Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information

• US 7,188,007 B2
• Filed: 12/24/2003
• Issued: 03/06/2007
• Est. Priority Date: 12/24/2003
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Gunn, Peter D., Mumaw, Randall J., Griffin, John C. III, Boorman, Daniel J.
• Primary Examiner(s): ARTHUR JEANGLAUDE, GERTRUDE
• Application Number:
  US10/746,912
• Publication Number:
  US 20050143871A1
• Time in Patent Office: 1,168 Days
• Field of Search: 701 3- 4, 701/11, 701 14- 16, 701120-122, 340/945, 340/947, 340971-980, 244/75.1, 244/76.R, 244/183, 244189-190
• US Class Current: 701/3
• 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: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00

Abstract

Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.

Claims

1. A computer-implemented method for controlling an aircraft, comprising:

displaying at least one first indicator to an operator of an aircraft, the at least one first indicator corresponding to at least one first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator, the first indicator corresponding to a first type of manuever directed to a first target; and

displaying at least one second indicator to the operator, the at least one second indicator corresponding to at least one second instruction for directing a second aircraft behavior at least approximately the same as the first aircraft behavior, the at least one second instruction to be automatically implemented at a future time, the at least one second indicator being at least approximately the same as the at least one first indicator and corresponding to a second type of maneuver at least generally similar to the first type of maneuver directed to a second target different than the first target.

2. The method of claim 1 wherein displaying at least one first indicator includes displaying at least one first indicator corresponding to any aircraft behavior mode or submode selectable by the operator.

3. The method of claim 1 wherein displaying at least one first indicator includes displaying an indicator identifying the behavior of the aircraft in a vertical direction.

4. The method of claim 1 wherein displaying at least one first indicator includes displaying an indicator identifying the behavior of the aircraft in a lateral direction.

5. The method of claim 1 wherein displaying at least one first indicator includes displaying an indicator identifying the airspeed of the aircraft.

6. The method of claim 1 wherein displaying the at least one first indicator includes displaying an indicator identifying the direction of travel of the aircraft and a target to which the aircraft is directed.

7. The method of claim 1, further comprising automatically implementing the second instruction.

8. The method of claim 1, further comprising implementing the first instruction, and wherein implementing the first instruction includes automatically directing the aircraft to a target.

9. The method of claim 1, further comprising:

receiving an input from the operator to automatically implement the first instruction; and

automatically implementing the first instruction by automatically directing the aircraft to a target.

10. The method of claim 1, further comprising implementing the first instruction, and wherein implementing the first instruction includes displaying a guide by which the operator can manually fly the aircraft.

11. The method of claim 1 wherein displaying the at least one first indicator includes displaying the at least one first indicator on a mode control panel of the aircraft, and wherein displaying the at least one second indicator includes displaying the at least one second indicator on the mode control panel, the mode control panel including at least one input device positioned to receive control inputs from the operator, and wherein the method further comprises receiving at least one aircraft control input from the operator at the at least one input device.

12. The method of claim 1 wherein displaying the at least one first indicator includes displaying an identification of a mode for controlling the aircraft.

13. The method of claim 1 wherein displaying the at least one first indicator includes displaying a textual indicator.

14. The method of claim 1 wherein displaying the at least one first indicator includes displaying an identification of a mode and a submode for controlling the aircraft, the submode being one of a plurality of available submodes corresponding to the mode.

15. The method of claim 1 wherein displaying the at least one first indicator includes displaying at least one lateral indicator corresponding to an aspect of the lateral motion of the aircraft, at least one vertical indicator corresponding to an aspect of the vertical motion of the aircraft, and at least one speed indicator corresponding to an aspect of the speed of the aircraft.

16. An aircraft system including a computer-readable medium having contents that perform a method, comprising:

displaying at least one first indicator to an operator of an aircraft, the at least one first indicator corresponding to at least one first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator, the at least one first indicator corresponding to a first type of maneuver directed to a first target; and

displaying at least one second indicator to the operator, the at least one second indicator corresponding to at least one second instruction for directing a second aircraft behavior at least approximately the same as the first aircraft behavior, the at least one second instruction to be automatically implemented at a future time, the at least one second indicator being at least approximately the same as the at least one first indicator, the at least one second indicator corresponding to a second type of maneuver at least generally similar to the first type of maneuver directed to a second target different than the first target.

17. The system of claim 16 wherein the contents of the computer-readable medium are configured to display at least one first indicator to include at least one first indicator corresponding to any aircraft behavior mode or submode selectable by the operator.

18. The system of claim 16 wherein the contents of the computer-readable medium are configured to display at least one first indicator to include an indicator identifying the behavior of the aircraft in a vertical direction.

19. The system of claim 16 wherein the contents of the computer-readable medium are configured to display at least one first indicator to include an indicator identifying the behavior of the aircraft in a lateral direction.

20. The system of claim 16 wherein the contents of the computer-readable medium are configured to display the at least one first indicator to include an indicator identifying the direction of travel of the aircraft and a target to which the aircraft is directed.

21. The system of claim 16, further comprising a mode control panel, and wherein the contents of the computer-readable medium are configured to display the at least one first indicator at the mode control panel and display the at least one second indicator at the mode control panel, the mode control panel including at least one input device positioned to receive control inputs from the operator, and wherein the contents of the computer-readable medium are configured to receive at least one aircraft control input from the operator at the at least one input device.

22. The system of claim 16 wherein the contents of the computer-readable medium are configured to display the at least one first indicator to include an identification of a mode for controlling the aircraft.

23. The system of claim 16 wherein the contents of the computer-readable medium are configured to display the at least one first indicator to include a textual indicator.

24. The system of claim 16 wherein the contents of the computer-readable medium are configured to display the at least one first indicator to include an identification of a mode and a submode for controlling the aircraft, the submode being one of a plurality of available submodes corresponding to the mode.

25. The system of claim 16 wherein the contents of the computer-readable medium are configured to display the at least one first indicator to include at least one lateral indicator corresponding to an aspect of the lateral motion of the aircraft, at least one vertical indicator corresponding to an aspect of the vertical motion of the aircraft, and at least one speed indicator corresponding to an aspect of the speed of the aircraft.

26. A computer-implemented method for controlling an aircraft, comprising:

displaying at least one first indicator to an operator of an aircraft, the at least one first indicator corresponding to at least one tactical first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator; and

displaying at least one second indicator to the operator, the at least one second indicator corresponding to at least one strategic second instruction from a pre-determined flight plan for directing a second aircraft behavior at least approximately the same as the first aircraft behavior, the at least one second instruction to be automatically implemented at a future time, the at least one second indicator being at least approximately the same as the at least one first indicator.