Airborne cell tower system for wireless communications in remote and rural geographic areas

• US 10,374,690 B2
• Filed: 03/23/2015
• Issued: 08/06/2019
• Est. Priority Date: 03/28/2014
• Status: Active Grant

• Current Assignee: Tara Chand Singhal
• Original Assignee: Tara Chand Singhal
• Inventors: Singhal, Tara Chand
• Primary Examiner(s): Flores, Leon
• Application Number:
  US14/664,921
• Publication Number:
  US 20150280811A1
• Time in Patent Office: 1,597 Days
• CPC Class Codes: H04B 7/18504 Aircraft used as relay or high altitude atmospheric platform
• CPC Class Codes: H04W 40/20 based on geographic position or location

Abstract

An airborne cell tower system for providing wireless communication in remote and sparsely populated areas provides wireless communication coverage in that region. The system 10 has an airborne cell tower unit assembly, where the assembly is airborne with the help of a helium balloon. Multiple units are positioned in an air region in a pattern to provide wireless coverage for a specified geographic region to provide wireless communication coverage in that region.

Claims

1. An airborne cell tower system for providing wireless communication, the system comprising:

multiple units of an airborne cell tower unit assembly, wherein the airborne cell tower unit assembly is tethered to a helium balloon and is airborne with the help of the helium balloon, and wherein the airborne cell tower unit assembly has electronics and antennas to provide wireless communications coverage to mobile wireless devices;

a ground based computer system, wherein the ground based computer system is configured with a central processing unit (CPU), a memory and a system management logic operating therein, wherein the system management logic is configured to position and maintain multiple units of the airborne cell tower unit assembly in a grid pattern in an air region, wherein the multiple units of the airborne cell tower unit assembly provide wireless communications coverage for a specified geographic region;

each unit of the multiple units of the airborne cell tower unit assembly is configured with a unit management computer, wherein the unit management computer is configured with a CPU, a memory, and a drift zone logic operating therein;

the unit management computer is configured additionally with a global positioning system (GPS) receiver and a GPS function, wherein the GPS function is configured for computing a location of the airborne cell tower unit assembly;

the drift zone logic is configured to receive a periodic input of the location of the airborne cell tower unit assembly from the GPS function and is configured to output control signals to a location control system of the airborne cell tower unit assembly that maintains the location of the airborne cell tower unit assembly in a pre-defined drift zone of a specified air borne location in the air region;

the drift zone logic is further configured to maintain the location of the airborne cell tower unit assembly in the air region within an height envelope of approximately two to four miles, thereby maintain the airborne cell tower unit assembly above cloud cover and below high winds.

2. The system as in claim 1, comprising:

the system management logic is configured to being initialized with coordinates of the air region and is configured to receive and receives GPS location data from each of the multiple units, selects an individual unit and sends commands to the unit management computer of the individual unit for positioning the individual unit on an edge of the air region, wherein the edge of the air region provides a wireless line of sight access to a ground based cell tower or a mobile switching center for establishing a communication link to connect the system to a global telecommunication network.

3. The system as in claim 1, comprising:

the system management logic is configured to define and defines the air region with GPS coordinates with a size of one of (i) 100 square miles, (ii) 1000 square miles (iii) 10,000 square miles;

the system management logic being configured to input GPS coordinates of the air region that creates a shape of the air region from one of, square, rectangular, irregular shape, and longitudinal shape by defining GPS coordinates of a boundary of the air region, where the air region covers population or communities of interest which lack communication capabilities.

4. The system as in claim 1, comprising:

the system management logic is configured to position and positions the cell tower unit assembly air borne in air above a minimum height and below a maximum height above ground, wherein maintaining the unit assembly above the minimum height keeps the unit assembly above cloud level and maintaining the unit assembly below the maximum height keeps the unit assembly below a region of strong air currents.

5. The system as in claim 1, comprising:

the system management logic is configured to provide and provides a telemetry interface logic for sending and receiving telemetry data with each cell tower unit assembly, wherein each unit assembly has telemetry electronics and is in communication with the ground based computer system, wherein the ground based computer system has a computer with a memory and a CPU, and therein stored in the memory and operating in the CPU is a command and control logic that can assess the health of each cell tower unit assembly from the telemetry data and reposition the cell tower unit assembly for maintenance and deploy spare cell tower unit assemblies that are pre-positioned on a standby status in the air region.

