Systems and methods for selectively altering a ground proximity message

• US 8,483,889 B2
• Filed: 01/29/2010
• Issued: 07/09/2013
• Est. Priority Date: 03/06/2006
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Ishihara, Yasuo, Johnson, Steve C
• Primary Examiner(s): Dager, Jonathan M
• Application Number:
  US12/696,555
• Publication Number:
  US 20100286851A1
• Time in Patent Office: 1,257 Days
• Field of Search: 701300-302
• US Class Current: 701/9
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0086 for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935
• CPC Class Codes: G08G 5/045 Navigation or guidance aids, e.g. determination of anti-collision manoeuvers radar or analogous systems specially adapted for anti-collision between aircraft G01S13/933

Abstract

Systems and methods for selectively altering a ground proximity warning message. In an embodiment, a ground proximity warning system for a flight vehicle includes a processor that is configured to generate a look-ahead envelope that defines a region extending outwardly from the flight vehicle and to generate a terrain proximity message when the defined region intersects a terrain feature. An interface device is coupled to the processor that is operable to configure the system in a first operating mode wherein the generated terrain proximity message is selectively suppressed, and a second operating mode wherein the terrain proximity message is not suppressed.

Claims

1. A method of selectively altering a ground proximity warning message for an aircraft, comprising:

constructing a suitably configured look-ahead envelope that extends outwardly from the aircraft;

detecting an intersection of the look-ahead envelope with a terrain feature and generating the ground proximity warning message;

identifying at least one alternate flight path, wherein the aircraft possesses suitable performance characteristics to execute the alternate flight path to navigate;

in response to identifying the at least one alternate flight path, continuing a first operating mode that suppresses the ground proximity warning message; and

altering the ground proximity warning message from the suppression state if the at least one alternate flight path comprising an executable aircraft bank angle exists that avoids the intersection.

2. The method of claim 1, wherein constructing the suitably configured look-ahead envelope further comprises generating a look-ahead envelope having a terrain warning portion adjacent to the flight vehicle, and a terrain advisory portion that extends outwardly from the terrain warning portion.

3. The method of claim 2, further comprising suppressing the ground proximity warning message when the terrain advisory portion intersects the terrain feature, and presenting the ground proximity warning message when the terrain warning portion intersects the terrain feature.

4. The method of claim 1, further comprising:

determining if the aircraft possesses suitable performance characteristics to execute the aircraft bank angle to navigate along the alternate path;

generating the at least one alternate flight path only when the aircraft possesses the suitable performance characteristics to execute the aircraft bank angle.

5. The method of claim 4, wherein determining if the aircraft possesses suitable performance characteristics to navigate along the alternate path further includes determining if the aircraft possesses at least one of a suitable rate of climb and a suitable thrust.

6. The method of claim 1, wherein altering the ground proximity warning message further comprises suppressing at least one of a visual warning message and an aural warning message.

7. The method of claim 1, further comprising actuating an interface device that alters the ground proximity warning message.

8. The method of claim 7, wherein actuating an interface device further comprises actuating the interface device using at least one of a speech recognition device and a manual actuation device.

9. The method of claim 1, further comprising:

identifying from a plurality of alternate flight paths the at least one alternate flight path, wherein the alternate flight path is identified if the aircraft possesses suitable performance characteristics to execute the aircraft bank angle to navigate along the alternate path.

10. A method of selectively altering a ground proximity warning message for an aircraft, comprising:

constructing a suitably configured look-ahead envelope that extends outwardly from the aircraft;

detecting an intersection of the look-ahead envelope with a terrain feature and generating the ground proximity warning message;

identifying from a plurality of alternate flight paths at least one alternate flight path, wherein the alternate flight path is identified if the aircraft possesses suitable performance characteristics to execute at least an aircraft bank angle to navigate along the alternate flight path;

altering the ground proximity warning message if at least one alternate flight path comprising the executable aircraft bank angle exists that avoids the intersection;

in response to failure to identify the at least one alternate flight path, overriding a first operating mode that suppresses the ground proximity warning message; and

in response to overriding the first operating mode, issuing the ground proximity warning message, wherein the ground proximity warning message is altered from a suppressed state to an issued state.

11. The method of claim 10, wherein issuing the ground proximity warning message further comprises:

issuing an aural ground proximity warning message.

12. The method of claim 10, wherein issuing the ground proximity warning message further comprises:

issuing an aural ground proximity warning message and a visual ground proximity warning message.

13. A method of selectively altering a ground proximity warning message for an aircraft, comprising:

constructing a suitably configured look-ahead envelope that extends outwardly from the aircraft;

detecting an intersection of the look-ahead envelope with a terrain feature and generating the ground proximity warning message;

identifying from a plurality of alternate flight paths at least one alternate flight path, wherein the alternate flight path is identified if the aircraft possesses suitable performance characteristics to execute at least an aircraft bank angle to navigate along the alternate flight path;

in response to identifying the at least one alternate flight path, continuing a first operating mode that suppresses the ground proximity warning message; and

altering the ground proximity warning message if the at least one alternate flight path comprising the executable aircraft bank angle exists that avoids the intersection.

14. The method of claim 13, wherein continuing the first operating mode that suppresses the ground proximity warning message further comprises:

suppressing an aural ground proximity warning message; and

issuing a visual ground proximity warning message.

15. The method of claim 13, wherein continuing the first operating mode that suppresses the ground proximity warning message further comprises:

suppressing an aural ground proximity warning message and a visual ground proximity warning message.