Non-uniform multi-beam satellite communications method

• US 6,456,846 B2
• Filed: 08/29/2001
• Issued: 09/24/2002
• Est. Priority Date: 10/17/1997
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (Rtx Corporation), News America Incorporated (The Walt Disney Company)
• Original Assignee: Hughes Electronics Corporation (Rtx Corporation)
• Inventors: Pontual, Romulo, Norin, John L., Rao, Sudhakar, Regulinski, Paul
• Primary Examiner(s): Maung, Nay
• Assistant Examiner(s): Persino, Raymond B.
• Application Number:
  US09/942,340
• Publication Number:
  US 20020006795A1
• Time in Patent Office: 391 Days
• Field of Search: 455/429, 455/427, 455/444, 455/449, 455/446, 455/443, 455/13.3, 455/12.1, 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 respective reflectors on a spacecraft to different respective target area locations in a non-uniform beam pattern, with at least some of said beams broadcast from different sized reflectors and having different beam roll-off characteristics, 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 peak-to-edge power differentials.

9. A spacecraft broadcast method, comprising:

broadcasting multiple communication signal beams from respective reflectors on 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 of said beams broadcast from different sized reflectors and having different beam roll-off characteristics, and

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

10. The method of claim 9, 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.

11. The method of claim 9, wherein at least some of said beams are broadcast to produce different beam powers at their respective target area locations.

12. The method of claim 11, wherein said at least some beams are braodcast from the spacecraft with different respective beam powers.

13. The method of claim 9, wherein at least some of said beams with different signal frequency spectrums are broadcast to overlapping target area locations.

14. The method of claim 9, wherein at least some of said beams are broadcast with different respective signal bandwidths.

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

16. A spacecraft broadcast method, comprising:

broadcasting multiple communication signal beams from respective reflectors on a spacecraft to different respective target area locations with at least some of said beams having different beam powers at their respective target area locations, and at least some of said beams broadcast from different sized reflectors and having different beam roll-off characteristics, and

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

17. The method of claim 16, wherein said at least some beams are broadcast from the spacecraft with different respective beam powers.

18. The method of claim 16, 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.

19. The method of claim 16, wherein at least some of said beams with different frequency bands are broadcast to overlapping target area locations.

20. The method of claim 16, wherein at least some of said beams are broadcast with different respective signal bandwidths.

21. The method of claim 16, wherein at least some of said beams are broadcast with different peak-to-edge power differentials.

22. A spacecraft broadcast method, comprising:

broadcasting multiple communication signal beams from respective reflectors on 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, with at least some of said beams broadcast from different sized reflectors and having different beam roll-off characteristics, and

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

23. The method of claim 22, wherein at least some of said beams are broadcast to produce different beam powers at their respective target area locations.

24. The method of claim 23, wherein said at least some beams are broadcast from the spacecraft with different respective beam powers.

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

26. The method of claim 22, wherein at least some of said beams are broadcast with different peak-to-edge power differentials.

27. A spacecraft broadcast method, comprising:

broadcasting multiple communications signal beams from a spacecraft to different respective target area locations in a non-uniform beam pattern, with at least some of said beams broadcast with different design peak-to-edge power differentials, and

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

28. The method of claim 27, 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.

29. The method of claim 27, wherein at least some of said beams have different sizes at their respective target area locations.

30. The method of claim 27, wherein at least some of said beams are broadcast to produce different beam powers at their respective target area locations.

31. The method of claim 30, wherein said at least some beams are broadcast from the spacecraft with different respective beam powers.

32. The method of claim 27, wherein at least some of said beams with different signal frequency spectrums are broadcast to overlapping target area locations.

33. The method of claim 27, wherein at least some of said beams are broadcast with different respective signal bandwidths.

34. The method of claim 27, wherein at least some of said beams are broadcast with different beam roll-off characteristics.

35. 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 of said beams broadcast with different design peak-to-edge power differentials, and

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

36. The method of claim 35, 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.

37. The method of claim 35, wherein at least some of said beams are broadcast to produce different beam powers at their respective target area locations.

38. The method of claim 37, wherein said at least some beams are broadcast from the spacecraft with different respective beam powers.

39. The method of claim 35, wherein at least some of said beams with different signal frequency spectrums are broadcast to overlapping target area locations.

40. The method of claim 35, wherein at least some of said beams are broadcast with different respective signal bandwidths.

41. The method of claim 35, wherein at least some of said beams are broadcast with different beam roll-off characteristics.

42. A spacecraft broadcast method, comprising:

broadcasting multiple communication signal beams from a spacecraft to different respective target area locations with at least some of said beams having different beam powers at their respective target area locations, and at least some of said beams broadcast with different design peak-to-edge power differentials, and

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

43. The method of claim 42, wherein said at least some beams are broadcast from the spacecraft with different respective beam powers.

44. The method of claim 42, 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.

45. The method of claim 42, wherein at least some of said beams with different frequency bands are broadcast to overlapping target area locations.

46. The method of claim 42, wherein at least some of said beams are broadcast with different respective signal bandwidths.

47. The method of claim 42, wherein at least some of said beams are broadcast with different beam roll-off characteristics.

48. 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, with at least some of said beams broadcast with different design peak-to-edge power differentials, and

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

49. The method of claim 48, wherein at least some of said beams are broadcast to produce different beam powers at their respective target area locations.

50. The method of claim 49, wherein said at least some beams are broadcast from the spacecraft with different respective beam powers.

51. The method of claim 48, wherein at least some of said beams are broadcast with different respective signal bandwidths.

52. The method of claim 48, wherein at least some of said beams are broadcast with different beam roll-off characteristics.