Object detection system

Patent metadata

Field	Value
Publication number	US-10107910-B2
Application number	US-201615376165-A
Country	US
Kind code	B2
Filing date	Dec 12, 2016
Priority date	Dec 12, 2016
Publication date	Oct 23, 2018
Grant date	Oct 23, 2018

Abstract

An in-flight detection system includes a camera mounted to a platform aircraft configured to define a field of regard containing a target aircraft. A lidar system is mounted to the platform aircraft and is configured to continuously scan the field of regard defined by the camera. The lidar system determines position data between the platform aircraft and the target aircraft. A controller is operatively connected to the camera and the lidar system and is configured to activate the lidar system after the camera defines the field of regard.

First claim

What is claimed is:

1. An object detection system, comprising:
a camera mounted to a platform aircraft configured to define a field of regard containing a target aircraft;
a lidar system mounted to the platform aircraft configured to continuously scan the field of regard defined by the camera and determine position data between the platform aircraft and the target aircraft; and
a controller operatively connected to the camera and the lidar system configured to activate the lidar system after the camera defines the field of regard.

2. The detection system of claim 1 , wherein the camera defines the field of regard based on thermal signature produced from the target aircraft.

3. The detection system of claim 1 , wherein the lidar system includes at least one laser configured to direct an optical beam within a field of view of the lidar system and a detection system configured to receive a reflected portion of the optical beam from the field of view.

4. The detection system of claim 3 , further comprising a scanning mechanism including a mirror, positioning motors, and encoders or resolvers to determine pointing angle configured to point the lidar laser and receiver field of view.

5. The detection system of claim 4 , further comprising:
a processor operatively connected to the camera and lidar device connected to a memory, wherein the memory includes instructions recorded thereon that, when read by the processor, cause the processor to:
receive the portion of the laser beam from the field of view; and
provide distance to the target aircraft.

6. The detection system of claim 5 , wherein the memory is configured to store coordinates of the field of regard.

7. The detection system of claim 6 , wherein the controller is operatively connected to the memory and wherein the controller is configured to trigger the memory to maintain the lidar system pointing and scanning within the coordinates of the field of regard.

8. The detection system of claim 1 , wherein the camera and lidar system are mounted for scanning the target aircraft with the target aircraft positioned above the platform aircraft.

9. The detection system of claim 1 , further comprising a control unit on the platform aircraft operatively connected to the controller, wherein the control unit is arranged to control the platform aircraft to steer the platform aircraft to a position for connecting a fuel feeder and nozzle of the target aircraft to the platform aircraft.

10. The detection system of claim 9 , wherein the lidar system is configured to provide a three dimensional image to determine location of the fuel feeder and nozzle relative to the platform aircraft.

11. The detection system of claim 1 , wherein the control unit on the platform aircraft is operatively connected to the target aircraft and is arranged to steer the target aircraft to avoid airborne objects.

12. An object detection system, comprising:
a camera mounted to a platform aircraft configured to define a field of regard containing a target aircraft;
a lidar system mounted to the platform aircraft configured to continuously scan the field of regard defined by the camera;
a controller operatively connected to the camera and the lidar system configured to activate the lidar system after the camera defines the field of regard; and
a processor operatively connected to the camera and lidar system connected to a memory, wherein the memory is configured to store coordinates of the field of regard and wherein the memory includes instructions recorded thereon that, when read by the processor, cause the processor to provide position data of the target aircraft relative to the platform aircraft,
wherein the controller is configured to trigger the memory to maintain the lidar system pointing and scanning within the coordinates of the field of regard.

13. The detection system of claim 12 , wherein the camera and lidar system are mounted for scanning the target aircraft with the target aircraft positioned above the platform aircraft.

14. The detection system of claim 12 , further comprising a control unit on the platform aircraft operatively connected to the controller, wherein the control unit is arranged to control the platform aircraft to steer the platform aircraft to a position for connecting a fuel feeder and nozzle of the target aircraft to the platform aircraft.

15. The detection system of claim 12 , wherein the control unit on the platform aircraft is operatively connected to a control unit on the target aircraft.

16. The detection system of claim 15 , wherein the control unit on the platform aircraft arranged to steer the target aircraft to avoid airborne objects.

17. A method of detecting an object, the steps comprising:
triggering a camera mounted to a platform aircraft to define a field of regard containing a target aircraft;
communicating the field of regard coordinates to a controller operatively connected to the camera;
activating a lidar system operatively connected to the controller and mounted to the platform aircraft to continuously scan the field of regard defined by the camera; and
determining position data between the platform aircraft and the target aircraft.

18. The detection system of claim 1 , wherein the lidar system includes at least one laser configured to direct an optical beam within the field of regard defined by the camera.

19. The detection system of claim 1 , wherein the lidar system includes a lidar receiver and detection system part configured to receive a portion of the an optical emitted by a laser of the lidar system.

20. The detection system of claim 1 , further comprising a scanning mechanism including a mirror, positioning motors, and encoders or resolvers to determine pointing angle scans of a field of view of the lidar system.

Assignees

• Goodrich Corp

Inventors

• Johnson James B
• Marden Michael C
• Humphrey Ian P

Classifications

• B64D39/00

  Refuelling during flight · CPC title

• G01S17/933

  of aircraft or spacecraft · CPC title

• G01S17/42

  Simultaneous measurement of distance and other co-ordinates (indirect measurement G01S17/46) · CPC title

• G01S17/86 Primary

  Combinations of lidar systems with systems other than lidar, radar or sonar, e.g. with direction finders · CPC title

• B64D47/08

  Arrangements of cameras · CPC title