IP Library Granted Patent US 12692016
Granted Patent B2
US 12692016 · App. 18/425,142 · Granted Jul 28, 2026

Method and system for monitoring operations of landing gears of aircraft

Inventor: Cameron Graeme Cooke (Toulouse, FR)
Assignee: Airbus SAS
B64D45/0005G06N20/00G06T7/74G06T2207/20081G06T2207/30252
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Quick Facts
Patent No.
US 12692016
App. No.
18/425,142
Granted
Jul 28, 2026
Kind
B2
Abstract

A system and method for providing an operational state of a monitored landing gear of an aircraft by obtaining, in real-time, captured signals, such as images, of an actual position of the monitored landing gear. The captured signals are then transformed in a descriptor vector using Principal Components Analysis. The descriptor vector is then injected in a machine learning-based model trained and configured to transform descriptor vectors into equivalent operational states of landing gears, the equivalent operational states including up-locked, up-unlocked, in-transit, down-unlocked, and down-locked. The operational state, selected from the equivalent operational states, of the monitored landing gear is then provided to avionics of the aircraft. Finally, the operational state of the landing gear is displayed on a visual display for further analysis.

Claims (27)

1 . A method for providing an operational state of a monitored landing gear of an aircraft, the method being performed by a system comprising electronic circuitry, the method comprising:

obtaining, in real-time, captured signals representative of an actual position of the monitored landing gear;

transforming the captured signals in a descriptor vector using Principal Components Analysis;

injecting the descriptor vector in a machine learning-based model trained and configured to transform descriptor vectors into equivalent operational states of landing gears, the equivalent operational states consisting of up-locked, up-unlocked, in-transit, down-unlocked, and down-locked;

providing an operational state of the monitored landing gear to avionics of the aircraft, the operational state identified as one of the equivalent operational states;

displaying the operational state of the landing gear for further analysis by the avionics; and

modifying, via the avionics, control surfaces of the aircraft responsive to the operational state of the landing gear.

2 . The method according to claim 1 , wherein the captured signals are captured images.

3 . The method according to claim 1 , wherein the images are captured by at least one video camera located in the aircraft in a vicinity of the monitored landing gear in such a way so as to capture the images of the monitored landing gear regardless of the operational state of the monitored landing gear.

4 . The method according to claim 1 , wherein, before the obtaining, the method comprises initializing the machine learning-based model by a computer system by:

obtaining a set of reference signals representative of candidate operational states of landing gears;

generating, in an un-supervised mode, a codebook of using Principal Components Analysis on the set of reference signals, the codebook gathering descriptor vectors obtained from the set of reference signals using Principal Components Analysis; and,

building the machine learning-based model, in a supervised mode, for labelling descriptor vectors with information representative of a corresponding operational state of landing gears.

5 . The method according to claim 4 , wherein the set of reference signals is a set of reference images comprising a plurality of images of each candidate operational state, captured with different lighting conditions, with different background interference, or both.

6 . A non-transitory storage medium storing a computer program comprising instructions which, when executed by a processor, perform the method according to claim 1 .

7 . A system for providing an operational state of a monitored landing gear of an aircraft, the system comprising:

at least one capturing device to capture signals of the monitored landing gear; and

electronic circuitry configured to:

obtain, in real-time, the captured signals representative of an actual position of the monitored landing gear from the at least one capturing device;

transform the captured signals in a descriptor vector using Principal Components Analysis;

inject the descriptor vector in a machine learning-based model trained and configured to transform descriptor vectors into equivalent operational states of landing gears, the equivalent operational states consisting of up-locked, up-unlocked, in-transit, down-unlocked, and down-locked;

provide an operational state of the monitored landing gear to avionics of the aircraft, the operational state identified as one of the equivalent operational states;

display the operational state of the landing gear for further analysis by the avionics; and

modify, via the avionics, control surfaces of the aircraft responsive to the operational state of the landing gear.

8 . An aircraft comprising:

at least one landing gear; and,

the system according to claim 7 .