Fault tolerant lateral waypoint sequencing system and method

• US 9,254,911 B2
• Filed: 06/07/2013
• Issued: 02/09/2016
• Est. Priority Date: 06/07/2013
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Sheikh, Shiraz, Haberstock, James Kenneth, Lewis, Daniel E., Duffourd, Baptiste, Paricaud, Erwan
• Primary Examiner(s): To, Tuan C.
• Assistant Examiner(s): SMITH, ISAAC G
• Application Number:
  US13/912,551
• Publication Number:
  US 20140365037A1
• Time in Patent Office: 977 Days
• Field of Search: 701/3, 701/4, 701/466, 370/400, 370/401, 714/11
• US Class Current: 1/1
• CPC Class Codes: B64C 19/00 Aircraft control not otherwise provided for
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G05D 1/0077 using redundant signals or controls
• CPC Class Codes: G05D 1/0202 specially adapted to aircraft
• CPC Class Codes: G06F 11/0739 in a data processing system embedded in automotive or aircraft systems
• CPC Class Codes: G06F 11/16 Error detection or correction of the data by redundancy in hardware
• CPC Class Codes: G08G 5/0034 Assembly of a flight plan
• CPC Class Codes: G08G 5/0039 Modification of a flight plan

Abstract

Fault-tolerant lateral waypoint sequencing is provided for a system that includes at least a first flight management computer and a second flight management computer. A processing operation associated with lateral leg sequencing of an aircraft flight plan is implemented in the flight management computers. A determination is made in the first flight management computer as to whether the first flight management computer has received, within a predetermined period of time from when the first flight management computer implemented the processing operation, a notification from the second flight management computer that the second flight has also implemented the processing operation. An action is initiated in the first flight management computer when the first flight management computer has not received the notification from the second flight management computer within the predetermined period of time.

Claims

1. A method of providing fault-tolerant lateral waypoint sequencing in a system comprising at least a first flight management computer and a second flight management computer, the method comprising the steps of:

implementing, in the first flight management computer, a processing operation associated with lateral leg sequencing of an aircraft flight plan;

implementing, in the second flight management computer, the processing operation associated with lateral leg sequencing of an aircraft flight plan;

determining, in the first flight management computer, if the first flight management computer has received, within a predetermined period of time from when the first flight management computer implemented the processing operation, a notification from the second flight management computer that the second flight management computer has also implemented the processing operation; and

initiating an action, in the first flight management computer, when the first flight management computer has not received the notification from the second flight management computer within the predetermined period of time,

wherein the second flight management computer implements the processing operation associated with lateral leg sequencing of an aircraft flight plan without first receiving a request from the first flight management computer to implement the processing operation.

2. The method of claim 1, wherein the step of initiating an action comprises generating a request that causes the first and second flight management computers to operate in independent mode.

3. The method of claim 1, further comprising:

initiating a timer, in the first flight management computer, upon implementing the processing operation.

4. The method of claim 1, wherein the processing operation comprises at least determining that leg sequencing conditions have been met to process a lateral leg sequence of the aircraft flight plan.

5. The method of claim 4, wherein the processing operation further comprises processing the lateral leg sequence of the aircraft flight plan, and wherein the method further comprises:

transmitting the notification from the second flight management computer to the first flight management computer when the second flight management computer has processed the lateral leg sequence.

6. The method of claim 5, wherein the notification transmitted from the second flight management computer is a second notification, and wherein the method further comprises:

transmitting a first notification from the first flight management computer to the second flight management computer when the first flight management computer has processed the lateral leg sequence.

7. The method of claim 4, further comprising:

processing the lateral leg sequence of the aircraft flight plan in the second flight management computer upon receipt of the first notification.

8. The method of claim 1, wherein the processing operation comprises processing the lateral leg sequence of the aircraft flight plan.

9. The method of claim 8, further comprising:

initiating a first timer, in the first flight management computer, when the first flight management computer implements the processing operation; and

initiating a second timer, in the second flight management computer, when the second flight management computer implements the processing operation.

10. The method of claim 1, further comprising:

determining that the first and second flight management computers have both implemented the processing operation within the predetermined period of time; and

issuing a lateral leg sequence event from the first flight management computer that causes the first and second flight management computers to simultaneously sequence an active lateral leg.

11. The method of claim 1, further comprising:

computing, in the first flight management computer, cross track error and track angle error relative to a new flight plan leg associated with the lateral leg sequencing.

12. A flight management system that provides fault-tolerant lateral waypoint sequencing, comprising:

a first flight management computer configured to implement a processing operation associated with lateral leg sequencing of an aircraft flight plan; and

a second flight management computer in communication with the first flight management computer, the second flight management computer configured to also implement the processing operation and, upon implementing the processing operation, to transmit a notification to the first flight management computer,

wherein;

the first flight management computer is further configured to initiate an action when the first flight management computer has not received the notification from the second flight management computer within a predetermined period of time from when the first flight management computer implemented the processing operation, and

the second flight management computer implements the processing operation associated with lateral leg sequencing of an aircraft flight plan without first receiving a request from the first flight management computer to implement the processing operation.

13. The system of claim 12, wherein the action that is initiated comprises generating a request to operate the first and second flight management computers in independent mode.

14. The system of claim 12, wherein the first flight management computer is further configured to initiate a timer upon implementing the processing operation.

15. The system of claim 12, wherein the processing operation comprises at least determining that leg sequencing conditions have been met to process a lateral leg sequence of the aircraft flight plan.

16. The system of claim 15, wherein:

the processing operation further comprises processing the lateral leg sequence of the aircraft flight plan; and

the second flight management computer is further configured to transmit the notification to the first flight management computer when the second flight management computer has processed the lateral leg sequence.

17. The system of claim 16, wherein:

the notification transmitted from the second flight management computer is a second notification; and

the first flight management computer is further configured to transmit a first notification to the second flight management computer when the first flight management computer has processed the lateral leg sequence.

18. The system of claim 15, wherein the second flight management computer is further configured to process the lateral leg sequence of the aircraft flight plan upon receipt of the first notification.

19. The system of claim 12, wherein the processing operation comprises processing the lateral leg sequence of the aircraft flight plan.

20. The system of claim 19, wherein:

the first flight management computer is further configured to initiate a first timer when the first flight management computer implements the processing operation; and

the second flight management computer is further configured to initiate a second timer when the second flight management computer implements the processing operation.

21. The system of claim 12, wherein:

the first and second flight management computers are further configured to determine that the first and second flight management computers have both implemented the processing operation within the predetermined period of time; and

the first flight management computer is further configured to issue a lateral leg sequence event that causes the first and second flight management computers to simultaneously sequence an active lateral leg.

22. The system of claim 12, wherein the first flight management computer is further configured to compute cross track error and track angle error relative to a new flight plan leg associated with the lateral leg sequencing.