Systems and methods for performing wingtip protection

• US 9,229,101 B2
• Filed: 05/21/2013
• Issued: 01/05/2016
• Est. Priority Date: 05/30/2012
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Kirk, James C, Bui, Long, Vacanti, David C, Freeman, Catherine L
• Primary Examiner(s): Gregory, Bernarr
• Application Number:
  US13/899,298
• Publication Number:
  US 20130321194A1
• Time in Patent Office: 959 Days
• Field of Search: 342 27- 51, 342/61, 342 70- 72, 342 73- 81, 342147-158, 342/175, 342/195, 342/13, 342/350, 342/385, 342/386, 342/407, 342/410, 342/411, 343/700.R, 343705-708, 343711-717, 701/300, 701/301
• US Class Current: 1/1
• CPC Class Codes: B60Q 9/008 for anti-collision purposes
• CPC Class Codes: B64C 25/42 Arrangement or adaptation of brakes
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• 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: G01S 13/66 Radar-tracking systems; Analogous systems
• CPC Class Codes: G01S 13/765 with exchange of information between interrogator and responder
• 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: G01S 2013/9329 cooperating with reflectors or transponders
• CPC Class Codes: G01S 7/04 Display arrangements
• 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 creating a narrow vertical pathway of detection that permits the enforcement of a fixed “exclusion zone” that is narrow and does not widen with range. An advantage to this approach is that the zone or corridor does not widen with range, permitting a fixed exclusion zone that will ignore items that will pass above or below the wing. An exemplary system located on a vehicle includes at least two vertically separated antennas that receive radar reflection signals, a processor, and an output device. The processor receives the radar reflection signals received by the antennas, determines vertical position of any obstacles identified in the radar reflection signals and determines if the obstacles are within a predefined alert zone. The output device outputs an alert if any obstacle is within the alert zone. The predefined alert zone is related to a protruding portion of the vehicle.

Claims

1. A system located on a vehicle, the system comprising:

at least two vertically separated antennas configured to receive radar reflection signals, wherein the antennas are spaced at a half wavelength interval from each other;

a processor configured to;

receive the radar reflection signals received by the antennas,

determine a vertical position of any obstacles identified in the radar reflection signals based on monopulse discrimination by at least determining a phase differential of corresponding radar reflection signals and determining the vertical position based on the phase differential, and

determine if the obstacles are within a predefined alert zone; and

an output device configured to output an alert if any obstacle is within the alert zone,

wherein the predefined alert zone is related to a protruding portion of the vehicle and defined by whether the motion of the vehicle will result in collision with an object located therein.

2. The system of claim 1, wherein the protruding portion of the vehicle comprises at least one of a portion of a wing or a portion of a nacelle attached to the wing.

3. The system of claim 1, further comprising:

a memory device configured to store obstacle information in a three-dimensional buffer based on associated determined vertical position information.

4. The system of claim 1, wherein the predefined alert zone comprises a volume of space along at least one of a projection forward of a vehicle structure or a current path of the vehicle structure.

5. The system of claim 1, wherein the predefined alert zone has a constant upper limit, a constant lower limit, a first distance limit and a second distance limit, wherein the shape of the predefined alert zone is based on the vehicle structure that the predefined alert zone relates to.

6. A method comprising:

at at least two vertically separated antennas spaced at a half wavelength (λ

/2) interval from each other, receiving radar reflection signals;

at a processor;

receiving the radar reflection signals received by the antennas;

determining a vertical position of any obstacles identified in the radar reflection signals based on monopulse discrimination, wherein determining the vertical position comprises;

determining a phase differential of corresponding radar reflection signals; and

determining the vertical position based on the phase differential; and

determining if the obstacles are within a predefined alert zone; and

at an output device, outputting an alert if any obstacle is within the alert zone,

wherein the predefined alert zone is related to a protruding portion of the vehicle and defined by whether the motion of the vehicle will result in collision with an object located therein.

7. The method of claim 6, wherein the vehicle is an aircraft and the protruding portion of the aircraft comprises at least one of a portion of a wing or a portion of a nacelle attached to the wing.

8. The method of claim 6, further comprising:

storing obstacle information in a three-dimensional buffer based on associated determined vertical position information.

9. The method of claim 6, wherein the predefined alert zone comprises a volume of space along at least one of a projection forward of a vehicle structure or a predefined path of the vehicle structure.

10. The method of claim 6, wherein the predefined alert zone has a constant upper limit, a constant lower limit, a first distance limit, and a second distance limit, wherein the shape of the predefined alert zone is based on the vehicle structure that the predefined alert zone relates to.

11. A system comprising:

first and second means for receiving radar reflection signals, the first and second means for receiving radar reflection signals being spaced at a half wavelength (λ

/2) interval from each other;

means for receiving the radar reflection signals received from the first and second means for receiving radar reflection signals;

means for determining a vertical position of any obstacles identified in the radar reflection signals based on monopulse discrimination, wherein the means for determining the vertical position comprises;

means for determining a phase differential of corresponding radar reflection signals; and

means for determining the vertical position based on the phase differential;

means for determining if the obstacles are within a predefined alert zone; and

means for outputting an alert if any obstacle is within the alert zone,

wherein the predefined alert zone is related to a protruding portion of the vehicle and defined by whether the motion of the vehicle will result in collision with an object located therein.

12. The system of claim 11, wherein the vehicle is an aircraft and the protruding portion of the aircraft comprises at least one of a portion of a wing or a portion of a nacelle attached to the wing.

13. The system of claim 11, further comprising:

a means for storing obstacle information in a three-dimensional buffer based on associated determined vertical position information.

14. The system of claim 11, wherein the predefined alert zone comprises a volume of space along at least one of a projection forward of a vehicle structure or a predefined path of the vehicle structure.

15. The system of claim 11, wherein the predefined alert zone has a constant upper limit, a constant lower limit, a first distance limit, and a second distance limit, wherein the shape of the predefined alert zone is based on the vehicle structure that the predefined alert zone relates to and whether the motion of the vehicle will result in collision with an object located therein.