Methods and apparatus for a distributed airborne wireless communications fleet
First Claim
1. A communication fleet, comprising:
- an airborne communication payload subdivided into multiple payload sections, wherein the multiple payload sections of the airborne communication payload combine to function as a single network component; and
a plurality of airborne platforms each including a payload section, wherein each airborne platform comprises an airframe, a propulsion system, a power system, and flight control electronics, wherein the propulsion system is configured to provide propulsion power and thrust to maintain level flight, ascend, descend and maneuver the airborne platform, wherein the power system provides electrical power to the propulsion system, the flight control electronics, and the payload section, wherein an RF or optical signal transmitted between the plurality of airborne platforms controls operation of the multiple payload sections of the airborne communication payload, and wherein the flight control electronics provide capability to control a position, speed, and flight pattern of the airborne platform.
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Accused Products
Abstract
Embodiments of methods and apparatus for providing distributed airborne wireless communications are provided herein. In some embodiments, a communication fleet includes: an airborne communication payload subdivided into multiple payload sections; and a plurality of airborne platforms each including a payload section, wherein each airborne platform comprises an airframe, a propulsion system, a power system, and flight control electronics, wherein the propulsion system is configured to provide propulsion power and thrust to maintain level flight, ascend, descend and maneuver the airborne platform, wherein the power system provides electrical power to the propulsion system, the flight control electronics, and the payload section, and wherein the flight control electronics provide capability to control a position, speed, and flight pattern of the airborne platform.
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Citations
28 Claims
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1. A communication fleet, comprising:
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an airborne communication payload subdivided into multiple payload sections, wherein the multiple payload sections of the airborne communication payload combine to function as a single network component; and a plurality of airborne platforms each including a payload section, wherein each airborne platform comprises an airframe, a propulsion system, a power system, and flight control electronics, wherein the propulsion system is configured to provide propulsion power and thrust to maintain level flight, ascend, descend and maneuver the airborne platform, wherein the power system provides electrical power to the propulsion system, the flight control electronics, and the payload section, wherein an RF or optical signal transmitted between the plurality of airborne platforms controls operation of the multiple payload sections of the airborne communication payload, and wherein the flight control electronics provide capability to control a position, speed, and flight pattern of the airborne platform. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17)
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18. A method of operating a communication fleet, comprising:
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dividing an airborne communication payload into multiple payload sections, wherein the multiple payload sections of the airborne communication payload combine to function as a single network component; providing a plurality of airborne platforms, wherein each airborne platform comprises an airframe, a propulsion system, a power system, and flight control electronics, wherein the propulsion system in configured to provide propulsion power and thrust to maintain level flight, ascend, descend and maneuver the airborne platform, wherein the power system provides electrical power to the propulsion system, the flight control electronics, and the payload section, wherein an RF or optical signal transmitted between the plurality of airborne platforms controls operation of the multiple payload sections of the airborne communication payload, and wherein the flight control electronics provide capability to control a position, speed, and flight pattern of the airborne platform; and placing each payload section in an airborne platform of the plurality of airborne platforms. - View Dependent Claims (19, 20, 21, 22, 23, 24, 25, 26, 27, 28)
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Specification