Satellite communication system employing unique spot beam antenna design

• US 6,496,682 B2
• Filed: 09/14/1998
• Issued: 12/17/2002
• Est. Priority Date: 09/14/1998
• Status: Expired due to Term

• Current Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Original Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Inventors: Butte, Eric G, Tyner, Randall D
• Primary Examiner(s): Urban, Edward F.
• Assistant Examiner(s): Mehrpour, Naghmeh
• Application Number:
  US09/152,555
• Publication Number:
  US 20020068526A1
• Time in Patent Office: 1,555 Days
• Field of Search: 455/429, 455/427, 455/428, 455/430, 455/12.1, 455/13.1, 455/13.4, 455/13.3
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays

Abstract

A satellite communication system includes a plurality of spacecraft in geosynchronous orbit, where each spacecraft provides a plurality of beams on the surface of the earth, and a plurality of ground stations individual ones of which are located in one of the beams for transmitting uplink signals to one of the spacecraft. Each spacecraft has a plurality of receivers for receiving a plurality of the uplinked signals from ground stations, a frequency translator for translating the received uplink signals to a transmission frequency of a plurality of downlink signals, and a plurality of transmitters for transmitting the plurality of downlink signals within the same beams as the corresponding uplink signals. In accordance with the invention the beams have at least one of different sizes and shapes, including circular and elliptical, and are non-contiguous over a least a portion of the surface of the earth.

Claims

1. A communication system, comprising:

a plurality of spacecraft in geosynchronous orbit, each spacecraft cooperating to provide a fixed plurality of beams on the surface of the earth; and

a fixed plurality of ground stations individual ones of which are located in one of said beams for transmitting uplink signals to one of said spacecraft;

wherein

each spacecraft is comprised of;

a plurality of input hybrids, each input hybrid being for receiving a plurality of the uplink signals from ground stations and for combining said uplink signals,

a plurality of receivers, a single receiver being coupled to an output of each input hybrid, each receiver being for receiving a combined plurality of uplink signals combined by one of said input hybrids, each receiver having a frequency translator for translating the received combined uplink signals to a transmission frequency of a plurality of downlink signals,

a plurality of channel amplifiers, a single channel amplifier being coupled to an output of an input multiplexer filter, an input of the input multiplexer filter being connected to an output of a respective receiver, each channel amplifier being for amplifying one of the downlink signals,

at least one output hybrid for combining a plurality of outputs of said channel amplifiers, and

a plurality of transmitters, each transmitter being for receiving an output from one of said hybrids and for transmitting the plurality of downlink signals within the same beams as the corresponding uplink signals.

2. A system as in claim 1, wherein each of said plurality of channel amplifiers is gain controlled by a corresponding one of said ground stations.

3. A system as in claim 1, wherein the portion of the surface of the earth is CONUS.

4. A system as in claim 1, wherein uplink beams to a first one of said satellites have a first polarization and downlink beams have a second, opposite polarization, and wherein uplink beams to a second one of said satellites have said second polarization and downlink beams have said first polarization.

5. A system as in claim 1, wherein the uplink and downlink signals comprise digital data signals.

6. A system as in claim 1, wherein the uplink and downlink signals comprise digital television signals.

7. A system as in claim 6, wherein individual ones of said spot beams overlie a predetermined one of a designated television market area.

8. A system as in claim 1, wherein each spacecraft is comprised of a plurality of different sized reflector antennas for both transmitting and receiving said beams.

9. A system as in claim 1, wherein each spacecraft is comprised of a plurality of reflector antennas for both transmitting and receiving said beams, wherein at least two of said reflector antennas have different shapes.

10. A system as in claim 1, wherein each spacecraft is comprised of a plurality of reflector antennas for both transmitting and receiving said beams, wherein said plurality of reflector antennas are each comprised of a Gregorian antenna.

11. A system as in claim 1, wherein each spacecraft is comprised of a plurality of reflector antennas for both transmitting and receiving said beams, wherein said plurality of reflector antennas are each comprised of a Cassegrain antenna.

12. A system as in claim 1, wherein uplink beams to a first one of said satellites have a right hand circular polarization (RHCP) and downlink beams have a left hand circular polarization (LHCP), and wherein uplink beams to a second one of said satellites have LHCP and downlink beams have RHCP.

