초록 ▼

A system and method for determining a predicted stopping performance of an aircraft moving on a runway. A predicted stopping force acting on the aircraft to stop the aircraft is determined by a processor unit as the aircraft is moving on the runway. A predicted deceleration of the aircraft moving on

A system and method for determining a predicted stopping performance of an aircraft moving on a runway. A predicted stopping force acting on the aircraft to stop the aircraft is determined by a processor unit as the aircraft is moving on the runway. A predicted deceleration of the aircraft moving on the runway is determined by the processor unit using the predicted stopping force acting on the aircraft to stop the aircraft. The predicted stopping performance of the aircraft on the runway is determined by the processor unit using the predicted deceleration of the aircraft.

대표청구항 ▼

1. A method for determining a predicted stopping performance of an aircraft moving on a runway, comprising: determining, by a processor unit, a predicted stopping force acting on the aircraft to stop the aircraft as the aircraft is moving on the runway;determining, by the processor unit, a predicted

1. A method for determining a predicted stopping performance of an aircraft moving on a runway, comprising: determining, by a processor unit, a predicted stopping force acting on the aircraft to stop the aircraft as the aircraft is moving on the runway;determining, by the processor unit, a predicted deceleration of the aircraft moving on the runway using the predicted stopping force acting on the aircraft to stop the aircraft;determining, by the processor unit, the predicted stopping performance of the aircraft on the runway using the predicted deceleration of the aircraft;determining a predicted stopping position of the aircraft with respect to the runway using the predicted deceleration of the aircraft; andsetting the predicted deceleration of the aircraft equal to a predicted deceleration for the aircraft due to maximum braking in response to a determination that an automatic braking system is active and the predicted deceleration of the aircraft due to maximum braking is less than a target deceleration for the aircraft of the automatic braking system. 2. The method of claim 1, wherein determining the predicted stopping force acting on the aircraft comprises: determining a predicted braking force provided by a braking system on the aircraft to stop the aircraft;determining a predicted thrust provided by a number of engines on the aircraft to stop the aircraft; anddetermining a predicted aerodynamic force provided by an aerodynamic system on the aircraft to stop the aircraft. 3. The method of claim 1, wherein determining the predicted stopping force acting on the aircraft comprises: identifying runway condition information indicating a condition of the runway; determining a current braking force provided by a braking system on the aircraft to stop the aircraft; anddetermining a predicted braking force provided by the braking system on the aircraft for each of a plurality of different speeds of the aircraft on the runway using the runway condition information, the current braking force provided by the braking system, and information identifying a relationship between the braking force provided by the braking system on the aircraft and a speed of the aircraft. 4. The method of claim 1, wherein determining the predicted stopping force acting on the aircraft comprises: in response to a determination that an amount of time since the aircraft touched down on the runway is less than a threshold time period, determining a predicted thrust provided by a number of engines on the aircraft to stop the aircraft using an assumption for operation of a thrust system on the aircraft to provide thrust by the number of engines on the aircraft to stop the aircraft; andin response to a determination that the amount of time since the aircraft touched down on the runway is greater than the threshold time period, determining the predicted thrust provided by the number of engines on the aircraft to stop the aircraft using an actual setting for the thrust system on the aircraft to provide the thrust by the number of engines on the aircraft to stop the aircraft. 5. The method of claim 1, wherein determining the predicted stopping force acting on the aircraft comprises: in response to a determination that an amount of time since the aircraft touched down on the runway is less than a threshold time period, determining a predicted aerodynamic force provided by an aerodynamic system on the aircraft to stop the aircraft using an assumption for operation of the aerodynamic system on the aircraft to provide aerodynamic force to stop the aircraft; andin response to a determination that the amount of time since the aircraft touched down on the runway is greater than the threshold time period, determining the predicted aerodynamic force provided by the aerodynamic system on the aircraft to stop the aircraft using an actual setting for the aerodynamic system on the aircraft to provide the aerodynamic force to stop the aircraft. 6. The method of claim 1, wherein: determining the predicted stopping performance of the aircraft on the runway comprises determining a predicted distance to stop for the aircraft using the predicted deceleration of the aircraft; and further comprising:providing an overrun warning in response to a determination that the predicted distance to stop for the aircraft is greater than a distance remaining from the aircraft to an undesirable position for stopping the aircraft with respect to the runway. 7. The method of claim 6 further comprising: identifying a length of the runway; andadjusting the predicted distance to stop for the aircraft based on the length of the runway. 8. The method of claim 1, further comprising: displaying an indication of the predicted stopping position of the aircraft with respect to a representation of the runway. 9. A method for displaying a predicted stopping position of an aircraft moving on a runway, comprising: identifying, by a processor unit, a current position of the aircraft on the runway;identifying, by the processor unit, a current speed of the aircraft on the runway;determining, by the processor unit, a predicted deceleration of the aircraft moving on the runway;determining, by the processor unit, the predicted stopping position of the aircraft with respect to the runway using the current position of the aircraft, the current speed of the aircraft, and the predicted deceleration of the aircraft;identifying a planned stopping performance for the aircraft with respect to the runway;displaying, at a same time, an indication of the predicted stopping position of the aircraft and an indication of the planned stopping performance for the aircraft with respect to a representation of the runway; andsetting the predicted deceleration of the aircraft equal to a predicted deceleration for the aircraft due to maximum braking in response to a determination that an automatic braking system is active and the predicted deceleration of the aircraft due to maximum braking is less than a target deceleration for the aircraft of the automatic braking system. 