PASSIVE AIRCRAFT WINGTIP STRIKE DETECTION SYSTEM AND METHOD

• US 20150213721A1
• Filed: 04/22/2014
• Published: 07/30/2015
• Est. Priority Date: 01/30/2014
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Conner, Kevin J., Ishihara, Yasuo, Johnson, Steve, Berry, Ray
• Application Number:
  US14/258,839
• Publication Number:
  US 20150213721A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G05D 1/0083 to help an aircraft pilot in the rolling phase
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91
• CPC Class Codes: G08G 5/0086 for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935
• CPC Class Codes: G08G 5/04 Anti-collision systems
• CPC Class Codes: G08G 5/06 for control when on the ground
• CPC Class Codes: G08G 5/065 Navigation or guidance aids, e.g. for taxiing or rolling
• CPC Class Codes: G09B 29/006 Representation of non-cartographic information on maps, e.g. population distribution, wind direction, radiation levels, air and sea routes
• CPC Class Codes: G09B 29/007 using computer methods
• CPC Class Codes: G09B 9/052 characterised by provision for recording or measuring trainee's performance devices for psychotechnics, e.g. for vehicle drivers A61B5/16, A61B5/18

Abstract

A system and method for passively detecting aircraft wingtip strikes includes generating a digital base map represented by a plurality of aerodrome cells. A numeric value is assigned to each of the aerodrome cells that is representative of the specific wingtip strike threat associated with that aerodrome cell. An index count array is generated that has a separate entry for each numeric value. A digital aircraft structure is generated that is representative of an aircraft, and is represented by a plurality of aircraft cells. A portion of the aerodrome cells are replaced with the plurality of aircraft cells. Each numeric value of the aerodrome cells that are replaced is counted to determine a replacement count associated therewith and that is entered into the separate entry in the index count array for that numeric value. One or more potential aircraft wingtip strikes are detected based on the replacement counts.

Claims

1. A method for passively detecting aircraft wingtip strikes, comprising the steps of:

in a processing system;

generating a digital base map of at least a portion of an aerodrome that includes one or more specific wingtip strike threats, the digital base map represented by a plurality of aerodrome cells;

assigning a numeric value to each of the aerodrome cells, the numeric value assigned to each aerodrome cell representative of the specific wingtip strike threat associated with that aerodrome cell;

generating an index count array, the index count array having a separate entry for each numeric value;

generating a digital aircraft structure representative of an aircraft, the digital aircraft structure represented by a plurality of aircraft cells;

replacing a portion of the aerodrome cells with the plurality of aircraft cells;

counting each numeric value of the aerodrome cells that are replaced to determine a replacement count associated therewith;

entering the replacement count associated with each numeric value into the separate entry in the index count array for that numeric value;

detecting one or more potential aircraft wingtip strikes based on the replacement counts in the index count array.

2. The method of claim 1, wherein the digital aircraft structure comprises a protective envelope around the aircraft.

3. The method of claim 2, wherein the protective envelope has a size, and wherein the method further comprises:

detecting aircraft speed; and

varying the size of the protective envelope based on the detected aircraft speed.

4. The method of claim 1, further comprising:

determining a current location of the aircraft; and

replacing the portion of the aerodrome cells with the plurality of aircraft cells at the current location.

5. The method of claim 4, further comprising:

predicting a plurality of future locations of the aircraft; and

replacing the portion of the aerodrome cells with the plurality of aircraft cells at each of the plurality of future locations.

6. The method of claim 1, further comprising:

selectively generating an alert based on the one or more potential aircraft wingtip strikes that are detected.

7. The method of claim 1, wherein the one or more specific wingtip strike threats comprise:

an open region;

a terminal building;

a non-terminal building;

a fixed obstacle; and

a moving object.

8. The method of claim 7, further comprising:

determining when the one or more potential wingtip strikes include a specific wingtip strike threat that is not an open region; and

generating an alert based on the specific wingtip strike threat.

9. The method of claim 1, wherein the step of generating the digital base map comprises:

retrieving compressed aerodrome data representative of the aerodrome from an aerodrome database;

decompressing retrieved aerodrome data; and

copying the decompressed aerodrome data into a geo-referenced memory array.

10. The method of claim 1, further comprising:

selectively rendering, on a display device, the digital base map and the digital aircraft structure.

17. The system of claim 1, wherein the one or more specific wingtip strike threats comprise:

an open region;

a terminal building;

a non-terminal building;

a fixed obstacle; and

a moving object.

18. The system of claim 17, wherein:

the processor is further configured to determine when the one or more potential wingtip strikes include a specific wingtip strike threat that is not an open region and upon making this determination, generate an alert signal based on the specific wingtip strike threat; and

the system further comprises an alert device coupled to receive the alert signal and configured, in response thereto, to generate an alert.

11. A passive aircraft wingtip strike detection system, comprising:

an aerodrome database having aerodrome data stored therein, the aerodrome data including data representative of specific wingtip strike threats; and

a processor in operable communication with the aerodrome database, the processor configured to selectively retrieve aerodrome data from the aerodrome database and, upon retrieval thereof to;

generate a digital base map of at least a portion of an aerodrome that includes one or more specific wingtip strike threats, the digital base map represented by a plurality of aerodrome cells;

assign a numeric value to each of the aerodrome cells, the numeric value assigned to each aerodrome cell representative of the specific wingtip strike threat associated with that aerodrome cell;

generate an index count array, the index count array having a separate entry for each numeric value;

generate a digital aircraft structure representative of an aircraft, the digital aircraft structure represented by a plurality of aircraft cells;

replace a portion of the aerodrome cells with the plurality of aircraft cells;

count each numeric value of the aerodrome cells that are replaced to determine a replacement count associated therewith;

enter the replacement count associated with each numeric value into the separate entry in the index count array for that numeric value; and

detect one or more potential aircraft wingtip strikes based on the replacement counts in the index count array.

12. The system of claim 11, wherein the digital aircraft structure comprises a protective envelope around the aircraft.

13. The system of claim 12, wherein:

the protective envelope has a size;

processor is adapted to receive data representative of aircraft speed; and

the processor is further configured to vary the size of the protective envelope based on the aircraft speed.

14. The system of claim 11, wherein the processor is adapted to receive aircraft location data and is configured, upon receipt thereof, to determine current location of the aircraft and replace the portion of the aerodrome cells with the plurality of aircraft cells at the current location.

15. The system of claim 14, wherein the processor is further configured to predict a plurality of future locations of the aircraft and replace the portion of the aerodrome cells with the plurality of aircraft cells at each of the plurality of future locations.

16. The system of claim 11, wherein:

the processor is further configured to selectively supply an alert signal based on the one or more potential aircraft wingtip strikes that are detected; and

the system further comprises an alert device coupled to receive the alert signal and configured, in response thereto, to generate an alert.

19. The system of claim 11, wherein:

the retrieved aerodrome data are compressed aerodrome data; and

the processor is further configured to decompress the retrieved aerodrome data and copy the decompressed aerodrome data into a geo-referenced memory array.

20. The system of claim 11, further comprising:

a display device coupled to receive image rendering display commands and configured, upon receipt of the image rendering display commands, to render images,

wherein the processor is further configured to selectively supply image rendering display commands to the display device that cause the display device to render images of the digital base map and the digital aircraft structure.