Phase array routing connectivity
A communication system has a control module with a control processing device, and a plurality of common modules. Each of the common modules has a common processing device. The control module and the plurality of common modules are connected with at least one adjacent common module to form a communication array. The control module and the common modules communicate via a first routing path having a first path of common modules of the plurality of common modules, and a second routing path having a second path of common modules of the plurality of common modules different than the first path of common modules. The control module and the plurality of common modules communicate via the second routing path when one of the first set of common modules fails.
1. A satellite module comprising:
an antenna;
a high-speed return link input for receiving return link data from a first adjacent satellite module connected to the satellite module by at least one wire;
a high-speed return link output for transmitting return link data to a second adjacent satellite module connected to the satellite module by at least one wire; and
a low-speed link for transmitting and receiving routing path commands when said high-speed return link input fails to receive return link data and/or said high-speed return link output fails to transmit return link data,
wherein the satellite module is connected to a control satellite module via the first adjacent satellite module, the second adjacent satellite module, or both, via a routing path;
wherein the satellite module, the first adjacent satellite module, the second adjacent satellite module, and the control satellite module are within a phased array of satellite modules, wherein the routing path allows the satellite module, the first adjacent satellite module and the second adjacent satellite module to communicate with the control satellite and wherein the routing path is updated when an active connection within the phased array fails.
2. The satellite module of claim 1 , further comprising:
a high-speed forward link input for receiving forward link data;
a high-speed forward link output for transmitting forward link data; and
the low-speed link transmitting and receiving commands when said high-speed forward link input fails to receive forward link data and/or said high-speed forward link output fails to transmit forward link data.
3. The satellite module of claim 1 , further comprising a processing device for receiving return link data on said high-speed return link input, aggregating the received return link data with return link data from said satellite module antennas, and transmitting the aggregated return link data on said high-speed return link output.
4. The satellite module of claim 2 , said processing device receiving forward link data on said high-speed forward link input, transmitting the received forward link data over its antennas, and transmitting a copy of the received forward link data on said high-speed forward link output.
5. A satellite module comprising:
an antenna;
a plurality of high-speed return link inputs each for receiving return link data from a first adjacent satellite module that is connected to the satellite module through at least one wire;
a plurality of high-speed return link outputs each for transmitting return link data to a second adjacent satellite module or a control satellite module that is connected to the satellite module by at least one wire;
a plurality of high-speed forward link inputs each for receiving forward link data from the second adjacent satellite module or the control satellite module;
a plurality of high-speed forward link outputs each for transmitting forward link data to the first adjacent satellite module;
a low-speed link for transmitting and receiving routing path commands; and
a processing device determining if one of said plurality of high-speed return link inputs, said plurality of high-speed return link outputs, said plurality of high-speed forward link inputs, said plurality of high-speed forward link outputs, fails; and based on that determination, communicating forward link data and/or return link data over the low-speed link,
wherein the satellite module is connected to the control satellite module via the first adjacent satellite module, the second adjacent satellite module, or both, via a routing path;
wherein the satellite module, the first adjacent satellite module, the second adjacent satellite module, and the control satellite module are within a phased array of satellite modules, wherein the routing path allows the satellite module, the first adjacent satellite module and the second adjacent satellite module to communicate with the control satellite and wherein the routing path is updated when an active connection within the phased array fails.
6. The satellite module of claim 5 , further comprising a low-speed link reporting receiving a return link routing path and a forward link routing path and/or reporting a failure to a control satellite.
7. The satellite module of claim 5 , wherein said processing device determination is based on a return link routing path and a forward link routing path received from a control satellite.
8. The satellite module of claim 5 , said processing device receiving return link data on one or two of said plurality of high-speed return link inputs, aggregating the received return link data with return link data from said satellite module, and transmitting the aggregated return link data on one of said plurality of high-speed return link output.
9. The satellite module of claim 5 , said processing device receiving forward link data on said high-speed forward link input, sending the received forward link data over said antenna, and transmitting copies of the received forward link data on one or two said high-speed forward link outputs.
10. The satellite module of claim 5 , wherein said processing device determines which one of said plurality of high-speed return link inputs, said plurality of high-speed return link outputs, said plurality of high-speed forward link inputs, and said plurality of high-speed forward link outputs to communicate over based on a routing path.
11. The satellite module of claim 1 , wherein the first adjacent satellite module communicates with the satellite module through at least one wire.
12. The satellite module of claim 1 , wherein the first adjacent satellite module is physically connected to the satellite module.
13. The satellite module of claim 5 , wherein the first adjacent satellite module communicates with the satellite module through at least one wire.
14. The satellite module of claim 5 , wherein the first adjacent satellite module is physically connected to the satellite module.