Self diagnosis and self healing scheme for digital beam-forming

• US 6,084,541 A
• Filed: 07/13/1998
• Issued: 07/04/2000
• Est. Priority Date: 07/13/1998
• Status: Expired due to Term

• Current Assignee: Vizada Incorporated (Airbus SE)
• Original Assignee: COMSAT Corporation (Reorganized ISA SA)
• Inventors: Sayegh, Soheil I.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US09/114,495
• Time in Patent Office: 722 Days
• Field of Search: 342/352, 342/354, 342/373, 455/8, 455/428, 455/450, 455/452
• US Class Current: 342/354
• CPC Class Codes: H01Q 3/26 varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture H01Q3/12, H01Q3/22, H01Q3/24 take precedence
• CPC Class Codes: H04B 7/18519 Operations control, administration or maintenance

Abstract

A completely autonomous failure recovery scheme for digital beam forming that provides self-diagnosis and self-healing of faulty processing chains in a communications satellite payload. A baseline processor comprises a plurality of processing chains that are identical in hardware and differ only in software. A redundant chain is programmed identically to the first processing chain by downloading the appropriate software coefficients from a controller. The first chain is then selected by a SELECT logic component its output is compared by a COMPARE logic component to the output of the redundant chain. In the absence of malfunctions, the two outputs should be identical. If the two outputs are not identical, the chain is diagnosed as faulty and it is replaced by a "hot" standby redundant chain. Further, a control signal from the diagnosis module alters the position of at least one output switch to disconnect the faulty module. The redundant chain is then programmed identically to the second processing chain and the outputs are compared to determine whether the chain is faulty. The cycle repeats for each consecutive processing chain. This permits the identification of which chain, if any, is faulty. This scheme is completely autonomous providing both self-diagnosis and self-healing.

Claims

1. A payload for communications satellite having digital channelization and digital beam-forming comprising:

a plurality of processing chains each defined by respective signal processing coefficients;

a redundant chain that is programmable to have signal processing coefficients that are identical to a selected one of said plurality of processing chains; and

an analog to digital converter;

a demultiplexer coupled to the output of said analog to digital converter and a demultiplexer having an output that is coupled in common to said plurality of processing chains and said redundant chain;

wherein each of said plurality of processing chains and said redundant chain comprise;

digital beam-forming means;

a buffer coupled to the output of said digital beam-forming means; and

a remultiplexer coupled to the output of said buffer.

2. A payload for a communications satellite as defined in claim 1, wherein said digital beam forming means forms beams in desired directions by using a predetermined delay in each path of said array antenna elements of said array antenna.

3. A payload for a communications satellite having digital channelization and digital beam-forming comprising:

a plurality of processing chains each defined by respective signal processing coefficients;

a redundant chain that is programmable to have signal processing coefficients that are identical to a selected one of said plurality of processing chains;

a selection logic component, coupled to the outputs of said plurality of processing chains, for selecting the output of one of said plurality of processing chains; and

a comparing logic component, coupled to the outputs of said digital logic component and said redundant chain, for comparing the output of said one of said plurality of processing chains, selected by said selection logic component, with the output of said redundant chain, and determining whether the compared outputs are different.

4. A payload for a communications satellite as defined in claim 3, wherein said one of said plurality of processing chains, selected by said selection logic component, is diagnosed as a faulty processing chain when its output and said output of said redundant chain, compared in said logical component, are not identical.

5. A payload for a communications satellite as defined in claim 4, wherein said redundant chain is a hot standby redundant chain;

and further comprising switching means, connected to said hot standby redundant chain for disconnecting said faulty chain and replacing it with said hot standby redundant chain.

6. A payload for a communications satellite as defined in claim 4, further comprising a diagnosis module for generating a control signal upon diagnosis of said faulty processing chain so that said faulty processing chain is disconnected from at least one output switch.

7. A method for self diagnosis and self healing of a faulty processing chain, among a plurality of processing chains, in a communications satellite payload having a digital beam-forming network and at least one programmable redundant chain, said method comprising the steps of:

(a) programming a redundant chain of said payload to have parameters identical to one processing chain among said plurality of processing chains;

(b) selecting said one processing chain;

(c) comparing the output of said selected processing chain with the output of said redundant chain;

(d) judging whether the outputs of said processing chain and said redundant chain are identical;

(e) diagnosing said processing chain as faulty if said outputs are judged not to be identical in said step (d); and

(f) determining that there are no malfunctions in said processing chain if said outputs are judged to be identical in said step (d).

8. The method as claimed in claim 7, wherein said method further comprises the step (g) of replacing said one processing chain with a hot standby redundant chain if said processing chain is diagnosed as faulty in said step (e).

9. The method as claimed in claim 8, wherein said method further comprises the step of (h) of disconnecting said one processing chain from at least one output switch if said processing chain is diagnosed as faulty in said step (e).

10. The method as claimed in claim 8, wherein said method further comprises the step of (i) repeating said steps (a)-(h) for at least one other processing chain of said plurality of processing chains.

11. The method as claimed in claim 8, wherein said method further comprises the step of (i) repeating said steps (a)-(h) for all currently operational processing chains of said plurality of processing chains.