6. An airborne cell tower unit assembly comprising:

sub-assemblies of (i) a unit management computer configured with a central processing unit (CPU), a memory and a logic operating therein, wherein the logic provides a location control management function, wherein the location control management function is configured to receive a periodic input of the location of the airborne cell tower unit assembly from a global positioning system (GPS) function and is configured to output control signals to a location control system of the airborne cell tower unit assembly that maintains the location of the airborne cell tower unit assembly in a pre-defined drift zone of a specified air borne location in the air region and is further configured to maintain and maintains the location of the unit assembly in the air region within an height envelope of approximately two to four miles, thereby maintain the unit assembly above cloud cover and below high winds;

(ii) a telemetry system computer configured with a CPU, a memory and a logic operating therein, wherein the logic provides telemetry functions, (iii) a solar cell system computer configured with a CPU, a memory and a logic operating therein, wherein the logic provides management of the solar panels that are coupled with a storage battery, (iv) an antenna group computer configured with a CPU, a memory and a logic operating therein, wherein the logic provides antenna coverage for a ground area, (v) a second antenna group configured with a CPU, a memory and a logic operating therein, wherein the logic provides communication links to other cell tower units and a ground based system, (vi) a routing computer configured with a CPU, a memory and a routing logic operating therein, wherein the routing logic provides routing of communication signals, and a (vii) a communication computer configured with a CPU, a memory and a logic operating therein, wherein the logic provides receiving and transmitting communication signals.

7. The assembly as in claim 6, the airborne cell tower unit further comprising:

(viii) a GPS computer configured with a CPU, a memory and a logic operating therein, wherein the logic provides GPS function for location determination, (ix) a thruster subsystem computer configured with a CPU, a memory and a logic operating therein, wherein the logic provides control of thrusters, (x) an air valve system computer configured with a CPU, a memory and a logic operating therein, wherein the logic provides control of the air valve system, (xi) a drift management computer configured with a CPU, a memory and a logic operating therein, wherein the logic, by computing and implementing a change in position of the unit based on a ground command, and sending a GPS location status of the unit to a ground system; and

using these sub-assemblies (viii), (ix), (x) and (xi) the assembly positions a unit in a specified air borne location in an air region.

8. The assembly as in claim 6, comprising:

the routing logic configured to use the link antennas to create and maintain a routing map of the airborne cell tower units that are positioned around a airborne cell tower unit;

the routing logic configured to use the routing map, to route data packets to a destination.

9. The assembly as in claim 6, comprising:

the airborne cell tower unit assembly configured to route wireless communications to and from wireless handsets in a geographic region to other wireless handsets in a global communication network;

the airborne cell tower unit assembly configured to use a routing map of the airborne cell tower units in the region and routes data packets to a destination in the global communication network.

10. The assembly as in claim 6, comprising:

the airborne cell tower unit assembly configured to provide an antenna group for providing links to other airborne cell tower units and ground based system;

wherein antennas of the antenna group are mounted on a four sides of the airborne cell tower unit with a communication pattern to be able to communicate with other airborne cell tower units in vicinity as part of a grid of airborne cell tower units;

the airborne cell tower unit assembly configured to use selected units to communicate with a ground based cell tower system to be able to link the units to a national communication network.

11. A method for an airborne cell tower system for providing wireless communication, comprising the steps of:

providing multiple units of an airborne cell tower unit assembly, wherein the airborne cell tower unit assembly is tethered to a helium balloon and is airborne with the help of the helium balloon, and wherein the airborne cell tower unit assembly has electronics and antennas to provide wireless communications coverage to mobile wireless devices;

providing a ground based computer system, wherein the ground based computer system is configured with a central processing unit (CPU), a memory and a system management logic operating therein, wherein the system management logic is configured to position and maintain multiple units of the airborne assembly in a grid pattern in an air region, wherein the multiple units provide wireless communications coverage for a specified geographic region;

