Ground-based software tool for controlling redundancy management switching operations

• US 7,412,291 B2
• Filed: 01/12/2005
• Issued: 08/12/2008
• Est. Priority Date: 01/12/2005
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Judd, Thomas D., Kayser, Michael J.
• Primary Examiner(s): Pham; Thomas K
• Application Number:
  US10/905,608
• Publication Number:
  US 20060156053A1
• Time in Patent Office: 1,308 Days
• Field of Search: 700/21, 700/82, 714/2, 714/5, 714/6, 714/11, 701/43
• US Class Current: 700/21
• CPC Class Codes: G06F 11/2023 Failover techniques
• CPC Class Codes: G06F 11/2038 with a single idle spare processing component
• CPC Class Codes: G06F 11/2048 where the redundant components share neither address space nor persistent storage

Abstract

Systems, methods, and computer program products for easily altering redundancy management data values associated with redundancy management logic that is executed by redundant data processing systems. The redundancy management data values are altered on a computer device remote from the system that includes the redundant data processing systems.

Claims

1. A system comprising:

a device comprising;

at least two data processing systems arranged to perform redundant operations, wherein at least one of the at least two data processing systems serves as a master;

control logic arranged to determine which of the at least two data processing systems is a master; and

memory arranged for storing data values used by the control logic to determine which of the at least two data processing systems is a master; and

a computer configured to execute a ground based software tool, wherein the ground-based software tool includes a component configured to allow a user to change at least one of the stored data values used by the control logic to determine which of the at least two data processing systems is a master.

2. The system of claim 1, wherein the data values include weight values.

3. The system of claim 1, wherein the data values include time limit values.

4. The system of claim 1, wherein the data values include switching threshold values.

5. The system of claim 1, wherein the data values include weight values, time limit values, and switching threshold values.

6. The system of claim 1, wherein the device is an aircraft.

7. The system of claim 6, wherein the at least two redundant data processing systems include communication management units.

8. The system of claim 1, wherein the device is a communication system.

9. The system of claim 1, wherein the computer stores data values on a removable storage device, the device further includes a data loader for receiving the removable storage device and storing the data values on the storage device into the memory.

10. A method comprising:

altering at least one redundancy management data value associated with redundancy management logic at a computer;

saving the altered data value on a removable storage device;

sending the at least one altered redundancy management data value from the removable storage device to memory included in an apparatus, wherein (1) the apparatus includes at least two data processing systems, (2) at least one of the at least two data processing systems serves as a master, and (3) the at least two data processing systems perform redundant operations and execute redundancy management based on the one or more redundancy management data values stored in the memory; and

using the at least one altered redundancy management data value to determine which of the at least two data processing systems serves as a master.

11. The method of claim 10, wherein the redundancy management data values include weight values.

12. The method of claim 10, wherein the redundancy management data values include time limit values.

13. The method of claim 10, wherein the redundancy management data values include switching threshold values.

14. The method of claim 10, wherein the redundancy management data values include weight values, time limit values, and switching threshold values.

15. The method of claim 10, wherein the apparatus is an aircraft.

16. The method of claim 15, wherein the at least two redundant data processing systems include communication management units.

17. The method of claim 10, wherein the apparatus is a communication system.

18. The method of claim 10, further comprising:

receiving the removable storage device at a data loader of the apparatus; and

storing the data values on the storage device into the memory.

19. The method of claim 10, wherein the at least one redundancy management data value includes weight values, time limit values, and switching threshold values.