A compact directed energy system is disclosed that is configured to generate directed energy beams. The compact directed energy system includes a radio frequency system configured to provide a directed energy beam in a frequency range between 500 MHz to 20 Ghz.

A system and a method are provided for achieving long range, over the horizon (OTH), persistent surveillance, alerting, tracking and situational awareness against small, low radar cross section moving targets. The system and method use one or more tethered unmanned arial systems, or unmanned arial vehicles, to lift components including a radar antenna to a height above nearby obstacles or much higher. The system and method can also be used for subsurface radar detection and tracking applications, as well as communications with submarines.

A method for enabling autonomous emergency assistance for one or more communication device, CD, registered in a regular cellular network. The method is performed in an autonomous unmanned aerial vehicle, UAV, and comprises emulating a cellular network in a geographical region, wherein the UAV and the one or more CD are without connectivity with the regular cellular network, sending an information message in the geographical region, the message comprising an emergency response trigger, receiving an automatic emergency data response from the one or more CD in the geographical region, in response to the sent message, and determining an action based on the received automatic emergency data response. A CD, a UAV, a computer program and a computer program product are also presented.

An information collection device according to the present disclosure is an information collection device that causes a small unmanned aerial vehicle to fly from a departure point to a destination and collects information at the destination using the small unmanned aerial vehicle, and includes a control device that causes the small unmanned aerial vehicle to fly from the departure point to the destination by transmitting a control signal to the small unmanned aerial vehicle by wireless information communication via a vehicle when determination is made that the wireless information communication is able to be executed with the small unmanned aerial vehicle via the vehicle located between the departure point and the destination.

Systems, apparatus, and methods for remote monitoring and piloting of a ship. Examples include a method of delivering remote monitoring equipment to the ship and establishing a data and communication exchange for shore-based pilotage of the ship from a remote location. The equipment usable for remote monitoring and communication between the ship and pilot (at the remote location) is stored in a package and delivered to the ship by unmanned aircraft. The package is distributed and installed by ship's crew to specified locations. The remote pilot while located ashore has access to all the information that is needed to assist in safe navigation of the ship by exchanging data and/or streaming real time video from the ship to shore. Additionally, the system may extract navigational data from the ship and transmit it to shore in real-time.

An example system for flying to a target location is provided, comprising a parent aerial vehicle and at least one child vehicle releasably coupled to the parent vehicle. The parent vehicle is configured to transport the at least one child aerial vehicle to a region containing a target location, uncouple from the at least one child aerial vehicle, and transmit information to the at least one child aerial vehicle relevant to operation of the child aerial vehicle. The child aerial vehicle comprises at least one sensor for surveillance at the target location.

A High Altitude Pseudo Satellite (HAPS) aircraft is disclosed, the aircraft including at least one aeroelastic span loaded fixed wing, an aspect ratio greater than 15 and wing loading less than 6 kg/m.sup.2, where the at least one wing has a plurality of spoilers distributed across the span of the wing and each spoiler being chordwise located adjacent the centre of pressure of the wing. The HAPS aircraft further includes a control system for controlling the spoilers, sensors which allow at least one of the quantity or quantities selected from the group comprising the amount of lift at points or regions along the wing span the pitch and roll at points or regions along the wing span, the bending and torsional strain at points or regions along the wing span, or the net speed and roll and pitch angle of the wing to be determined by the control system, and the spoiler being activatable to reduce the lift experienced by the wing in the location of the spoiler in response to the quantities determined by control system.

A method for improving wireless communication for a drone swarm, the method comprising, at a computing system, receiving, from a plurality of drones of a drone swarm, data comprising radio frequency signal characteristics detected by the plurality of drones; generating a model of a radio frequency environment for the drone swarm based on the data received from the plurality of drones; and controlling at least one wireless communication system to improve wireless communication for the drone swarm based on the model of the radio frequency environment.

The present disclosure discloses a method for managing a UAV control operation that includes: periodically receiving a request for transmission of UAV assistance information from a network entity and establishing a radio resource control (RRC) connection with the network entity. In response to the received request, the method further includes determining a triggering of at least one event corresponding to an initiation of a UAV control operation and transmitting UAV assistance information to the network entity in an RRC connected state based on the determined triggering of the at least one event. The method further includes receiving a control message from the network entity in response to the transmitted UAV assistance information. The control message includes information related to an execution of the UAV control operation. Thereafter, the method further includes executing the UAV control operation based on the information included in the received control message.

A fluid tank for integration into a structure of an unmanned aircraft includes a shell having a first axial wall, an oppositely arranged second axial wall, an upper side, a lower side, and an enclosed interior, at least one receiving chamber in the interior for storing fluid, and a collection chamber, which is arranged on the lower side and which is fluidically connected to the at least one receiving chamber. The collection chamber includes a bottom surface, through which there extends a drain, wherein a covering surface is arranged above the bottom surface and covers at least a portion of the collection chamber. At least one flow opening could be arranged on an upper side of the collection chamber, which flow opening allows gas bubbles to escape in the direction of the upper side of the fluid tank.