Systems and methods for displaying obstacle-avoidance information during surface operations

• US 9,959,774 B2
• Filed: 02/11/2013
• Issued: 05/01/2018
• Est. Priority Date: 05/30/2012
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Vasek, Jiri, Khatwa, Ratan, Kirk, James C., Olofinboba, Olukayode, Kolcarek, Pavel, Svoboda, Tomas, Dusik, Matej
• Primary Examiner(s): Backer, Firmin
• Assistant Examiner(s): Kingston, Shawna M
• Application Number:
  US13/764,701
• Publication Number:
  US 20130321176A1
• Time in Patent Office: 1,905 Days
• Field of Search: None
• CPC Class Codes: G01S 13/93 for anti-collision purposes
• CPC Class Codes: G01S 13/931 of land vehicles
• CPC Class Codes: G01S 13/934 on airport surfaces, e.g. while taxiing
• 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 5/04 Anti-collision systems
• 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
• CPC Class Codes: G08G 5/065 Navigation or guidance aids, e.g. for taxiing or rolling

Abstract

Systems and methods for aiding in pilot awareness of obstacles relative to aircraft features. An exemplary processor receives sensor information from one or more sensors mounted in an aircraft feature (e.g. light modules), determines if at least one obstacle is located within a predefined field of view based on the received sensor or database information and generates an image. The image includes an ownship icon having at least one feature representing wingtips of the aircraft and at least one indicator associated with the determined at least one obstacle. A display device presents the generated image. The display device presents a tip of a first sense coverage area adjacent to one wingtip feature associated with the port wing and a tip of the second sense coverage area adjacent to one wingtip feature associated with the starboard wing. The indicator is presented within at least one of the coverage areas.

Claims

1. A system comprising:

a processor configured to;

receive sensor information from one or more sensors mounted in at least one of a wingtip light module, fuselage, engine cowling, landing gear or tail component of an aircraft, wherein each of the one or more sensors has a field of view that is selected based on a stopping distance range of the aircraft,

determine a braking distance for the aircraft based on a weight and a current speed of the aircraft,

determine a trajectory of at least one aircraft element based on a location of the at least one aircraft element, the current speed of the aircraft, and a heading of the aircraft,

detect at least one obstacle based on the received sensor information and the determined aircraft braking distance, and

generate an image comprising;

an ownship icon comprising at least one feature representing the at least one wingtip light module, fuselage, engine cowling, landing gear, or tail component of the aircraft,

a first vector generated based on the determined trajectory of an associated aircraft element,

a second vector generated based on the determined trajectory of an associated aircraft element, wherein the first vector and the second vector are based on at least one of a distance value or a time value, and

at least one indicator associated with the detected at least one obstacle; and

a display device configured to present the generated image.

2. The system of claim 1, wherein the at least one feature comprises a first feature representing a port wing and a second feature representing a starboard wing of the aircraft, wherein the generated image comprises a first sense coverage area and a second sense coverage area, wherein the display device presents a tip of the first sense coverage area adjacent the first feature and a tip of the second sense coverage area adjacent the second feature, wherein the at least one indicator is presented within at least one of the coverage areas.

3. The system of claim 2, wherein the coverage areas and the ownship icon are presented in a one-to-one relationship and the coverage areas and the ownship icon are presented in one of at least two different range resolutions.

4. The system of claim 2, wherein the at least one indicator comprises a range feature of at least one of the coverage areas, wherein the range feature corresponds to obstacle distance information included in at least one of the received sensor or stored information.

5. The system of claim 2, wherein the at least one indicator comprises a distance value located in at least one of the coverage areas, wherein the distance value corresponds to obstacle distance information included in the received sensor information.

6. The system of claim 2, further comprising:

memory configured to store airport facility information,

wherein the at least one indicator comprises at least a partial outline of the at least one determined obstacle based on at least one of the received sensor information or the stored airport facility information, and

wherein the at least a partial outline is presented within at least one of the coverage areas.

