Aircraft landing event system and method
An aircraft landing event system is disclosed including a processor, the processor being configured to receive aircraft braking performance information from a plurality of aircraft that have performed a landing event on a particular runway. The processor is configured to determine an aircraft braking performance indicator on the basis of the aircraft braking performance information of the plurality of aircraft, and communicate the aircraft braking performance indicator to an aircraft landing system of an approaching aircraft that is about to perform a landing event on the particular runway.
1. An aircraft landing event system, comprising:
a receiver configured to receive aircraft braking performance information from a plurality of aircraft that have performed a landing event on a particular runway;
a processor configured to determine an aircraft braking performance indicator on the basis of the aircraft braking performance information of the plurality of aircraft;
a transmitter configured to communicate the aircraft braking performance indicator to an aircraft landing system of an approaching aircraft that is about to perform a landing event on the particular runway;
wherein the processor is configured to cause control of at least a part of the landing system of the approaching aircraft based on the transmitted aircraft braking performance indicator; and,
wherein the aircraft braking performance information received by the processor, for each one of the plurality of aircraft, comprises
a wheel slip,
a braking force,
a braking torque,
a friction coefficient of the runway, or
a maximum reactive force between one or more wheels of the landed aircraft and the runway,
wherein the aircraft braking performance information is determined by a braking system of the respective aircraft during the respective landing event as a function of respective position of respective aircraft in both a longitudinal and a lateral direction of the runway, and
wherein the processor is configured to control the braking system of the approaching aircraft based on the transmitted aircraft braking performance indicator and determine a landing distance of the approaching aircraft on the runway.
2. The aircraft landing event system of claim 1 , wherein the aircraft braking performance information received by the processor comprises, for each one of the plurality of aircraft, a wheel slip determined by a braking system of the respective aircraft during the respective landing event.
3. The aircraft landing event system of claim 1 , wherein the aircraft braking performance information received by the processor comprises, for each one of the plurality of aircraft, an aircraft braking performance profile defining the aircraft braking performance information as a function of a position of the respective aircraft on the runway during the respective landing event.
4. The aircraft landing event system of claim 1 , wherein, to determine the braking performance indicator, the processor is configured to determine an average of the aircraft braking performance information.
5. The aircraft landing event system of claim 1 , wherein, to determine the aircraft braking performance indicator, the processor is configured to determine a weighted average of the aircraft braking performance information.
6. The aircraft landing event system of claim 5 , wherein the weighted average aircraft braking performance indicator is weighted towards aircraft braking performance information of more recent landing events.
7. The aircraft landing event system of claim 1 , wherein the processor is configured to determine a deviation of the aircraft braking performance information of the most recent landing event from the aircraft performance information of an earlier landing event.
8. The aircraft landing event system of claim 7 , wherein, in the event the deviation determined by the processor is less than a threshold deviation, the processor is configured to determine the aircraft braking performance indicator on the basis of the aircraft braking performance information received from the plurality of aircraft.
9. The aircraft landing event system of claim 8 wherein, in an event the deviation determined by the processor exceeds the threshold deviation, the processor is configured to discard the aircraft braking performance information received from the plurality of aircraft and determine the aircraft braking performance indicator to be a predetermined aircraft braking performance indicator.
10. The aircraft landing event system of claim 1 , wherein the processor is configured to determine, for the aircraft braking performance information received by the processor from each one of the plurality of aircraft, an elapsed time since the respective landing event occurred.
11. The aircraft landing event system of claim 10 , wherein only the aircraft braking performance information for which the elapsed time is within a predetermined elapsed time threshold is used by the processor to determine the aircraft braking performance indicator.
12. The aircraft landing event system of claim 1 , wherein the processor is configured to determine, based on the aircraft braking performance indicator, a landing distance of the approaching aircraft on the runway.
13. The aircraft landing event system of claim 12 , wherein instead of, or in addition to, communicating the aircraft braking performance indicator to the approaching aircraft, the processor is configured to communicate the landing distance determined by the processor to the approaching aircraft.
14. A method of determining an aircraft braking performance indicator, comprising:
receiving aircraft braking performance information from a plurality of aircraft that have performed a landing event on a particular runway;
providing a processor, wherein the processor is configured to determine an aircraft braking performance indicator on a basis of the aircraft braking performance information of the plurality of aircraft;
communicating the aircraft braking performance indicator to an aircraft landing system of an approaching aircraft that is about to perform a landing event on the particular runway;
wherein the processor is configured to cause control of at least a part of the landing system of the approaching aircraft based on the transmitted aircraft braking performance indicator;
wherein the aircraft braking performance information received by the processor, for each one of the plurality of aircraft, comprises
a wheel slip,
a braking force,
a braking torque,
a friction coefficient of the runway, or
a maximum reactive force between one or more wheels of the landed aircraft and the runway,
wherein the aircraft braking performance information is determined by a braking system of the respective aircraft during the respective landing event as a function of respective position of respective aircraft in both a longitudinal and a lateral direction of the runway, and
wherein the processor is configured to control the braking system of the approaching aircraft based on the transmitted aircraft braking performance indicator and determine a landing distance of the approaching aircraft on the runway.
15. A non-transitory, computer-readable storage medium storing instructions that, when executed by a processor, is configured to perform the method of claim 14 .
16. An aircraft comprising the aircraft landing event system of claim 1 .
17. An aircraft comprising the non-transitory computer-readable storage medium of claim 15 .