Method and apparatus for providing substantially uninterrupted communications in a satellite network system

• US 20030211829A1
• Filed: 05/10/2002
• Published: 11/13/2003
• Est. Priority Date: 05/10/2002
• Status: Abandoned Application

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Chapelle, Michael de la, Quadracci, Leonard J., Morse, David C.
• Application Number:
  US10/143,693
• Publication Number:
  US 20030211829A1
• Time in Patent Office: Days
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/18578 Satellite systems for providing broadband data service to individual earth stations for selecting H04W; provisions for broadband connection, H04Q11/0478

Abstract

A communication management system and technique that provides a flexible yet efficient means of coordinating communications between an Earth bound user and a non-geosynchronous orbit (NGSO) satellite constellation. The system distributes the majority of the management of communications links to operations and control center and the ground based users. Therefore, the responsibility for handling communication management is performed by the ground based users and control center as opposed to being the responsibility of the NGSO satellites. This allows the NGSO satellites to be minimized in size and cost while maximizing the resources available to users. Furthermore, the ground based systems may be more easily updated and maintained than would be the case if the satellites were responsible for this task.

Claims

1. A communication planning system, comprising:

at least one satellite comprising a plurality of communication resources and adapted to produce a footprint comprising at least one signal beam, wherein said at least one signal beam is projected onto a ground surface;

a transceiver for communicating with said at least one satellite using at least a first of said plurality of communication resources; and

a control system, for determining a configuration of said plurality of communication resources such that said at least one satellite allocates said at least first communication resource to said transceiver.

2. The communication planning system of claim 1,

wherein said at least one signal beam comprises a plurality of signal beams;

and

wherein each of said plurality of signal beams comprises said plurality of communication resources.

3. The communication planning system of claim 4,

wherein said control system configures said plurality of signal resources before said transceiver initiates said communication with a first satellite of said plurality of satellites, such that said first satellite is apprised of a maximum capacity for each of said plurality of signal beams.

4. The communication planning system of claim 1, wherein said at least one satellite comprises a plurality of satellites.

5. The communication planning system of claim 1, wherein said plurality of signal resources comprises a communications channel within said at least one signal beam.

6. The communication planning system of claim 1, wherein said at least one signal resource of said plurality of signal resources is allocated by said at least one satellite when said transceiver initiates said communication with said at least one satellite.

7. The communication planning system of claim 1, wherein said transceiver is adapted to synchronously switch in real time with said at least one satellite between at least two of said plurality of signal resources.

8. The communication planning system of claim 1, wherein said at least one satellite comprises at least a first satellite and a second satellite, wherein said transceiver is allocated at least one signal resource of said second satellite while said transceiver is communicating with said first satellite.

9. The communication system of claim 8, wherein said transceiver transmits to said first satellite a path of said transceiver through said footprint of said second satellite, and wherein said first satellite transmits said path to said second satellite.

10. A method to ensure that a communication is generally constant between a satellite constellation and a transceiver comprising an organizational unit, the method comprising:

providing a satellite constellation comprising at least one satellite orbiting the Earth in a non-geosynchronous orbit;

providing a plurality of signal resources on said at least one satellite;

producing a footprint comprising a plurality of signal beams adapted to allow transmission of a data stream using said plurality of signal resources;

transmitting a data stream between the transceiver and said at least one satellite by transmitting a signal along said signal beam using one of said signal resources; and

determining an optimal configuration of said plurality of signal resources to ensure that said data stream is substantially continuous between said transceiver and said at least one satellite.

11. The method of claim 10, further comprising:

configuring a registration comprising a look up table for each of said plurality of signal beams to include at least one of said plurality of signal resources based upon said optimal configuration.

12. The method of claim 11, wherein said step of communicating between said transceiver and said satellite, comprises:

transmitting from said transceiver to said at least one satellite a location of said transceiver;

transmitting to said at least one satellite from said transceiver through which of said plurality of said signal beams said transceiver will pass; and

receiving and transmitting a data stream between said transceiver and said at least one satellite as said transceiver passes through said footprint.

13. The method of claim 12, further comprising:

reserving at least one of said plurality of signal resources in said registration;

transmitting to said transceiver said reserved signal resource; and

setting said transceiver to send and receive a data stream using said reserved signal resource.

14. The method of claim 10, wherein the step of determining an optimal configuration, comprises:

determining a location of said transceiver;

determining a location of an uplink cell, wherein said location of the transceiver is relative said location of said uplink cell;

predicting a future usage of said transceiver; and

determining said optimum distribution of said plurality of signal resources for said uplink cell based upon said predicted usage patterns.

15. The method of claim 10,

wherein the step of providing a satellite constellation comprising at least one satellite comprises providing at least a first satellite and a second satellite, wherein said first satellite produces a first footprint and said second satellite produces a second footprint;

transmitting to said first satellite from said transceiver a path of said transceiver through said second footprint;

transmitting to said second satellite from said first satellite said path of said transceiver through said second footprint; and

reserving on said second satellite signal resources in said path for said transceiver.

16. A system for providing substantially uninterrupted communications between a terrestrial based transceiver and an orbiting satellite network, comprising:

at least one transceiver adapted to communicate with a satellite in at least one configuration;

at least one satellite adapted to communicate with said transceiver, wherein said satellite comprises a communication resource and an antenna, wherein said antenna is adapted to produce a footprint comprising at least two beams which are movable relative to said transceiver;

a storage system for storing a location of said transceiver;

a processor, for allocating said communication resources among said two beams; and

wherein said configuration of said transceiver corresponds to said communication resource to allow sending and receiving a data stream between said transceiver and said satellite.

17. The system of claim 16,

wherein said transceiver comprises a plurality of transceivers each having a discrete location;

and

wherein said storage system stores the locations of each of said plurality of transceivers.

18. The system of claim 16,

wherein said two beams comprise a first beam and a second beam;

and

wherein said transceiver transmits to said satellite to inform said satellite when said transceiver will pass from said first beam to said second beam.

19. The system of claim 16,

wherein said satellite comprises at least a first satellite and a second satellite, wherein said first satellite produces a first footprint and said second satellite produces a second footprint;

wherein said transceiver transmits to said first satellite a time and a path through which said transceiver will pass through said first footprint; and

wherein said transceiver transmits to said first satellite a time and a path through which said transceiver will pass from said first footprint to said second footprint and a time and a path through which said transceiver will pass through said second footprint; and

wherein said first satellite transmits to said second satellite said time and said path said transceiver will pass from said second footprint.