Satellite communications system and method therefor

• US 4,689,625 A
• Filed: 11/06/1984
• Issued: 08/25/1987
• Est. Priority Date: 11/06/1984
• Status: Expired due to Fees

• Current Assignee: Martin Marietta Corporation
• Original Assignee: Martin Marietta Corporation
• Inventors: Barmat, Melvin
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): Hayes, Jr., Donald E.
• Application Number:
  US06/668,849
• Time in Patent Office: 1,022 Days
• Field of Search: 343/353, 343/356, 343/361-365, 342/353, 342/356, 342/361-365
• US Class Current: 342/356
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

A satellite communications system and method of communication which results in increased frequency-reusage within assigned frequency bands and allows for a reduction in satellite transponder requirements per unit of bandwidth employed. The disclosed system employs a satellite in a geostationary orbit having transponders and one or more large-aperture, high-gain antennas that provide a broad-area beam for a relatively wide service area and for transmitting to and receiving signals from N narrow-area beams for N respective sub-areas, the sub-areas corresponding to the high-traffic nodes. Both beam types operate in the same allocated frequency bands but with opposite linear or opposite handed circular polarizations, or, alternatively, with arbitrarily determined portions of the allocated frequency band pairs with dual polarization so that the allocated frequency spectrum is used at least N+1 times. Since the narrow-area beams provide a substantially smaller illumination pattern than the broad-area beam, substantially less power is required to form each narrow-area beam at the satellite antenna so that each additional narrow-area beam results in a frequency reuse with only a relatively small incremental increase in drive power requirements. Because of the reduced incremental satellite power requirements associated with the multiple additional frequency reusages, the high power amplifiers (HPA'"'"'s) of the satellite transponders for the narrow-area beams can be backed-off from non-linear operation into their linear regions to allow multiple signal carrier amplification in each HPA to thus reduce the total HPA requirements for the system.

Claims

1. A satellite communications system comprising:

a communications satellite in a geostationary orbit above the earth'"'"'s surface, said satellite having transponder means and antenna means, said antenna means for receiving multiple carrier up-link transmissions from the earth and for directing down-link transmissions to the earth, the up-link and down-link transmissions allocated frequency bands of selected bandwidth, the down-link transmissions including transmissions of selected carriers in a broad-area beam polarized in a first alignment for illuminating a selected service area and transmissions of selected carriers in at least N narrow-area beams polarized in a second alignment for illuminating selected sub-areas within the service area, said transponder means including signal processing means for processing received up-link transmissions for down-link transmission to the earth, said signal processing means inlcuding band pass filter means for dividing the received up-link transmissions into frequency-distinct signal carriers, signal carrier combining means for combining selected of the frequency-distinct signal carriers and providing the selected carriers to a signal carrier amplifier means that includes high power amplifier means operable in a linear region and in a non-linear region, at least two signal carriers for transmission in one of said at least N narrow-area beams being amplified by a high power amplifier means operating in its linear regions and a signal carrier for broad-area down-link transmission being amplified by a high power amplifier means operting in its non-linear region.

2. The satellite communications system of claim 1, wherein said polarization alignments are linear.

3. The satellite communications system of claim 2, wherein said polarizations alignments are orthogonal.

4. The satellite communications system of claim 1, wherein said polarization alignments are circular.

5. The satellite communications system of claim 4, wherein said polarization alignments are of opposite hand.

6. The satellite communications system of claim 1, wherein said narrow-area beams include at least one narrow-area beam outside the broad-area beam service area.

7. The satellite communications system of claim 1, wherein said broad-area beam subtends approximately four by six degrees.

8. The satellite communications system of claim 1, wherein at least one of said narrow-area beams subtends between 0.3 and 0.8 degrees.

9. The satellite communications system of claim 1, wherein said down-link transmissions are in the 11.7 to 12.2 GHz band.

10. The satellite communications system of claim 1, wherein said up-link transmissions are in the 14.0 to 14.5 GHz band.

11. The satellite communications system of claim 1, wherein said narrow-area beam illumination patterns are separated sufficiently on the earth'"'"'s surface to minimize interference.