupled to the fuselage adjacent the first payload module, the second payload module further having a second control module removably coupled to the second attachment plate and a second payload having a second energetic element.
MOBILE AERIAL DRONE EARLY WARNING PRIVACY BREACH DETECT, INTERCEPT, AND DEFEND SYSTEMS AND METHODS
Systems and methods for aerial unmanned vehicle (for example, drone) early warning privacy breach detection, interception, and defense are disclosed. The system detects drones within a threshold distance of an individual or configurable location, notifies the individual of the drones' existence, tracks the drones, and executes countermeasures. The system can communicate with telecommunication networks or other sources (for example, FAA) to identify and filter out drones that are authorized to be in the airspace around the individual.
ELEVON CONTROL SYSTEM
A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) configured to control pitch, roll, and/or yaw via airfoils having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns. Embodiments include one or more rudder elements which may be rotatably attached and actuated by an effector member disposed within the fuselage housing and extendible in part to engage the one or more rudder elements.
ARMED AERIAL PLATFORM
An armed aerial platform (100) includes a weapon for firing a projectile from a barrel (102) that defines a weapon axis (104). The weapon is supported by a single-axis gimbal mechanism (116) within a central vertical slot (112) in a rigid body (108) of a UAV (108) carried by a propulsion system (114) including at least four rotary propulsion units. The gimbal mechanism (116) provides an elevation adjustment of the weapon axis (104), while the azimuth adjustment is provided by motion of the UAV (108) itself.