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

• US 7,751,948 B2
• Filed: 12/14/2006
• Issued: 07/06/2010
• Est. Priority Date: 12/24/2003
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Boorman, Daniel J., Gunn, Peter D., Mumaw, Randall J., Griffin, John C. III
• Primary Examiner(s): Jeanglaude; Gertrude Arthur
• Application Number:
  US11/639,791
• Publication Number:
  US 20080091311A1
• Time in Patent Office: 1,300 Days
• Field of Search: 701/3, 701/4, 701/11, 701 14- 16, 701120-123, 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 are disclosed. 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:

presenting a plurality of first level options for controlling an aspect of the aircraft'"'"'s motion, at least one of the first level options having associated with it a plurality of second level options;

receiving a first input corresponding to a selection of the at least one first level option;

presenting a plurality of second level options corresponding to the at least one first level option; and

receiving a second input corresponding to a selection of one of the second level options,

wherein during unlinked operation, an instruction corresponding to at least one of the first and second inputs is implemented in response to an operator request, and during linked operation, the instruction is incorporated into a flight plan of the aircraft for automatic execution at a future time, and

wherein at least one of the first or second level options is displayed when the aircraft is engaged in linked operation and hidden when the aircraft is engaged in unlinked operation.

2. The method of claim 1, further comprising:

displaying the first level options on a display panel; and

changing a characteristic of a display of the at least one first level option after receiving a first input corresponding to a selection of the at least one first level option.

3. The method of claim 1 wherein presenting a plurality of first level options includes presenting at least two of the first level options at a display as a switch is manipulated.

4. The method of claim 1 wherein presenting a plurality of second level options includes providing at least two of the second level options as text messages on a display panel.

5. The method of claim 1 wherein presenting a plurality of second level options includes providing temporally sequential alphanumeric indications of the second level options as the operator manipulates a switch.

6. The method of claim 1 wherein presenting a plurality of first level options includes providing a first set of first level options for controlling a lateral motion of the aircraft, a second set of first level options for controlling a vertical motion of the aircraft, and a third set of first level options for controlling a speed of the aircraft.

7. The method of claim 1 wherein presenting a plurality of first level options includes presenting a plurality of flight modes in accordance with which the motion of the aircraft may be controlled, and wherein presenting a plurality of second level options includes presenting a plurality of flight submodes in accordance with which the motion of the aircraft may be controlled.

8. The method of claim 7 wherein the flight modes correspond to alternate manners in which the aircraft is directed to a target, and wherein at least one of the flight modes includes multiple alternate flight submodes, each of which is associated with the at least one flight mode.

10. The system of claim 7 wherein the contents of the computer-readable medium are configured to:

display the first level options on a display panel; and

change a characteristic of a display of the at least one first level option after receiving a first input corresponding to a selection of the at least one first level option.

11. The system of claim 7 wherein the contents of the computer-readable medium are configured to present a plurality of second level options to include at least two of the second level options as text messages on a display panel.

12. The system of claim 7 wherein the contents of the computer-readable medium are configured to present a plurality of first level options to include a first set of first level options for controlling a lateral motion of the aircraft, a second set of first level options for controlling a vertical motion of the aircraft, and a third set of first level options for controlling a speed of the aircraft.

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

presenting a plurality of first level options for controlling an aspect of the aircraft'"'"'s motion, at least one of the first level options having associated with it a plurality of second level options;

receiving a first input corresponding to a selection of the at least one first level option;

presenting a plurality of second level options corresponding to the at least one first level option; and

receiving a second input corresponding to a selection of one of the second level options,

wherein during unlinked operation, an instruction corresponding to at least one of the first and second inputs is implemented in response to an operator request, and during linked operation, the instruction is incorporated into a flight plan of the aircraft for automatic execution at a future time, and

wherein at least one of the first or second level options is displayed when the aircraft is engaged in linked operation and hidden when the aircraft is engaged in unlinked operation.

13. The system of claim 9 wherein presenting a plurality of first level options includes presenting a plurality of flight modes in accordance with which the motion of the aircraft may be controlled, and wherein presenting a plurality of second level options includes presenting a plurality of flight submodes in accordance with which the motion of the aircraft may be controlled.

14. The system of claim 13 wherein the flight modes correspond to alternate manners in which the aircraft is directed to a target, and wherein at least one of the flight modes includes multiple alternate flight submodes, each of which is associated with the at least one flight mode.