10. The method of claim 9, further comprising: determining a predicted braking force provided by a braking system on the aircraft to stop the aircraft;determining a predicted thrust provided by a number of engines on the aircraft to stop the aircraft;determining a predicted aerodynamic force provided by an aerodynamic system on the aircraft to stop the aircraft; anddetermining the predicted deceleration of the aircraft using the predicted braking force, the predicted thrust, and the predicted aerodynamic force. 11. The method of claim 10, wherein determining the predicted braking force provided by the braking system on the aircraft comprises: identifying runway condition information indicating a current condition of the runway;determining a current braking force provided by the braking system on the aircraft to stop the aircraft; anddetermining the predicted braking force provided by the braking system on the aircraft for each of a plurality of different speeds of the aircraft on the runway using the runway condition information, the current braking force provided by the braking system, and information identifying a relationship between the braking force provided by the braking system on the aircraft and a speed of the aircraft. 12. The method of claim 9, wherein determining the predicted deceleration of the aircraft moving on the runway comprises: in response to a determination that the automatic braking system for the aircraft is not active, setting the predicted deceleration of the aircraft equal to a selected one of a current deceleration of the aircraft and a predicted deceleration of the aircraft that is determined using a predicted stopping force acting on the aircraft to stop the aircraft as the aircraft is moving on the runway;setting the predicted deceleration of the aircraft equal to a predicted deceleration of the aircraft without brakes in response to a determination that the automatic braking system is active and the predicted deceleration of the aircraft without brakes is greater than or equal to the target deceleration for the aircraft of the automatic braking system; andotherwise setting the predicted deceleration of the aircraft equal to the target deceleration for the aircraft of the automatic braking system. 13. An apparatus, comprising: a stopping force predictor configured to determine a predicted stopping force acting on an aircraft to stop the aircraft as the aircraft is moving on a runway;a deceleration predictor configured to determine a predicted deceleration of the aircraft moving on the runway using the predicted stopping force acting on the aircraft to stop the aircraft; anda stopping performance predictor configured to: determine a predicted stopping performance of the aircraft on the runway using the predicted deceleration of the aircraft; anddetermine a predicted stopping position of the aircraft with respect to the runway using the predicted deceleration of the aircraft;wherein the predicted deceleration of the aircraft is set equal to a predicted deceleration for the aircraft due to maximum braking in response to a determination that an automatic braking system is active and the predicted deceleration of the aircraft due to maximum braking is less than a target deceleration for the aircraft of the automatic braking system. 14. The apparatus of claim 13, wherein the stopping force predictor is configured to: determine a predicted braking force provided by a braking system on the aircraft to stop the aircraft;determine a predicted thrust provided by a number of engines on the aircraft to stop the aircraft; anddetermine a predicted aerodynamic force provided by an aerodynamic system on the aircraft to stop the aircraft. 15. The apparatus of claim 13, wherein the stopping force predictor is configured to: identify runway condition information indicating a current condition of the runway;determine a current braking force provided by a braking system on the aircraft to stop the aircraft; anddetermine a predicted braking force provided by the braking system on the aircraft for each of a plurality of different speeds of the aircraft on the runway using the runway condition information, the current braking force provided by the braking system, and information identifying a relationship between the braking force provided by the braking system on the aircraft and a speed of the aircraft. 16. The apparatus of claim 13, wherein the stopping force predictor is configured to: in response to a determination that an amount of time since the aircraft touched down on the runway is less than a threshold time period, determine a predicted thrust provided by a number of engines on the aircraft to stop the aircraft using an assumption for operation of a thrust system on the aircraft to provide thrust by the number of engines on the aircraft to stop the aircraft; andin response to a determination that the amount of time since the aircraft touched down on the runway is greater than the threshold time period, determine the predicted thrust provided by the number of engines on the aircraft to stop the aircraft using an actual setting for the thrust system on the aircraft to provide the thrust by the number of engines on the aircraft to stop the aircraft. 17. The apparatus of claim 13, wherein the stopping force predictor is configured to: in response to a determination that an amount of time since the aircraft touched down on the runway is less than a threshold time period, determine a predicted aerodynamic force provided by an aerodynamic system on the aircraft to stop the aircraft using an assumption for operation of the aerodynamic system on the aircraft to provide the aerodynamic force to stop the aircraft; andin response to a determination that the amount of time since the aircraft touched down on the runway is greater than the threshold time period, determine the predicted aerodynamic force provided by the aerodynamic system on the aircraft to stop the aircraft using an actual setting for the aerodynamic system on the aircraft to provide the aerodynamic force to stop the aircraft. 18. The apparatus of claim 13, wherein the stopping performance predictor is configured to: determine a predicted distance to stop for the aircraft using the predicted deceleration of the aircraft; andgenerate an overrun warning in response to a determination that the predicted distance to stop for the aircraft is greater than a distance remaining from the aircraft to an undesirable position for stopping the aircraft with respect to the runway. 19. The apparatus of claim 18, wherein the stopping performance predictor is further configured to: identify a length of the runway; andadjust the predicted distance to stop for the aircraft based on the length of the runway. 20. The apparatus of claim 13, wherein the stopping performance predictor is configured to: generate a predicted stopping position display comprising an indication of the predicted stopping position of the aircraft with respect to a representation of the runway.