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

• US 7,945,354 B2
• Filed: 06/28/2010
• Issued: 05/17/2011
• Est. Priority Date: 12/24/2003
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Mumaw, Randall J., Gunn, Peter D., Griffin, John C. III, Boorman, Daniel J.
• Primary Examiner(s): ARTHUR JEANGLAUDE, GERTRUDE
• Application Number:
  US12/825,135
• Publication Number:
  US 20100262358A1
• Time in Patent Office: 323 Days
• Field of Search: 701/3, 701/4, 701/8, 701/13, 701/14, 244/75.1, 244/118.5, 340/945, 340/980
• 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 method for controlling an aircraft system to direct vertical motion of an aircraft, the method comprising:

receiving a request from an aircraft operator for an aircraft descent when the aircraft is at a first altitude above a threshold altitude; and

based solely on the request, automatically directing the aircraft to descend to a second altitude along a path that at least approximately minimizes the descent rate of the aircraft.

2. The method of claim 1, wherein the aircraft includes a computer having at least one input device to receive the request.

3. The method of claim 1, wherein the request includes a request to be executed during engine-out operation of the aircraft.

4. The method of claim 1, further comprising specifying the threshold altitude in response to input received from a vertical selector component.

5. The method of claim 4, wherein the vertical selector component is a hardware input device.

6. The method of claim 1, wherein the request is received through a single-purpose hardware control.

7. The method of claim 6, wherein the request is generated based only on the input to the single-purpose hardware control.

8. The method of claim 1, wherein the second altitude is equal to the threshold altitude.

9. The method of claim 1, further comprising:

initially operating the aircraft automatically in accordance with a flight plan; and

automatically unlinking a vertical motion axis of the aircraft from the automatic operation in response to the request.

10. A computer-readable medium containing instructions for controlling an aircraft computer system to direct vertical motion of an aircraft, by a method comprising:

receiving a request from an aircraft operator for an aircraft descent when the aircraft is at a first altitude above a threshold altitude; and

based solely on the, request, automatically directing the aircraft to descend to a second altitude along a path that at least approximately minimizes the descent rate of the aircraft.

11. The computer-readable medium of claim 10, wherein the request is received from an input device in the aircraft.

12. The computer-readable medium of claim 10, wherein the request includes a request to be executed during engine-out operation of the aircraft.

13. The computer-readable medium of claim 10, the method further comprising specifying the threshold altitude in response to input received from a vertical selector component.

14. The computer-readable medium of claim 10, wherein the request is received through a single-purpose hardware control.

15. The computer-readable medium of claim 14, wherein the request is generated based only on the input to the single-purpose hardware control.

16. The computer-readable medium of claim 10, wherein the second altitude is equal to the threshold altitude.

17. The computer-readable medium of claim 10, further comprising:

initially operating the aircraft automatically in accordance with a flight plan; and

automatically unlinking a vertical motion axis of the aircraft from the automatic operation in response to the request.

18. A system for controlling an aircraft system to direct vertical motion of an aircraft, comprising:

a vertical selector component configured to receive a target altitude;

a drift down selector component configured to receive a request from an aircraft operator for an aircraft descent when the aircraft is at a first altitude above a threshold altitude; and

an aircraft control component configured to automatically direct the aircraft to descend to the target altitude along a path that at least approximately minimizes the descent rate of the aircraft, based solely on the received request.

19. The system of claim 18, wherein the drift down selector component is a single-purpose hardware control.

20. The system of claim 18, wherein when the aircraft is initially operating automatically in accordance with a flight plan, the aircraft control component is further configured to automatically unlink a vertical motion axis of the aircraft from the automatic operation in response to the request.