7. The system of claim 1, wherein the generated image comprises:

a first zone associated with first areas outside the aircraft, the first areas being one where, if an obstacle was detected therein, the aircraft would avoid contact based on current heading of the aircraft; and

a second zone associated with a second area outside the aircraft, the second area being one where, if an obstacle was detected therein, the aircraft would be likely to collide with the obstacle based on current heading of the aircraft.

8. The system of claim 7, wherein a first portion of the first zone and a first portion of the second zone are presented from a port wingtip of the ownship icon, and wherein a second portion of the first zone and a second portion of the second zone are presented from a starboard wingtip of the ownship icon.

9. The system of claim 8, wherein the at least one indicator comprises a nearest obstacle icon presented in a first format in one of the zone portions based on the sensor information, and wherein the at least one indicator comprises a next-nearest obstacle icon presented in a second format in one of the zone portions based on the sensor information.

10. The system of claim 8, wherein the at least one indicator comprises a nearest obstacle icon in the first zone presented in a first format in one of the zone portions of the first zone based on the sensor information, and wherein the at least one indicator comprises a nearest obstacle icon in the second zone presented in a second format in one of the zone portions of the second zone based on the sensor information.

11. The system of claim 1, wherein the determined trajectories are not linear.

12. A method comprising:

at a processor,

receiving sensor information from one or more sensors mounted in at least one aircraft feature, wherein each of the one or more sensors has a field of view that is selected based on a stopping distance range of the aircraft;

determining a braking distance for the aircraft based on a weight and a current speed of the aircraft;

determining a trajectory of at least one aircraft element based on a location of the at least one aircraft element, the current speed of the aircraft, and a heading of the aircraft;

detecting at least one obstacle based on the received sensor information and the determined aircraft braking distance; and

generating an image comprising;

an ownship icon comprising the at least one aircraft feature;

a first vector generated based on the determined trajectory of an associated aircraft element;

a second vector generated based on the determined trajectory of an associated aircraft element, wherein the first vector and the second vector are based on at least one of a distance value or a time value; and

at least one indicator associated with the detected at least one obstacle; and

at a display device, presenting the generated image.

13. The method of claim 12, wherein the at least one feature comprises a first feature representing a port wing and a second feature representing a starboard wing of the aircraft, wherein the generated image comprises a first sense coverage area and a second sense coverage area, wherein presenting comprises presenting a tip of the first sense coverage area adjacent the first feature and a tip of the second sense coverage area adjacent the second feature, wherein the at least one indicator is presented within at least one of the coverage areas.

14. The method of claim 13, wherein the coverage areas and the ownship icon are presented in a one-to-one relationship and the coverage areas and the ownship icon are presented in one of at least two different range resolutions.

15. The method of claim 13, wherein generating the image comprising the at least one indicator comprises uniquely depicting a range feature of at least one of the coverage areas, wherein the uniquely depicted range feature corresponds to obstacle distance information included in the received sensor information.

16. The method of claim 13, wherein the at least one indicator comprises a distance value located in at least one of the coverage areas, wherein the distance value corresponds to obstacle distance information included in the received sensor information.

17. The method of claim 13,

wherein the at least one indicator comprises at least a partial outline of the at least one determined obstacle, and wherein generating the image comprises presenting the at least the partial outline within at least one of the coverage areas based on at least one of the received sensor information or airport facility information stored by a memory.

18. The method of claim 12, wherein the generated image comprises:

a first zone associated with first areas outside the aircraft, the first areas being one where, if an obstacle was detected therein, the aircraft would avoid contact based on current heading of the aircraft; and

a second zone associated with a second area outside the aircraft, the second area being one where, if an obstacle was detected therein, the aircraft would be likely to collide with the obstacle based on current heading of the aircraft.

19. The method of claim 18, wherein a first portion of the first zone and a first portion of the second zone are presented from a port wingtip of the ownship icon,

wherein a second portion of the first zone and a second portion of the second zone are presented from a starboard wingtip of the ownship icon,

wherein the at least one indicator comprises a nearest obstacle icon presented in a first format in one of the zone portions based on the sensor information, and

wherein the at least one indicator comprises a next-nearest obstacle icon presented in a second format in one of the zone portions based on the sensor information.