Abstract:
Embodiments of methods for providing distributed airborne wireless communications are provided herein. In some embodiments, a method of providing wireless communication services includes: receiving a radio frequency (RF) signal from a first area by a distributed airborne communication payload, wherein the distributed airborne communication payload is comprised of sections located on respective ones of a plurality of airborne platforms; relaying the RF signal along the sections located on different airborne platforms; and transmitting the RF signal to a second area.
Abstract:
Embodiments of the present invention provide an aircraft for vertical take-off and landing. In various embodiments, an aircraft assembly includes at least one first wing portion providing a lift force during a horizontal flight, at least one wing opening disposed on a vertical axis of the at least one first wing portion and at least one thruster positioned inside the at least one wing opening to provide vertical thrust during a vertical flight. The aircraft assembly can further include air vents positioned inside at least one of the wing openings. The air vents can further include louvres positioned over or under the air vents to open and close the wing openings. The thruster can further be used to provide flight control for the aircraft.
Abstract:
Embodiments of methods for providing distributed airborne wireless communications are provided herein. In some embodiments, a method of providing wireless communication services includes: receiving a radio frequency (RF) signal from a first area by a distributed airborne communication payload, wherein the distributed airborne communication payload is comprised of sections located on respective ones of a plurality of airborne platforms; relaying the RF signal along the sections located on different airborne platforms; and transmitting the RF signal to a second area.
Abstract:
Methods and apparatus for providing distributed airborne wireless communications are provided. An airborne wireless communication system may include: an airborne fleet comprising a plurality of airborne platforms; a distributed communication payload subdivided into parts, each distributed on respective airborne platforms. The communication payload comprises air-to-user link equipment and air-to-air link equipment to provide communications between the airborne wireless communication system and end-users and between individual airborne platforms; and payload control electronics to control the air-to-user and air-to-air equipment and manage operation of the airborne wireless communication system. The air-to-user link equipment comprises an RF antenna to produce an RF beam in a direction towards the ground. A communication cell is defined on the ground and in the airspace below the fleet bounded by a boundary of the RF beam. The air-to-user communication equipment is configured to provide communication links between the airborne fleet and end-user devices within the communication cell.