Aircraft door camera system for jet bridge alignment monitoring

Patent metadata

Field	Value
Publication number	US-12340703-B2
Application number	US-202217886193-A
Country	US
Kind code	B2
Filing date	Aug 11, 2022
Priority date	Aug 11, 2021
Publication date	Jun 24, 2025
Grant date	Jun 24, 2025

Abstract

A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that a jet bridge cabin is within the field of view of the camera when the aircraft is within a docking distance of the jet bridge cabin. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera by identifying physical characteristics of the jet bridge cabin, extracting, using the identified physical characteristics of the jet bridge cabin, alignment features corresponding to the physical characteristics of the jet bridge cabin that are indicative of alignment between the jet bridge cabin and the aircraft door, determining, based on the alignment features, whether the physical characteristics of the jet bridge cabin within the captured image data satisfy threshold alignment criteria to produce an alignment state, and outputting an indication of the alignment state.

First claim

The invention claimed is:

1. A system for monitoring an external environment of an aircraft, the system comprising:
A plurality of aircraft doors;
a plurality of cameras, at least one camera of the plurality of cameras being disposed within the aircraft door and each camera of the plurality of cameras having a field of view that is unique among the plurality of cameras and toward the external environment of the aircraft and disposed within the aircraft door such that a cabin of a jet bridge is within the field of view of at least one of the cameras when the aircraft is within a docking distance of the cabin of the jet bridge;
a display device disposed within an interior of the aircraft; and
a processor operatively coupled to the plurality of cameras and to the display device to:
receive, from each respective camera of the plurality of cameras, image data captured by each respective camera that is representative of the external environment of the aircraft within the field of view of the respective camera;
aggregate the captured image data received from each respective camera of the plurality of cameras to produce aggregated image data representative of the external environment of the aircraft, wherein image data from overlapping fields of view of the plurality of cameras is presented only once in the aggregated image data;
output the aggregated captured image data with duplicated image data shown only once for display at the display device; and
analyze the aggregated captured image data for jet bridge alignment by:
identifying, within the aggregated captured image data, physical characteristics of the cabin of the jet bridge;
extracting, using the identified physical characteristics of the cabin of the jet bridge, alignment features corresponding to the physical characteristics of the cabin of the jet bridge that are indicative of alignment between the cabin of the jet bridge and the aircraft door;
determining, based on the alignment features, whether the physical characteristics of the cabin of the jet bridge within the captured image data satisfy threshold alignment criteria to produce an alignment state; and
outputting an indication of the alignment state to the display device.

2. The system of claim 1 , wherein the physical characteristics of the cabin of the jet bridge comprise boundaries of the cabin of the jet bridge.

3. The system of claim 2 , wherein identifying the boundaries of the cabin of the jet bridge comprises identifying edges of the cabin of the jet bridge within the captured image data.

4. The system of claim 2 , wherein the alignment features comprise one or more of: relative orientation of the identified edges of the cabin of the jet bridge; size of the identified edges within the captured image data; and relative size of the identified edges within the captured image data.

5. The system of claim 1 , wherein the processor is operatively coupled to the aircraft to receive an indication that the aircraft is in a docking phase.

6. The system of claim 5 , wherein the processor is operatively coupled to an avionics system of the aircraft.

7. The system of claim 1 , wherein the processor is operatively coupled to the camera to utilize an edge detection algorithm to identify a boundary of the cabin of the jet bridge.

8. The system of claim 7 , wherein the edge detection algorithm is a Canny edge detector multi-stage algorithm.

9. A method of monitoring an external environment of an aircraft, the method comprising:
receiving, with a processor, aggregated image data captured by a plurality of cameras disposed within an aircraft door of the aircraft such that a cabin of a jet bridge is within a field of view of at least one of the cameras when the aircraft is within a docking distance of the cabin of the jet bridge;
analyzing the aggregated captured image data by:
identifying, within the captured image data, physical characteristics of the cabin of the jet bridge;
extracting, using the identified physical characteristics of the cabin of the jet bridge, alignment features corresponding to the physical characteristics of the cabin of the jet bridge that are indicative of alignment between the cabin of the jet bridge and the aircraft door;
determining, based on the alignment features, whether the physical characteristics of the cabin of the jet bridge within the captured image data satisfy threshold alignment criteria to produce an alignment state; and
outputting an indication of the alignment state to a display device disposed within an interior of the aircraft, wherein image data from overlapping fields of view of the plurality of cameras is presented only once in the aggregated image data; and

outputting the captured image data for display at the display device disposed within the interior of the aircraft.

10. The method of claim 9 , wherein the alignment features comprise at least one of: a relative orientation of boundaries of the cabin of the jet bridge, a size of an edge of the cabin of the jet bridge, and a relative size of a plurality of edges of the cabin of the jet bridge.

11. The method of claim 9 , wherein outputting the indication of the alignment state comprises outputting a graphical overlay of target alignment features over a graphical indication of the extracted alignment features.

Assignees

• Rosemount Aerospace Inc

Inventors

• Pesik Joseph T
• Boer Jonathan

Classifications

• G06T2207/30241

  Trajectory · CPC title

• G06T2207/30196

  Human being; Person · CPC title

• G06T2207/20076

  Probabilistic image processing · CPC title

• G06V10/759

  Region-based matching · CPC title

• G06V10/82

  using neural networks · CPC title