Sensor network

Patent metadata

Field	Value
Publication number	US-11753180-B2
Application number	US-202017111139-A
Country	US
Kind code	B2
Filing date	Dec 3, 2020
Priority date	May 27, 2016
Publication date	Sep 12, 2023
Grant date	Sep 12, 2023

Abstract

A sensor network for use in an aircraft, including a plurality of wireless nodes. A first wireless node of the plurality of wireless nodes is arranged to communicate with at least one other wireless node of the plurality of wireless nodes. The communication is via a secure communications channel and is on the basis of a control message received at the first wireless node. The at least one other wireless node is arranged to perform an operation on the basis of the control message.

First claim

The invention claimed is:

1. An aircraft sensor network on an aircraft, the aircraft sensor network comprising:
a plurality of wireless nodes located on at least one landing gear of the aircraft;
wherein a first wireless node of the plurality of wireless nodes is arranged to receive, over a first communications channel, from a remote computing device outside of and separate from the aircraft and the aircraft sensor network, at least one replacement cryptographic key and at least one control message to replace a current cryptographic key currently in use to secure communications transmitted over a secure second communications channel between the wireless nodes in the aircraft sensor network, and to communicate the at least one replacement cryptographic key to a second wireless node of the plurality of wireless nodes via the secure second communications channel which is different from the first communications channel,
wherein the second wireless node is arranged to perform at least one operation based on the at least one control message, wherein the at least one operation includes a configuration operation to replace the current cryptographic key with the at least one replacement cryptographic key,
wherein the first communications channel is a short-range wireless communications channel which operates on a radio frequency distinct from a radio frequency of the second communications channel,
wherein the first wireless node includes a communications interface configured to interface with the first communications channel over which is received the at least one replacement cryptographic key from the remote computing device, and
wherein the at least one operation comprises replacing, as a cryptographic key which secures the secure second communications channel, the current cryptographic key with the at least one replacement cryptographic key.

2. The aircraft sensor network of claim 1 , further comprising communicating using the at least one replacement cryptographic key in place of the current cryptographic key to secure communications over the second communications channel.

3. The aircraft sensor network of claim 2 , wherein the configuration operation comprises causing the second wireless node to send the at least one replacement cryptographic key to a third wireless node of the plurality of wireless nodes over the secure second communications channel in a communications encrypted by the current key.

4. The aircraft sensor network of claim 2 , wherein the sensor network is arranged to secure the secure second communications channel using the at least one replacement cryptographic key.

5. The aircraft sensor network of claim 4 , wherein the at least one control message comprises either a request for data stored on the sensor network to be sent to the first wireless node or an instruction to replace the current cryptographic key with the at least one replacement cryptographic key.

6. The aircraft sensor network of claim 5 , wherein the configuration operation comprises communicating the data to the first wireless node via the secure second communications channel.

7. The aircraft sensor network of claim 1 , wherein the first wireless node is a wireless sensor node and the second wireless node is a wireless access point.

8. The aircraft sensor node of claim 1 , wherein the short-range wireless communications channel has a maximum communication range of no more than 20 meters.

9. An aircraft wireless node configured for use in a sensor network in an aircraft, the sensor network comprising a plurality of wireless nodes each located on at least one landing gear of the aircraft, and each of the wireless nodes is configured to:
receive at least one control message and at least one replacement cryptographic key from a remote computing device communicating with a first wireless node of the wireless nodes over a first communication channel, wherein the remote control device is separate from the aircraft; and
communicate with at least one other wireless node of the plurality of wireless nodes of the sensor network, via a secure second communications channel, based on the at least one control message, wherein the secure second communications channel is secured by a current cryptographic key,
wherein the communication includes the first wireless node sending at least one replacement cryptographic key and the control message over the secure second communications channel,
wherein the first communication channel is on a radio frequency distinct from a radio frequency of the secure second communications channel,
wherein the remote computer device is outside of the aircraft sensor network and is external to the aircraft,
wherein the first wireless node includes a communications interface configured to interface with the first communications channel over which is received the at least one replacement cryptographic key from the remote computing device, and
wherein the at least one control message causes the at least one other wireless node to replace the current cryptographic key with the at least one replacement cryptographic key and use the at least one replacement cryptograph key to secure the second communications channel.

10. The aircraft wireless node of claim 9 , the aircraft wireless node is arranged to:
communicate, via the secure communications channel, with at least one other wireless node of the plurality of wireless nodes of the sensor network; and
perform an operation based on the communication via the secure communications channel, the operation being on the basis of a control message received at the at least one other wireless node.

11. The aircraft wireless node of claim 9 , wherein the first wireless node includes a first storage for storing the at least one replacement cryptographic key and a second storage for storing another cryptographic key wherein the first storage and second storage are isolated from each other.

12. The aircraft wireless node of claim 9 , wherein the first communications channel has a maximum communications range of no more than 20 meters.

13. An aircraft comprising the sensor network of claim 1 .

14. A method of operating a sensor network in an aircraft, the sensor network comprising a plurality of wireless nodes mounted on at least one landing gear of the aircraft, the method comprising:
a remote computing device wirelessly transmitting a control message and a replacement cryptographic key, via a first communication channel, to a first wireless node of the plurality of wireless nodes, wherein the remote computing device is outside of and separate from the aircraft and the sensor network;
the first wireless node communicating, via a secure second communications channel with a second wireless node of the plurality of wireless nodes of the sensor network, wherein the communicating includes sending the replacement cryptographic key and the control message; and
the second wireless node performing an operation on the basis of the control message, wherein the operation includes replacing the current cryptographic key with the replacement cryptographic key,
wherein the secure second communications channel is on a radio frequency distinct from a radio frequency of the first communications channel,
wherein the first wireless node includes a communications interface configured to interface with the first communications channel over which is received the at least one replacement cryptographic key from the remote computing device,
wherein the secure second communications channel is secured by a current cryptographic key, and
wherein the operation performed on the basis of the control message comprises replacing the curr

Assignees

• Airbus Operations Ltd
• Airbus Operations Gmbh

Inventors

• Bill Andrew
• Bruggemann Kurt
• Warns Timo

Classifications

• B64D45/00 Primary

  Aircraft indicators or protectors not otherwise provided for · CPC title

• H04W12/04 Primary

  Key management, e.g. using generic bootstrapping architecture [GBA] · CPC title

• H04L63/045

  wherein the sending and receiving network entities apply hybrid encryption, i.e. combination of symmetric and asymmetric encryption (cryptographic mechanisms or cryptographic arrangements using a plurality of keys or algorithms H04L9/14) · CPC title

• H04L63/0492

  by using a location-limited connection, e.g. near-field communication or limited proximity of entities · CPC title

• H04L63/062

  for key distribution, e.g. centrally by trusted party (cryptographic mechanisms or cryptographic arrangements for key distribution involving a central third party H04L9/0819) · CPC title