APPARATUSES AND METHODS FOR DISPLAYING AND RECEIVING TACTICAL AND STRATEGIC FLIGHT GUIDANCE INFORMATION

• US 20120179307A1
• Filed: 03/13/2012
• Published: 07/12/2012
• Est. Priority Date: 12/24/2003
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Boorman, Daniel J., Griffin, John C. III, Mumaw, Randall J., Gunn, Petter D.
• Granted Patent: US 8,364,329 B2
• Time in Patent Office: Days
• 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

1-40. -40. (canceled)

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

receiving an input corresponding to a target for directing an aircraft;

when the target is in a first direction relative to a current position of the aircraft, displaying a first indicator corresponding to an instruction for directing the aircraft to move toward the target; and

when the target is in a second direction opposite the first direction, displaying a second indicator corresponding to an instruction for directing the aircraft to move toward the target, the second indicator being different than the first indicator.

42. The system of claim 41, further comprising a computer having an least one input device to receive the input and at least one output device to display the first and second indicators.

43. The system of claim 41 wherein a receiver portion receives the input and a display portion displays the first and second indicators.

44. The system of claim 41, further comprising:

the aircraft; and

a computer having an least one input device to receive the input and at least one output device to display the indicators.

45. The system of claim 41, wherein the contents of the computer-readable medium are configured to display a first indicator to include a first textual indicator corresponding to a right turn, and wherein the contents of the computer-readable medium are configured to display a second indicator to include a second textual indicator corresponding to a left turn.

46. The system of claim 41, wherein the contents of the computer-readable medium are configured to display a first indicator to include a first indicator corresponding to a climb, and wherein the contents of the computer-readable medium are configured to display a second indicator to include a second indicator corresponding to a descent.

47-52. -52. (canceled)

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

receiving an input corresponding to a target for an aircraft;

displaying at least one indicator corresponding to an instruction for directing a behavior of the aircraft; and

directing activation of the instruction only if the instruction is consistent with the target.

54. The system of claim 53, further comprising a computer having an least one input device to receive the input and at least one output device to display the indicator.

55. The system of claim 53 wherein a receiver portion receives the input and a display portion displays the at least one indicator.

56. The system of claim 53, further comprising:

the aircraft; and

a computer having an least one input device to receive the input and at least one output device to display the at least one indicator.

57. The system of claim 53 wherein the contents of the computer-readable medium are configured to receive an input for a target altitude above a current altitude of the aircraft, and wherein the contents of the computer-readable medium are configured to not direct activation of the instruction if the instruction is for an aircraft descent.

58-77. -77. (canceled)