Satellite communication system using RF power sharing for multiple feeds or beams in downlinks

• US 6,456,824 B1
• Filed: 09/14/1998
• Issued: 09/24/2002
• 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): LEGREE, TRACY MICHELLE
• Application Number:
  US09/152,331
• Time in Patent Office: 1,471 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.3, 455/19, 455/20, 455/25, 455/102, 455/103, 455/129, 455/427, 455/430, 455/23, 455/234.2, 330/124.R, 370/281, 370/320, 370/319, 370/316, 370/335, 370/323
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays
• CPC Class Codes: Y02D 30/70 in wireless communication networks

Abstract

A satellite communication system includes at least one spacecraft in geosynchronous orbit for providing 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 the spacecraft. The 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. Each transmitter includes a combiner for combining together a plurality of frequency translated signals and a power amplifier, such as a TWTA, for amplifying the combined plurality of frequency translated signals. An analysis is performed of how many transponder channels can be combined and power amplified in a single TWTA, or multiple paralleled TWTAs, and a determination is then made as to which feeds and/or beams have low data traffic and low required downlink power that makes then suitable candidates for combining their feeds and/or beams into a linearly driven TWTA(s). A reverse output multiplexer is used to separate the combined feeds and/or beams to the separate individual downlinks after the RF power amplification.

Claims

1. A communication system, comprising:

at least one spacecraft in geosynchronous orbit, said spacecraft providing 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 said beams for transmitting uplink signals to said spacecraft;

wherein

said spacecraft is comprised of a plurality of receivers for receiving a plurality of the uplink signals in separate channels in said beam from ground stations, 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 adapted to amplify a respective transmitted uplink signal and each channel amplifier being gain controlled by a corresponding one of said ground stations, and a plurality of transmitters for transmitting the plurality of downlink signals within the same beams as the corresponding uplink signals; and

wherein

each said transmitter is comprised of a combiner for combining together a selected plurality of frequency translated channel amplified signals and a power amplifier for amplifying the combined plurality of frequency translated channel amplified signals, and further comprising an output splitter for separating the amplified combined plurality of frequency translated channel amplified signals into a plurality of downlink signals in a plurality of said beams.

2. A system as in claim 1, wherein said power amplifier is comprised of a linearly driven single TWTA or multiple paralleled TWTAs.

3. A system as in claim 2, wherein individual ones of the plurality of frequency translated signals are selected such that a sum of a maximum downlink RF power will not exceed the power handling capability and linearity of said single TWTA or multiple paralleled TWTAs.

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

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

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

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

8. A system as in claim 7, wherein said beams are spot beams having non-uniform sizes and shapes, and wherein individual ones of said spot beams overlie a predetermined one of a designated television market area.

9. The system of claim 1 wherein each channel amplifier provides approximately 50 db of gain to each frequency translated uplink signal.

10. The system of claim 1 wherein each ground station has separate RF control of its respective uplink signal.

11. The system of claim 1 wherein multiple ground stations are located within a single spot beam.

12. A method of power sharing in a satellite communication system comprising the steps of:

receiving a plurality of uplink signals from individual ground stations located in a beam of a satellite,

separating the uplink signals in each beam into into a transponder channel;

channel amplifying each transponder channel dependent on a control signal received from a corresponding ground station;

combining a plurality of beams of the satellite, each beam including a plurality of selected uplink signals from fixed users in a designated local to local closed system spot beam area, each selected uplink signal being assigned to a predetermined transponder channel that does not interfere with another selected uplink signal, wherein the signals in each beam are processed as a group;

feeding the combined plurality of beams to a single power amplifier, wherein a sum of a maximum RF power for a plurality of corresponding downlink signals for the beams selected to be combined does not exceed a power handling capability of the power amplifier;

separating the combined feeds into the plurality of downlink signals, each downlink signal assigned to the predetermined channel of the corresponding uplink channel; and

transmitting the individual downlink signals in the plurality of beams.

13. A communication system using a geostationary earth orbit satellite comprising:

at least one spacecraft in geosynchronous orbit, said spacecraft providing a plurality of beams on the surface of the earth; and

a plurality of fixed ground stations, individual ones of which are located in one of said beams for transmitting uplink signals to said spacecraft, wherein the system comprises a local to local closed system, and each fixed ground station

is located within a designated closed system spot beam area; and

wherein

said spacecraft is comprised of a plurality of receivers for receiving a plurality of the uplink signals in separate channels in said beam from ground stations, 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 adapted to amplify a respective transmitted uplink signal and each channel amplifier being gain controlled by a corresponding one of said ground stations, and a plurality of transmitters for transmitting the plurality of downlink signals within the same beams as the corresponding uplink signals; and

wherein

each said transmitter is comprised of a combiner for combining together a selected plurality of frequency translated channel amplified signals and a power amplifier for amplifying the combined plurality of frequency translated channel amplified signals, and further comprising an output splitter for separating the amplified combined plurality of frequency translated channel amplified signals into a plurality of downlink signals in a plurality of said beams.

14. A satellite communication system comprising:

at least one spacecraft providing a plurality of downlink beams on the surface of the earth;

a plurality of ground stations, multiple ground stations located in each of the beams, each ground station adapted to transmit and gain control an uplink signal transmitted from the ground station to the spacecraft, wherein each spacecraft comprises;

a plurality of receivers for receiving each uplink signal, each receiver adapted to receive each uplink signal on a separate channel of the receiver;

a frequency translator for translating each received uplink signal to a transmission frequency of a corresponding downlink signal;

a separate channel amplifier for each channel of the receiver, each channel amplifier being individually gain controlled by the ground station corresponding to the received uplink signal;

a combiner for combining together a selected plurality of frequency translated, channel amplified uplink signals;

a single power amplifier adapted to amplify the combined plurality of frequency translated, channel amplified uplink signals; and

an output splitter for separating the amplified the combined plurality of frequency translated, channel amplified uplink signals into a plurality of downlink signals in the beams for transmission.

15. A method of satellite communication comprising the steps of:

combining a plurality of lower power downlink beams in a transponder channel;

summing the combined plurality of lower power downlink beams in a combiner;

amplifying the summed, combined plurality of lower power downlink beams in a linearized high powered amplifier;

separating out the power amplified beams into separate beams; and

transmitting each separate beam with an associated downlink antenna.

16. The method of claim 15 further comprising the step, prior to the combining step, of adjusting a gain of a particular transponder channel using a corresponding channel amplifier prior to combining the transponder channel with other transponder channels, the gain being adjusted based on a control signal received from a corresponding ground station.

17. The method of claim 15 further comprising the step of monitoring a resulting downlink beam and compensating for any signal impairment by transmitting a signal amplification control signal from a corresponding ground station to a corresponding channel amplifier in the transponder channel.

18. The method of claim 15 further comprising the steps, prior to the step of summing of, determining the number of ground stations that can share a common TWTA and assigning a separate channel amplifier to each ground station.

19. The method of claim 15 further comprising the step of assigning a separate channel amplifier for each ground station, wherein multiple ground stations share a TWTA.

20. The method of claim 15 wherein the step of summing further comprises the step of using input multiplexers to sum signals arriving from the beams, wherein a use of a same transponder channel in a same input multiplexer is avoided and a summed output is transmitted to a single receiver.