Bus fault detection and isolation

• US 20060085692A1
• Filed: 10/05/2005
• Published: 04/20/2006
• Est. Priority Date: 10/06/2004
• Status: Abandoned Application

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Bestle, Edward R., Berbaum, Richard
• Application Number:
  US11/242,855
• Publication Number:
  US 20060085692A1
• Time in Patent Office: Days
• US Class Current: 714/43
• CPC Class Codes: G06F 11/2007 using redundant communication media
• CPC Class Codes: G06F 11/27 Built-in tests

Abstract

A bus fault detection and isolation system and method is disclosed that can operate non-intrusively to detect and isolate faults in a bus, such as a dual redundant MIL STD 1553 bus. The system and method of the present invention can be configured to operate within a bus controller using existing system commands and variables defined for testing. No additional equipment may be needed to utilize the bus fault detection and isolation system and method, so no additional failure points are introduced and the bus is in an unmodified state while fault detection and isolation takes place. Further, the bus fault detection and isolation system and method of the present invention may use accumulator variables to detect an intermittent fault which may then be isolated later even if the fault condition is no longer present on the bus.

Claims

1. A computer system for non-intrusive MIL STD 1553 bus fault detection and isolation, said computer system comprising:

a processor; and

a memory including software instructions adapted to cause the computer system to perform the steps of;

defining a first bus variable for a first bus in a redundant bus pair, the first bus variable including a built-in-test flag for each remote terminal connected to the first bus;

defining a second bus variable for a second bus in the redundant bus pair, the second bus variable including a built-in-test flag for each remote terminal connected to the second bus;

determining whether a fault has occurred on the first bus or the second bus based on a comparison of the first and second bus variables;

determining one or more bus coupler test variables corresponding to each bus coupler connected to the first bus or the second bus;

evaluating the bus coupler test variable for a bus coupler disposed at a physical end of the first bus and the second bus;

grouping the bus coupler test variables into logical segments and determining if a fault has occurred within a segment of the first bus or the second bus;

comparing the bus coupler test variables corresponding to the first bus with the bus coupler variables corresponding to the second bus in order to isolate a fault to a connection between a remote terminal and a first or second bus; and

comparing the built-in-test flags for each remote terminal for each of the first and second buses in order to isolate a fault to a connection between a remote terminal and a data bus coupler.

2. The computer system of claim 1, wherein the computer system is a bus controller and no additional apparatus is needed to detect and isolate faults on the bus.

3. The computer system of claim 1, wherein the software instructions further comprise creating one or more accumulator variables within the operating environment of a bus controller, each accumulator variable corresponding to a remote terminal, wherein the accumulator variable is incremented when a fault occurs in the remote terminal that the accumulator variable corresponds to such that intermittent failures may be detected.

4. The computer system of claim 1, wherein built-in-test data is correlated with physical configuration in order to perform fault isolation using a physical configuration mapping.

5. The computer system of claim 4, wherein the logical address of each remote terminal is not necessary to detect and isolate a fault.

6. A bus fault isolation method comprising:

defining a first bus variable for a first bus in a redundant bus pair, the first bus variable including a built-in-test flag for each remote terminal connected to the first bus;

defining a second bus variable for a second bus in the redundant bus pair, the second bus variable including a built-in-test flag for each remote terminal connected to the second bus;

determining whether a fault has occurred on the first bus or the second bus based on a comparison of the first and second bus variables;

determining one or more bus coupler test variables corresponding to each bus coupler connected to the first bus or the second bus;

evaluating the bus coupler test variable for a bus coupler at a physical end of the first bus and the second bus;

grouping the bus coupler test variables into logical segments and determining if a fault has occurred within a segment of the first bus or the second bus;

comparing the bus coupler test variables corresponding to the first bus with the bus coupler variables corresponding to the second bus in order to isolate a fault to a connection between a remote terminal and a first or second bus; and

comparing the built-in-test flags for each remote terminal for each of the first and second buses in order to isolate a fault to a connection between a remote terminal and a data bus coupler.

7. The bus fault isolation method of claim 6, wherein the first bus and the second bus comprise two redundant buses in a 1553 dual redundant bus system.

8. The bus fault isolation method of claim 6, wherein the method is adapted to be performed on a bus controller and no additional apparatus is needed to detect and isolate faults on the bus.

9. The bus fault isolation method of claim 8, further comprising creating one or more accumulator variables within the operating environment of the bus controller, each accumulator variable corresponding to a remote terminal, wherein the accumulator variable is incremented when a fault occurs in the remote terminal that the accumulator variable corresponds to such that intermittent failures may be detected.

10. The bus fault isolation method of claim 6, further comprising correlating built-in-test data with a physical configuration in order to perform fault isolation using a physical configuration mapping.

11. The bus fault isolation method of claim 6, wherein the logical address of each remote terminal is not necessary to detect and isolate a fault.

12. The bus fault isolation method of claim 6, further comprising determining that a fault has occurred on the first bus or the second bus.

13. A computer program product for bus fault detection and isolation, said computer program product comprising:

software instructions for enabling the computer to perform predetermined operations; and

a computer readable medium bearing the software instructions;

the predetermined operations including the steps of;

defining a first bus variable for a first bus in a redundant bus pair, the first bus variable including a built-in-test flag for each remote terminal connected to the first bus;

defining a second bus variable for a second bus in the redundant bus pair, the second bus variable including a built-in-test flag for each remote terminal connected to the second bus;

determining whether a fault has occurred on the first bus or the second bus based on a comparison of the first and second bus variables;

determining one or more bus coupler test variables corresponding to each bus coupler connected to the first bus or the second bus;

evaluating the bus coupler test variable for a bus coupler at a physical end of the first bus and the second bus;

grouping the bus coupler test variables into logical segments and determining if a fault has occurred within a segment of the first bus or the second bus;

comparing the bus coupler test variables corresponding to the first bus with the bus coupler variables corresponding to the second bus in order to isolate a fault to a connection between a remote terminal and a first or second bus; and

comparing the built-in-test flags for each remote terminal for each of the first and second buses in order to isolate a fault to a connection between a remote terminal and a data bus coupler.

14. The computer program product of claim 13, wherein the first bus and the second bus comprise two redundant buses in a MIL STD 1553 dual redundant bus system.

15. The computer program product of claim 13, wherein the computer program product is adapted to execute on a bus controller and no additional apparatus is needed to detect and isolate faults on the bus.

16. The computer program product of claim 15, further comprising creating one or more accumulator variables within the operating environment of the bus controller, each accumulator variable corresponding to a remote terminal, wherein the accumulator variable is incremented when a fault occurs in the remote terminal that the accumulator variable corresponds to such that intermittent failures may be detected.

17. The computer program product of claim 13, wherein the software instructions further comprise the step of correlating built-in-test data with a physical configuration in order to perform fault isolation using a physical configuration mapping.

18. The computer program product of claim 17, wherein the physical configuration mapping of built-in-test data permits fault detection and isolation such that a logical address of each remote terminal is not necessary to detect and isolate a fault.

19. The computer program product of claim 13, wherein the software instructions are configured to detect and isolate faults in real-time.

20. The computer program product of claim 19, wherein fault information is stored for later retrieval.