EP0910180A2

Non-uniform multi-beam satellite communications system and method

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 (1,2,3,4) 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.

EP0910180A2, drawing sheet 1
Sheet 1 of 9

Term

Term ended

Projected expiry passed 19 October 2018, 7.9 years ago.

  1. Priority
  2. Filed
  3. Published
  4. Projected expiry
  5. Today

8 claims: 5 independent, 3 dependent

  1. 1
    A spacecraft broadcast method, comprising:broadcasting multiple communication signal beams (1,2,3,4) from a spacecraft (28) to different respective target area locations (26a,26b,26c,26d) in a non-uniform beam pattern, and providing different respective signal frequency spectrums (51,52,53,54) for at least some of said beams.
  2. 4
    The method of any of claims 1-3, wherein at least some of said beams are broadcast to produce different beam powers at their respective target area locations.
  3. 5
    The method of any of claims 1-4, wherein at least some of said beams are broadcast with different beam roll-off characteristics.
  4. 6
    The method of any of claims 1-5, wherein at least some of said beams are broadcast with different peak-to-edge power differentials.
  5. 7
    A spacecraft broadcast system for multi-beam broadcasts to earth, comprising:a spacecraft (28), a plurality of antenna reflectors (30a,30b,30c,30d) with respective feed horns (36a,36b,36c) carried by said spacecraft, and a power supply (56) and radio frequency (RF) signal circuitry (38a,38b) carried by said spacecraft for energizing said feed horns to broadcast respective communication signal beams (1,2, 3,4) to respective target area locations (26a, 26b,26c,26d) 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 some of said beams having different sizes.