17. A system as in claim 1, further comprising an output linearizer disposed between an output of each one of said output hybrids and one of said plurality of transmitters.

18. A system as in claim 1, wherein each of said transmitters is a linearized TWTA.

19. A system as in claim 1, wherein said beams have at least one of different sizes and shapes, and at least some of said beams are non-contiguous over a portion of the surface of the earth.

25. The communication system of claim 1 wherein each channel amplifier is associated with each ground station, wherein a gain of each channel amplifier is controlled by a respective ground station.

26. The communication system of claim 1 further comprising a multiplexer coupled to an output of each receiver, each multiplexer adapted to separate out one or a set of uplink signals associated with each ground station.

13. A communication satellite for providing a fixed plurality of beams on the surface of the earth and for receiving uplink signals from a fixed plurality of ground stations individual ones of which are located in one of said beams, said satellite comprising:

a plurality of input hybrids, each input hybrid being for receiving a plurality of the uplink signals from one or multiple ground stations per beam and for combining said uplink signals,

a plurality of receivers, each receiver being for receiving a plurality of uplink signals combined by one of said input hybrids, each input hybrid adapted to sum a selected plurality of uplink signals in order to fill an uplink spectrum, each receiver having a frequency translator for translating the received uplink signals to a transmission frequency of a plurality of downlink signals,

a plurality of channel amplifiers, each channel amplifier associated with each ground station and being for amplifying one or a set of said downlink signals associated with each ground station wherein a gain of each channel amplifier is controlled by a respective ground station,

at least one output hybrid for combining a plurality of outputs of said channel amplifiers, and

a plurality of transmitters for transmitting a plurality of amplified downlink signals within the same beams as the corresponding uplink signals.

14. A communication satellite as in claim 13, further comprising an output linearizer disposed between an output of each one of said output hybrids and one of said plurality of transmitters.

15. A communication satellite as in claim 13, wherein each of said transmitters is a linearized TWTA.

16. A communication satellite as in claim 13, wherein said beams have different sizes and one or both are of a circular shape or a non-circular shape, said wherein at least some of said plurality of beams are non-contiguous and non-overlapping over at least a portion of the surface of the earth.

20. A satellite communication system comprising:

a plurality of spacecraft in a geosynchronous orbit providing a plurality of beams on a surface of the earth;

a plurality of individual ground stations, each ground station located in one of the beams and adapted to transmit uplink signals to the spacecraft;

at least one input hybrid for combining a one or multiple ground stations per beam, each input hybrid including a multiplexer adapted to sum a selected plurality of uplink transponder signals in order to fill up an uplink spectrum of a receiver;

the receiver being coupled to an output of the input hybrid, each receiver adapted to frequency translate the sum of the selected plurality of uplink transponder signals into a transmission frequency of a downlink signal;

a multiplexer coupled to an output of each receiver, the multiplexer adapted to separate out one or a set of transponder signal associated with each ground station;

a channel amplifier associated with each ground station coupled to each output of the input multiplexer and adapted to amplify each one or set of transponder signals associated with each ground station, wherein a gain of each channel amplifier is controlled by a respective ground station; and

a plurality of transmitters for transmitting the plurality of amplified one or set of transponder signals within the same beams as the corresponding uplink transponder signals.

21. The system of claim 20 wherein each spot beam includes multiple ground station and each ground station has multiple transponder channels.

22. The system of claim 20 wherein the system comprises a first satellite and a second satellite using alternate spot beam locations between the two satellites to cover all designated market areas, the first satellite adapted to uplink signals in a right hand circular polarization and downlink in a lefthand circular polarization, the second satellite adapted to uplink in a left hand circular polarization and downlink in a right hand circular polarization.

23. The system of claim 20 wherein the input hybrid is adapted to sum multiple beams, each beam having one or multiple ground stations per beam, into each receiver in order to fill up each transponder channel in the receiver.

24. The system of claim 20 further comprising a high power amplifier coupled to the output of the output hybrid, the power amplifier adapted to amplify the transponders of each beam as a group before being transmitted by the transmitter.