An in-flight aircraft tracking system may include a power transmission line suspended in the air and a radio frequency identification (RFID) reader configured to identify an aircraft in proximity to the power transmission line. A traffic control system may be configured to coordinate movement of multiple aircrafts in proximity to the power transmission line. An in-flight aircraft tracking method may include transmitting a reader signal from a RFID reader to an aircraft while the aircraft is in proximity to a power transmission line and receiving an identification signal in response to the reader signal from an RFID transmitter coupled to the aircraft.

A system and method for autonomous air-to-air refueling of an aircraft arranged on the receiver aircraft, including a vision system for capturing images of the receiver aircraft including the fuel receiving equipment and of the tanker aircraft comprising the dispensing equipment, an image processing system for receiving and processing the images to identify the shape of the fuel receiving equipment, the fuel dispensing equipment and the contour of the tanker aircraft and for calculating a distance between the fuel dispensing equipment and the fuel receiving equipment and the relative attitude of the tanker aircraft, a receiver aircraft positioning system for varying, based on the distance between the fuel receiving equipment and the fuel dispensing equipment and the relative attitude of the tanker aircraft, flight parameters of the receiver aircraft.

There is provided a technology that a user can select an alternative destination useful for the user. An information processing apparatus according to an embodiment of the present technology includes a control unit. The control unit sets an alternative destination of a moving route of a moving body based on profile information of the user in a case where the moving route of the moving body intersects a moving route of other moving body.

An in-flight contact charging system includes a charging contact, a power receiver, and a recharging controller connected to the charging contact. The charging contact is mounted on a support. The power receiver is mounted on an aerial vehicle containing an electrical load. The power receiver connects to the electrical load. The recharging controller can detect contact between the charging contact and the power receiver; transmit electricity to the charging contact; detect a spike in battery impedance; and discontinue transmission of electricity to the charging contact. The system enables a drone to rapidly recharge its battery while in flight by making brief contact between the charging contact and the power receiver. This system keeps the drone airborne, does not waste energy, and is comparatively cheap to build and maintain.

One embodiment includes an electrical tanker aircraft for in-flight recharging a worker aircraft, comprising: a charge source; an umbilical to engage an in-flight charge recipient aircraft; and control logic to determine that the umbilical has engaged the charge recipient aircraft, and to transfer charge until a termination condition is met.

A power recharging system may include an electrical conductor connected to a first aircraft and configured to connect to a second aircraft while the aircrafts are in flight. An AC signal may be induced in the electrical conductor it is in proximity to a changing magnetic field. The system may include a first rectifier circuit at the first aircraft that converts the AC signal into a DC signal for charging the first aircraft and a second rectifier circuit at the second aircraft that converts the AC signal into a second DC signal for charging the second aircraft. The electrical conductor may be part of a communication line. A communication system at the first aircraft may send and receive data communications via the communication line.

Computerized system and method of controlling a refueling device including, when the device is in a non-engaged state: receiving a first roll angle of a tanker, determining a first desired roll angle, and providing a command for controlling a roll element, thereby attempting to achieve or maintain a first roll angle that is substantially the same as the roll angle of the tanker. And, when the device is in an engaged state: receiving a second roll angle of the tanker, determining a second desired roll angle, and providing a command related to the desired roll angle for controlling a yaw element, thereby attempting to achieve or maintain a second roll angle that is substantially the same as the roll angle of the tanker, wherein the roll angle of the device during the engaged state is facilitated due to a degree of freedom between the refueling device body and refueling nozzle.

A power conversion unit may include two or more power modules for providing high-voltage direct current power to electrical loads, such as one or more propulsion motors aboard an aerial vehicle. Each of the power modules may be controlled by hysteresis, and may include one or more pairs of transistors that are switched by a gate driver with respect to differences between a reference current and a sensed current passing through a boost inductor. The number, size and shape of the power modules may be selected to accommodate the electrical loads, and may be switched on or off, as necessary. The power conversion unit may feature at least one more power module than is required to meet all anticipated electrical loads, thereby ensuring that the power conversion unit may continue to provide power even in the event that one of the power modules experiences a fault of any kind.

This invention is to provide a method to entirely and effectively shade fixed tracts of land, such as school yard or athletics stadium, etc., with no roof, pole to support roof, or the like. To fix a sheet to multiple flying objects so that such sheet forms a fixed size of surface and make such flying objects fly in accordance with flying positions (including heights) decided based on elements, such as positions of the sun, etc.

UAV airways system generally are disclosed. Such UAV airway systems may comprise UAV cargo transportation systems and UAV surveillance and monitoring systems. Such systems preferably overlay and are commensurate with a system of high-voltage power transmission lines of high-voltage transmission system, and electric field actuated (EFA) generators preferably are utilized in UAVs that travel along the transmission lines, in UAV charging stations located along the transmission lines, or in both. Each EFA generator represents a power supply and comprises first and second electrodes separated and electrically insulated from each other for enabling a differential in voltage at the first and second electrodes resulting from a differential in electric field strength experienced by the first and second electrodes arising from the power transmission lines of the high-voltage transmission system.