MODULAR DIGITAL PROCESSING SYSTEM FOR TELECOMMUNICATIONS SATELLITE PAYLOADS

• US 20110110401A1
• Filed: 04/17/2009
• Published: 05/12/2011
• Est. Priority Date: 04/18/2008
• Status: Active Grant

• Current Assignee: Astrium Limited (Airbus SE)
• Original Assignee: Astrium Limited (Airbus SE)
• Inventors: Craig, Anthony Duncan, Leong, Chiok Keng, Cornfield, Paul Simon
• Granted Patent: US 8,634,414 B2
• Time in Patent Office: Days
• US Class Current: 375/211
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays

Abstract

A telecommunications satellite payload processing system having one or more identical generic integrated processor modules is provided. The number of integrated processor modules can be selected in accordance with the antenna and bandwidth characteristics of a specified mission uplink and downlink in relation to the characteristics of the integrated processor module.

Claims

1. A telecommunications satellite payload processing system comprising one or more identical generic integrated processor modules, wherein the number of integrated processor modules is selected in accordance with the antenna and bandwidth characteristics of a specified mission uplink and downlink in relation to characteristics of the integrated processor module and wherein each integrated processor module contains a digital processing stage comprising:

a plurality of input ports adapted to receive signals corresponding to an uplink, each input port having a predetermined bandwidth;

a plurality of output ports adapted to output signals corresponding to a downlink, each output port having a predetermined bandwidth;

an A/D converter associated with each input port and arranged to convert an uplink signal of a predetermined bandwidth to digital sample form;

a D/A converter associated with each of the output ports and arranged to convert a processed digital signal of a predetermined bandwidth to an analogue downlink signal;

a plurality of frequency demultiplexers, each connected to one or more of the plurality of A/D converters and arranged to separate a sampled bandwidth of one or more of the sampled uplink signals into a plurality of channels;

a channel level processing stage associated with each of the channels and arranged to route processed channels to any of the plurality of output ports; and

a plurality of frequency multiplexers, each connected to the channel level processing stage and to one or more of the plurality of D/A converters and arranged to combine a plurality of routed channels.

2. A telecommunications satellite payload processing system according to claim 1,

wherein the number of individual integrated processor modules in the telecommunications satellite payload processing system is a function of the uplink and downlink antenna ports and the respective uplink and downlink bandwidth relative to the number of input (N) and output (M) ports and a respective input and output port bandwidth of the digital processor stage.

3. A telecommunications satellite payload processing system according to claim 1, wherein each integrated processing module comprises:

at least one out of a pre-processing stage and a post-processing stage.

4. A telecommunications satellite payload processing system, according to claim 1, wherein the channel level processing stage of the digital processor stage comprises:

a spatial switch system for flexibly routing a given input channel to one or more of the frequency multiplexers associated with the output ports.

5. A telecommunications satellite payload processing system, according to claim 1, wherein the channel level processing stage of the digital processor stage comprises:

a beam-forming network system.

6. A telecommunications satellite payload processing system according to claim 1, wherein the channel level processing stage of the digital processor stage comprises:

a memory switch arranged to provide flexible routing between uplink and downlink frequency slots.

7. A telecommunications satellite payload processing system, according to claim 1, wherein each integrated processor module comprises:

a pre-processing stage and the pre-processing stage is associated with the plurality of input ports of the digital processor module and is arranged to isolate a predetermined frequency band from the uplink, to down-convert the isolated band to an intermediate frequency and to apply a down-converted signal to one or more of the plurality of input ports.

8. A telecommunications satellite payload processing system, according to claim 7, wherein the pre-processing stage comprises:

a pre-processing chain associated with each of the input ports.

9. A telecommunications satellite payload processing system, according to claim 7, wherein the pre-processing stage comprises:

multiple pre-processor chains, outputs of which may be frequency multiplexed to provide predetermined input signals to one or more of the input ports.

10. A telecommunications satellite payload processing system according to claim 1, wherein each integrated processor module comprises:

a post-processing stage and the post-processing stage is associated with the plurality of outputs of the digital processor module and is arranged to filter and up-convert downlink signals to appropriate frequencies.

11. A telecommunications satellite payload processing system according to claim 10, wherein the post-processing stage of the integrated processor module comprises:

a post-processing chain associated with each of the output ports.

12. A telecommunications satellite payload processing system according to claim 10, wherein the post-processing stage of the integrated processor module comprises:

multiple post-processing chains characterised by different up-conversions and filtering.

13. A telecommunication satellite payload processing system according to claim 1, wherein each integrated processor module comprises:

both a pre-processing stage and a post-processing stage.

14. A telecommunications satellite payload processing system according to claim 1, wherein the integrated processor module is implemented in one of:

a mesh link, a forward link or a return link system architecture or a combination of these architectures.

