Non-uniform multi-beam satellite communications system and method

• US 6,463,282 B2
• Filed: 04/16/2001
• Issued: 10/08/2002
• Est. Priority Date: 10/17/1997
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.), News America Incorporated (The Walt Disney Company)
• Original Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Inventors: Norin, John L., Pontual, Romulo, Rao, Sudhakar, Regulinski, Paul
• Primary Examiner(s): Maung, Nay
• Assistant Examiner(s): Persino, Raymond B.
• Application Number:
  US09/835,536
• Publication Number:
  US 20010036826A1
• Time in Patent Office: 540 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, 343/786, 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 antenna array for multi-beam broadcasts to earth, comprising:

a plurality of antenna reflectors, and

at least one respective feed horn associated with each reflector,

said antenna reflectors and their respective feed horns configured to broadcast a plurality of communication signal beams in a non-uniform beam pattern with at least first and second ones of said beams having different sizes and beam powers, a common frequency band, and spatially overlapping main lobes to produce and sustain a substantially greater non-zero cross-beam interference, relative to beam power, in a peripheral portion of the main lobe of said first beam than of said second beam.

2. A spacecraft broadcast system for multi-beam broadcasts to earth, comprising:

a spacecraft,

a plurality of antenna reflectors with respective feed horns carried by said spacecraft, and

a power supply and radio frequency (RF) signal circuitry carried by said spacecraft for energizing said feed horns to broadcast respective communication signal beams to respective target area locations on earth via their respective reflectors,

said antenna reflectors and their respective feed horns configured to broadcast said beams in a non-uniform beam pattern with at least first and second ones of said beams having different sizes, a common frequency band, and spatially overlapping main lobes on earth to produce and sustain a substantially greater non-zero cross-beam interference, relative to beam power, in a peripheral portion of the main lobe of said first beam than of said second beam,

said power supply and RF signal circuitry configured to energize said feed horns to broadcast said overlapping beams to produce different respective beam powers at their respective target area locations.

3. The spacecraft broadcast system of claim 2, wherein said power supply and RF signal circuitry energize said feed horns to broadcast at least some of said beams within different respective signal frequency spectrums.

4. The spacecraft broadcast system of claim 3, wherein said reflectors and feed horns are configured to broadcast at least some of said beams with different signal frequency spectrums to overlapping target area locations.

5. The spacecraft broadcast system of claim 2, wherein said reflectors and feed horns are configured to broadcast at least some of said beams with a common frequency band to non-overlapping target area locations.