Non-uniform multi-beam satellite communications system and method

• US 6,463,281 B1
• Filed: 04/19/2000
• Issued: 10/08/2002
• Est. Priority Date: 10/17/1997
• Status: Expired due to Term

• Current Assignee: News America Incorporated (The Walt Disney Company)
• Original Assignee: Hughes Electronics Corporation (Rtx Corporation)
• Inventors: Norin, John L., Pontual, Romulo, Rao, Sudhakar, Regulinski, Paul
• Primary Examiner(s): Maung, Nay
• Assistant Examiner(s): Persino, Raymond B
• Application Number:
  US09/552,333
• Time in Patent Office: 902 Days
• Field of Search: 455/429, 455/427, 455/444, 455/449, 455/446, 455/443, 455/13.3, 455/12.2, 455/13.2, 342/354, 342/353, 342/352, 343/753, 343/776, 343/772, 343/775, 343/777, 343/779, 343/781.P, 343/781.R
• US Class Current: 455/429
• CPC Class Codes: H04B 7/18523 Satellite systems for providing broadcast service to terrestrial stations, i.e. broadcast satellite service arrangements specially adapted for satellite broadcast receiving H04H40/90; picture transmission via satellite H04N1/00103; television transmission via satellite H04N7/20
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

A satellite broadcast system and method, particularly useful for television signals, allows for local as well as nationwide broadcast service by allocating greater satellite resources to the more important local service areas. This is accomplished by broadcasting a non-uniform pattern of local service beams and designing the system to establish different service area priorities through factors such as the individual beam powers, sizes, roll-off characteristics and peak-to-edge power differentials. Frequency reuse is enhanced by permitting a certain degree of cross-beam interference, with lower levels of interference established for the more important service areas.

Claims

1. A spacecraft broadcast method, comprising:

broadcasting multiple communication signal beams from a spacecraft to different respective target area locations in a non-uniform beam pattern so that at least some of said beams have different sizes at their respective target locations, with at least some smaller beams having higher power levels than at least some larger beams, and

providing different respective signal frequency spectrums for at least some of said beams.

2. The method of claim 1, wherein at least some of said beams have a common signal frequency spectrum, and all of the beams with the same common frequency spectrum are directed to non-overlapping target area locations.

3. The method of claim 1, wherein at least some of said beams have different sizes at their respective target area locations.

4. The method of claim 1, wherein at least some of said beams are broadcast to produce different beam powers at their respective target area locations.

5. The method of claim 4, wherein said at least some beams are broadcast from the spacecraft with different respective beam powers.

6. The method of claim 1, wherein at least some of said beams with different signal frequency spectrums are broadcast to overlapping target area locations.

7. The method of claim 1, wherein at least some of said beams are broadcast with different respective signal bandwidths.

8. The method of claim 1, wherein at least some of said beams are broadcast with different beam roll-off characteristics.

9. The method of claim 1, wherein at least some of said beams are broadcast with different peak-to-edge power differentials.

10. A spacecraft broadcast method, comprising:

broadcasting multiple communication signal beams from a spacecraft to different respective target area locations so that at least some of said beams have different sizes at their respective target locations, with at least some smaller beams having higher power levels than at least some larger beams, and

providing different respective signal frequency spectrums for at least some of said beams.

11. The method of claim 10, wherein at least some of said beams-have a common signal frequency-spectrum, and all of the beams with the same common frequency spectrum are directed to non-overlapping target locations.

12. The method of claim 10, wherein at least some of said beams are broadcast to produce different beam powers at their respective target area locations.

13. The method of claim 12, wherein said at least some beams are broadcast from the spacecraft with different respective beam powers.

14. The method of claim 10, wherein at least some of said beams with different signal frequency spectrums are broadcast to overlapping target area locations.

15. The method of claim 10, wherein at least some of said beams are broadcast with different respective signal bandwidths.

16. The method of claim 10, wherein at least some of said beams are broadcast with different beam roll-off characteristics.

17. The method of claim 10, wherein at least some of said beams are broadcast with different peak-to-edge power differentials.

18. The spacecraft broadcast method of claim 10, wherein at least some of said beams have different beams powers at their respective target area locations.

19. The method of claim 18, wherein said at least some beams are broadcast from the spacecraft with different respective beam powers.

20. The method of claim 18, wherein at least some of said beams have a common signal frequency spectrum, and all of the beams with the same common frequency spectrum are directed to non-overlapping target area locations.

21. The method of claim 18, wherein at least some of said beams with different frequency bands are broadcast to overlapping target area locations.

22. The method of claim 18, wherein at least some of said beams are broadcast with different respective signal bandwidths.

23. The method of claim 18, wherein at least some of said beams are broadcast with different beam roll-off characteristics.

24. The method of claim 18, wherein at least some of said beams are broadcast with different peak-to-edge power differentials.

25. A spacecraft broadcast method, comprising:

broadcasting multiple communication signal beams from a spacecraft to respective non-overlapping target area locations so that at least some of said beams have different sizes at their respective target area locations and at least some smaller beams have higher power levels than at least some larger beams, and

providing a common signal frequency spectrum for each of said beams.

26. The method of claim 25, wherein at least some of said beams are broadcast to produce different beam powers at their respective target area locations.

27. The method of claim 26, wherein said-at least some beams are broadcast from the spacecraft with different respective beam powers.

28. The method of claim 25, wherein at least some of said beams are broadcast with different respective signal bandwidths.

29. The method of claim 25, wherein at least some of said beams are broadcast with different beam roll-off characteristics.

30. The method of claim 25, wherein at least some of said beams are broadcast with different peak-to-edge power differentials.