Hub communications satellite and system

• US 6,009,306 A
• Filed: 02/05/1996
• Issued: 12/28/1999
• Est. Priority Date: 02/05/1996
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Original Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Inventors: Hargis, Keith J.
• Primary Examiner(s): Chin, Wellington
• Assistant Examiner(s): SOBUTKA, PHILIP
• Application Number:
  US08/595,455
• Time in Patent Office: 1,422 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.2, 455/13.3, 455/53.1, 455/33.1, 455/427, 455/428, 342/356
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/19 Earth-synchronous stations

Abstract

A satellite communications system includes hub satellite which are equipped to communicate with at least three other satellites. The hub satellites include crosslink interfaces for each of the other satellites with which it may communicate and a switching system for routing those communications between interfaces. A system of a given number of satellites may include several hubs and may be configured in a way which permits any satellite within the system to communicate with a hub either directly or after transiting one or more intervening satellites. Systems which include fewer hubs may require communication with more than one intervening satellite before a hub is reached.

Claims

1. A satellite communications system for facilitating communications between communications ground stations of Earth, comprising:

a communications constellation distributed throughout one orbit around said Earth, said communications constellation formed with;

a) a plurality of satellites which each occupies a different position in said orbit and therefore has a pair of adjacent nearest-neighbor satellites;

b) a pair of crosslink interfaces positioned in each of said satellites to facilitate communications crosslinks with each of its nearest-neighbor satellites;

c) a plurality of groundlink interfaces which are each positioned in a different one of said satellites to facilitate a communications groundlink between that satellite and one of said communications ground stations; and

(d) at least one pair of cross-orbit crosslink interfaces which are each positioned in a different one of a pair of satellites that are not nearest-neighbor satellites to facilitate a cross-orbit communications link across said communications constellation;

wherein said cross-orbit communications link is absent in at least one of said satellites;

and wherein the number of pairs of cross-orbit crosslink interfaces is sufficient to prevent any one of said satellites from being separated from a cross-orbit communications link by more than one intervening satellite;

each of said satellites of said communications constellation thereby provided with at least three alternate communication paths to each other of said satellites which enhances communications routing flexibility between said satellites and said communications ground stations.

2. The satellite communications system of claim 1, wherein said orbit is a geosynchronous orbit.

3. The satellite communications system of claim 1, wherein said orbit is a geostationary orbit.

4. The satellite communications system of claim 1, wherein each of said satellites further includes a communications switching system which couples communications signals between any crosslink interfaces, groundlink interface and cross-orbit crosslink of that satellite.

5. The satellite communications system of claim 4, wherein said switching system includes:

a controller; and

a switch which interconnects communications signals in response to said controller.

6. The satellite communications system of claim 5, wherein said switch is a cross-bar switch.

7. The satellite communications system of claim 4, wherein each of said crosslink interfaces, said groundlink interfaces and said cross-orbit crosslink interfaces includes:

a receiving antenna;

a receiver arranged to couple communications signals from said receiving antenna to said switching system;

a transmitting antenna; and

a transmitter arranged to couple communications signals from said switching system to said transmitting antenna.

8. A satellite communications system for facilitating communications between communications ground stations of Earth, comprising:

a communications constellation distributed throughout one orbit around said Earth, said communications constellation formed with a plurality of satellites which each occupies a different position in said orbit;

at least two satellite groups formed by said satellites with each of said groups including;

a) a hub satellite;

b) a plurality of group satellites;

c) in each of said group satellites, a direct-access crosslink interface to facilitate a direct-access communications crosslink between that group satellite and said hub satellite; and

d) in each of said group satellites, a groundlink interface to facilitate a communications groundlink between that group satellite and one of said communications ground stations;

and

at least one cross-orbit communications link across said communications constellation that is facilitated by a pair of cross-orbit crosslink interfaces which are each positioned in a different one of a pair of hub satellites;

wherein said cross-orbit communications link is absent in all of said group satellites.

9. The satellite communications system of claim 8, wherein said orbit is a geosynchronous orbit.

10. The satellite communications system of claim 8, wherein said orbit is a geostationary orbit.

11. The satellite communications system of claim 8, wherein each of said satellite groups further includes a communications switching system which couples communications signals between any direct-access crosslink interface, groundlink interface and cross-orbit crosslink of that satellite group.

12. The satellite communications system of claim 11, wherein said switching system includes:

a controller; and

a switch which interconnects communications signals in response to said controller.

13. The satellite communications system of claim 12, wherein said switch is a cross-bar switch.

14. The satellite communications system of claim 8, wherein each of said direct-link crosslink interfaces, said groundlink interfaces and said cross-orbit crosslink interfaces includes:

a receiving antenna;

a receiver arranged to couple communications signals from said receiving antenna to said switching system;

a transmitting antenna; and

a transmitter arranged to couple communications signals from said switching system to said transmitting antenna.