A tethered uni-rotor network of multiple tethered satellite vehicles; each having lifting airfoil surfaces, stabilizers, control surfaces, fuselages, and propulsion systems, operating in persistent state of rotation, driven by propulsion units on each satellite vehicle, where airfoils generate lift which supports aerial system. As system rotates, centrifugal forces pull satellite vehicles outwards, which keeps tethers taught. The tethers are attached to inboard portions of each lifting surface, which places their structural members under tension, thereby eliminating an adverse bending moment common to all traditional fixed-wing aircraft. Tethers provide large spatial separation eliminating rotor downwash field interactions, slowing system rotation rate, and permitting an ideal elliptic load distribution across wings. This reduces weight within structural members, uses higher aspect ratio wings to minimize induced drag, and employ thin-thickness high-camber airfoil profiles for superior lift-to-drag ratios, resulting in a more aerodynamically efficient aircraft, requiring less power than fixed-wing without sacrificing hover capability.

The present disclosure relates to an information processing apparatus and method and a program capable of more easily capturing image in accordance with more various situations. An imaging device including an imaging function unit and an imaging range variable unit is controlled on the basis of vehicle information that is information regarding a vehicle. For example, on the basis of vehicle information obtained in a patrol car, such as vehicle location and position information, vehicle speed information, vehicle operation information, or vehicle attached equipment information, imaging of a subject by the imaging device provided to a flying body and flight by the flying body are controlled. The present disclosure can be applied to, for example, an information processing apparatus, an image processing apparatus, a communication apparatus, an electronic device, an information processing method, a program, or the like.

A system for electric power production from wind includes a glider having an airfoil, an on-board steering unit, a flight controller for controlling the steering unit, and a connection unit for a tether. The system further includes a ground station including a reel for the tether, a rotating electrical machine connected to the reel, and a ground station controller for controlling the reel and the rotating electrical machine. A master controller operates the system in at least first and second operation modes. In the first operation mode electric power is produced with the rotating electrical machine from rotation of the reel caused by reeling out the tether using a lift force generated upon exposure of the airfoil of the airborne glider to wind. In the second operation mode, the reel is driven by the rotating electrical machine, thereby reeling in the tether onto the reel.

An aerial vehicle electrical power system for use with a tethered aerial vehicle, and related methods are provided. The aerial vehicle electric power system includes a plurality of light-emitting diodes (LEDs) carried by an aerial vehicle. At least one electrical circuit is carried by the aerial vehicle. The at least one electrical circuit has a DC buck converter electrically in series with at least a portion of the plurality of LEDs. A tether is connected between the aerial vehicle and a power source positioned remote from the aerial vehicle. Electrical power is transmitted to the aerial vehicle and at least a portion of the plurality of LEDs through the tether. The electrical circuit minimizes variances in power supplied to the aerial vehicle and the plurality of LEDs.

A system comprising: an Unmanned Aerial Vehicle (UAV) carrier comprising a power supply, the UAV carrier connected, via respective wires, to one or more UVs, wherein: (a) each of the UVs is capable of performing maneuvers irrespective of maneuvers of the UAV carrier during performance of a mission; and (b) each of the UVs receives at least one of an electrical current from the power supply or digital data from the UAV carrier through the respective wires, during performance of the mission.

An automated drone-based surface treatment material delivery system includes a drone having a body, at least one propeller rotatably supported by the body, at least one propeller motor supported by the body and configured to selectively apply motive power to the at least one propeller, and a controller supported by the body and configured to control a flight path of the drone at least by manipulating a speed of the at least one propeller. The drone also has a rotary atomizer supported by the body for movement therewith. The rotary atomizer includes a rotating dispersion structure configured to disperse a surface treatment material from a material supply.

A deployable airborne sensor array system and method of use are provided herein. The system includes a tether configured to be coupled to and deployed from an aircraft and a plurality of airborne vehicles coupled to the tether. Each of the plurality of airborne vehicles includes different lift characteristics to form a three-dimensional (3D) array of airborne vehicles. Each airborne vehicle includes a sensing device configured to generate sensor data associated with a target. The system also include a computing device configured to process the sensor data received from each of the plurality of airborne vehicles and generate an image of the target based on the sensor data.

An unmanned aerial vehicle (UAV) system energized by power lines includes a UAV, a charging mechanism and an electric circuit. The charging mechanism is operatively coupled to a body of the UAV. The charging mechanism can connect to power transmission lines deployed near an air space in which the UAV is airborne and operating. The charging mechanism can draw power from the power transmission lines to power a flight of the UAV. The electric circuit is onboard the UAV. The electric circuit can generate charging currents based on the power drawn from the power transmission lines to power the flight of the UAV while the UAV is airborne.

A flying umbrella assembly includes a flying drone that can fly through the air. An umbrella is removably attachable to the flying drone such that the umbrella can be flown above the ground. A tracking unit is carried by a user and the tracking unit broadcasts a tracking signal to the flying drone thereby facilitating the flying drone to fly within a pre-determined distance of the tracking unit. In this way the flying drone positions the umbrella over the user regardless if the user is stationary or in motion. A personal electronic device is in wireless communication with the flying drone. The flying drone receives the sun tracking data from the personal electronic device to optimally position the umbrella for shading the user.

Various embodiments may relate to an aerial vehicle. The aerial vehicle may include a frame. The aerial vehicle may also include a camera assembly attached to the frame, the camera assembly including a cascaded bi-directional linear actuator and a camera attached to the cascaded bi-directional linear actuator such that the camera is configured to be moved to different positions by the cascaded bi-directional linear actuator to capture a plurality of images of an object. The aerial vehicle may further include a processor in electrical connection to the camera such that the processor is configured to determine one or more dimensions of the object based on the plurality of images. The aerial vehicle may additionally include a flight system configured to move the aerial vehicle. The aerial vehicle may also include an energy system in electrical connection to the camera assembly, the processor, and the flight system.