Aircraft ground collision avoidance system and method

• US 6,118,401 A
• Filed: 07/01/1996
• Issued: 09/12/2000
• Est. Priority Date: 07/01/1996
• Status: Expired due to Fees

• Current Assignee: Sun Microsystems Incorporated (Oracle Corporation)
• Original Assignee: Sun Microsystems Incorporated (Oracle Corporation)
• Inventors: Tognazzini, Bruce
• Primary Examiner(s): SOTOMAYOR, JOHN B
• Application Number:
  US08/671,299
• Time in Patent Office: 1,534 Days
• Field of Search: 342/27, 342/28, 342/29, 342/41, 342/55
• US Class Current: 342/29
• CPC Class Codes: G01S 13/04 Systems determining presence of a target based on relative movement of target G01S13/56
• CPC Class Codes: G01S 13/93 for anti-collision purposes
• CPC Class Codes: G01S 7/04 Display arrangements

Abstract

A system and method for avoiding collision between objects and wingtips of an aircraft when the aircraft is on the ground includes mounting detecting devices such as a low cost radar unit and a video camera in the wingtip. These detection devices are coupled with one or more indicators to provide an operator of the aircraft such as a pilot that an imminent collision with an object is about the occur. The indication can be an audio or visual signal, either within or outside of the aircraft.

Claims

1. A method of avoiding collision between a wingtip of an aircraft on the ground and an object comprising the steps of:

(a) detecting the presence of a nearby object which is in proximity to one of the wingtips of an aircraft when the aircraft is on the ground using a radar and at least one video camera, the proximity of the object capable of causing the wingtip and object to collide based on movement of the aircraft; and

(b) indicating the presence of the nearby object and the wingtip to which it is proximate to an operator controlling the movement of the aircraft so that the operator can react to avoid collision between the wingtip and the nearby object.

2. The method of claim 1 wherein said the radar is a micropower impulse type radar.

3. The method of claim 1 wherein said indicating step provides at least one of an audio signal, a video image and a visual warning.

4. The method of claim 1 wherein said detecting step detects objects which are at least one of full forward, full aft and to a side of each of the wingtips.

5. The method of claim 1 wherein said detecting step sequentially detects objects from a midpoint of each wingtip to one of full forward and full aft.

6. The method of claim 1 wherein said detecting step is responsive to steering of said aircraft so that a field of detection of said detecting step is varied with respect to a change in direction of movement of a respective said wingtip.

7. The method of claim 3 wherein said audio signal is provided both inside and outside of said aircraft.

8. A system for avoiding collision between an object and wingtips of an aircraft on the ground comprising:

(a) a detecting device comprising a radar unit and a video camera mountable to a respective wingtip of an aircraft for detection of an object near that wingtip; and

(b) an indicating device mountable to said aircraft for indicating the presence of said object and the wingtip proximate to said object is detected by at least one of said radar unit and said video camera so that an operator of said aircraft can react to avoid collision between said object and said wingtip.

9. The system of claim 8 wherein said indicating device is at least one of an audio signal device, a visual warning lamp and a video display.

10. The system of claim 8 wherein said indicating device is an audio signal device and an audio signal device is provided for each wingtip.

11. The system of claim 8 wherein said detecting device has a field of detection for said object and said system includes a drive to move said field of detection up to 270°

.

12. The system of claim 8 wherein said detecting device has a field of detection defining a distance between the detected object and the wingtip and said system includes a control to alter said field of detection to vary the distance of detection.

13. The system of claim 8 wherein said detecting device has a field of detection defining a distance for detecting the object and said system includes a control to alter said distance based on movement of said aircraft.

14. The system of claim 13 wherein said control increases said distance for one wingtip that moves faster than the other wingtip as a result of turning of said aircraft.

15. The system of claim 8 wherein said detecting device comprises a radar unit and video camera for each wingtip and an audio signal device and video display for each respective said radar unit and said video camera.

16. The system of claim 15 wherein each said audio signal device has capability for producing an audio signal inside and outside of said aircraft.

17. The system of claim 8 wherein said detecting device is a micropower impulse type radar.

18. An apparatus for avoiding collision between a wingtip of an aircraft on the ground and an object comprising:

a detector for detecting the presence of a nearby object which is in proximity to an aircraft when the aircraft is on the ground, the field of view of said detector changing with a change of direction of the aircraft; and

an indicator indicating the presence of the nearby object and the wingtip to which it is proximate to an operator controlling the movement of the aircraft so that the operator can react to avoid collision between the wingtip and the nearby object.