configuring each unit of the multiple units of an airborne cell tower unit assembly with a unit management computer, wherein the unit management computer is configured with a CPU, a memory, and a drift zone logic operating therein;

configuring additionally the unit management computer with a global positioning system (GPS) receiver and a GPS function, wherein the GPS function is configured for computing a location of the airborne cell tower unit assembly;

configuring the drift zone logic to receive a periodic input of the location of the airborne cell tower unit assembly from the GPS function and is configured to output control signals to a location control system of the airborne cell tower unit assembly that maintains the location of the airborne cell tower unit assembly in a pre-defined drift zone of a specified air borne location in the air region;

further configuring the drift zone logic to maintain and maintains the location of the unit assembly in the air region within an height envelope of approximately two to four miles, thereby maintain the unit assembly above cloud cover and below high winds.

12. The method as in claim 11, comprising the steps of:

configuring the unit management computer with logics for, (i) a management function for a unit location control, (ii) a telemetry function, (iii) a management function for a solar cell system coupled with a storage battery, (iv) a management function for an antenna group providing coverage for a ground area, (v) a management function for an antenna group for providing link to other units and ground based system, (vi) a routing management function, and a (vii) a communication management function.

13. The method as in claim 12, comprising the steps of:

configuring the unit management computer with logics for the location control management function, wherein the location control management function has (viii) a GPS function (ix) a thruster subsystem (x) an air valve system and wherein using these functions and systems the location control management function positions a unit in a specified air borne location in the region;

configuring the unit management computer with sub-functions of drift management, for managing drift of the unit, computing and implementing a change in position of the unit based on a ground command, and sending a GPS location status to a ground system.

14. The method as in claim 12, comprising the steps of:

configuring the system management logic by providing the routing management function using the link antennas to create and maintain a routing map of the unit assemblies and;

using the routing management function and the routing map, routing data packets to a destination.

15. The method as in claim 12, comprising the steps of:

configuring the airborne cell tower unit system by routing wireless communications to and from wireless handsets in a geographic region to other wireless handsets in a global communication network;

using by the airborne cell tower unit system a routing map of the airborne cell tower units in the region and routing data packets to a destination in the global communication network.

16. The method as in claim 11, comprising the steps of:

configuring the system management logic by initializing coordinates of an air region and receiving GPS location data from each of the multiple units, selecting an individual unit and sending commands to the unit management computer for positioning the individual unit on an edge of the air region that has wireless line of sight access to a ground based cell tower or a mobile switching center for a communication link to connect to a global telecommunication network.

17. The method as in claim 11, comprising the steps of:

configuring the system management logic by positioning the assembly air borne in air above a minimum height and below a maximum height above ground, wherein, maintaining the unit assembly above the minimum height keeps the assembly above cloud level and maintaining the unit assembly below the maximum height keeps the unit assembly below a region of strong air currents.

18. A method for creating an airborne cell tower system, wherein the airborne cell tower system is comprised of multiple airborne cell tower assembly units, comprising the steps of:

configuring an airborne cell tower system computer for launching the multiple airborne cell tower assembly units;

determining a geographic region in remote areas that lack wireless communication system and determining the number of airborne cell tower assembly units required for the geographic region;

provisioning the multiple assemblies of the air borne cell tower assembly and launching the multiple airborne cell tower assembly units in the geographic region;

providing in each of the air borne cell tower assembly unit a unit management computer and a global positioning system (GPS) receiver, wherein the unit management computer has been configured with a central processing unit (CPU), a memory, and resident in the memory and operating in the CPU, a drift zone logic and a GPS function;

maintaining, by the drift zone logic and the GPS function, the location of the air borne cell tower assembly unit in a pre-defined drift zone for positioning the airborne cell tower assembly unit in a specified air borne location in the air region.

19. The method for an airborne cell tower system of claim 18, comprising the steps of:

provisioning for spare airborne cell tower assembly units in a field area in the vicinity of the air region;

performing a test operation on the air borne cell tower assembly in the air region.

20. The method for an airborne cell tower system of claim 18, comprising the steps of:

controlling and managing the units with the airborne cell tower system computer at a ground station; and

activating the air borne cell tower system for operational use.