15. A telecommunications satellite payload processing system according to claim 1, wherein the integrated processor module is arranged to operate with single feed per beam (SFPB) antennas on both uplink and downlink and wherein the integrated processor module interfaces to the antennas are beam ports.

16. A telecommunications satellite payload processing system according to claim 1, wherein a user link antenna is a phased array comprising:

a plurality of antenna elements.

17. A telecommunications satellite payload processing system according to claim 1, wherein a user link antenna is an array fed reflector (AFR) comprising:

a plurality of feeds offset from the focal plane of a reflector.

18. A telecommunications satellite payload digital processing system, according to claim 1, wherein the digital processor stage is implemented in a forward link system architecture and wherein a given input channel is split to provide signals to multiple output ports with channel samples being multiplied by complex coefficients in order to control downlink beam properties for that channel.

19. A telecommunications satellite payload digital processing system, according to claim 1, wherein the integrated processor module is implemented in a return link system architecture and wherein a given input channel is formed by summation signals from multiple input ports with channel samples being multiplied by complex coefficients in order to control uplink beam properties for that channel.

20. A telecommunications satellite payload processing system according to claim 1, wherein the uplink or downlink relate to ground terminals supporting a frequency multiplex of a plurality of channels.

21. A telecommunications satellite payload processing system according to claim 5, wherein each uplink or downlink channel is associated with a separate digital beam-forming network, with a sampled channel being split N_e or N_f ways corresponding to a number of elements/feeds on respective downlink or uplink antenna.

22. A telecommunications satellite payload processing system according to claim 20, wherein a bandwidth of the uplink or downlink is partitioned into a number of bandwidth segments, each segment being applied to or output from a single input or output port of the digital processor stage.

23. A telecommunications satellite payload processing system according to claim 1, wherein a signal corresponding to each uplink beam or antenna element/feed is applied to a single input port of the digital processor stage and/or a signal corresponding to each downlink beam or antenna element/feed is output from a single output port (22_1-M) of the digital processor stage.

24. A telecommunications satellite payload processing system according to claim 1, wherein a signal corresponding to a plurality of uplink beams or antenna elements/feeds;

is applied to a single input port of the digital processor stage and/or a signal corresponding to a plurality of downlink beams or antenna elements/feeds is output from a single output port of the digital processor stage.

25. A telecommunications satellite payload processing system according to claim 24, wherein each integrated processor module comprises:

both a pre-processing stage and a post-processing stage and the pre-processing stage is arranged to selectively down-convert the signals from the plurality of uplink beams or antenna elements/feeds to different centre frequencies and to sum down-converted beams or element/feed signals prior to applying to the signal to an input port of the digital processor stage.

26. A telecommunications satellite payload processing system according to claim 25, wherein the post-processing stage of the integrated processor module is arranged to selectively up-convert a signal from an output port of the digital processor stage to a plurality of downlink beams or antenna element/feeds.

27. A telecommunications satellite payload processing system according to claim 1, comprising:

a plurality of integrated processor modules, wherein signals corresponding to a subset of a plurality of uplink beams or antenna elements or feeds are applied to the input ports of the digital processor stage of each module and/or signals corresponding to a subset of a plurality of downlink beams or antenna elements or feeds are output from the output ports of the digital processor stage of each module.

28. A telecommunications satellite payload processing system according to claim 1, comprising:

a plurality of integrated processor modules, wherein signals corresponding to an entire plurality of uplink beams or antenna elements or feeds are applied to the input ports of the digital processor stage of each module and/or signals corresponding to an entire plurality of downlink beams or antenna elements or feeds are output from the output ports of the digital processor stage of each module, and wherein each module is arranged to process a different segment of an overall beam or antenna element or feed bandwidth.

29. A telecommunications satellite payload processing system according to claim 1, comprising:

a plurality of integrated processor modules, wherein signals corresponding to predetermined frequency bandwidth segments of uplink beams or antenna elements or feeds are applied to the input ports of the digital processor stage of each module and/or signals corresponding to an entire plurality of downlink beams or antenna elements or feeds are output from the output ports of the digital processor stage of each module, and wherein each module is arranged to process a different segment of an overall beam or antenna element or feed bandwidth.

30. A telecommunications satellite payload processing system according to claim 1, comprising:

a plurality of processor modules, wherein each of the uplink beam signals is split into multiple identical paths which are input to the respective input ports of the digital processor stage of each module and wherein a subset of the downlink beams is associated with each module.

31. A telecommunications satellite payload processing system according to claim 1, comprising:

a plurality of processor modules, wherein a subset of the uplink beam signals are associated with each module and wherein downlink beam signals from respective output ports of the digital processor stage of each module are summed together.

32. A telecommunications satellite payload processor according to claim 1 wherein one or more of the input ports and/or output ports of the digital processor stage of the integrated processor module are redundant.