Runway condition monitoring

• US 8,773,289 B2
• Filed: 03/24/2010
• Issued: 07/08/2014
• Est. Priority Date: 03/24/2010
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Maggiore, Jeanne C., Majkowski, Wayne R., Swearingen, Kevin L.
• Primary Examiner(s): Wu, Daniel
• Assistant Examiner(s): Terrell, Emily C
• Application Number:
  US12/730,594
• Publication Number:
  US 20130127642A1
• Time in Patent Office: 1,567 Days
• Field of Search: 340/947, 340/945, 340/958, 340/959, 340/961, 340/962
• US Class Current: 340/947
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0065 for taking-off
• CPC Class Codes: G08G 5/0091 for monitoring atmospheric conditions radar or analogous systems specially adapted for meteorological use G01S13/95; meteorology G01W
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913
• CPC Class Codes: G08G 5/065 Navigation or guidance aids, e.g. for taxiing or rolling

Abstract

A method and apparatus are present for monitoring a runway. Data is received about the runway from a number of sensors associated with an aircraft while the aircraft performs an operation on the runway. A number of conditions are identified for the runway using the data received from the number of sensors.

Claims

1. A method for monitoring a runway, the method comprising:

receiving data about the runway from a number of sensors associated with an aircraft while the aircraft performs an operation on the runway;

processing the data received from the number of sensors, wherein the processing is performed by a data processing system in the aircraft to produce processed data;

determining a number of conditions are present on the runway using the processed data; and

making predictions about the number of conditions present on the runway or other conditions that may develop on the runway at a future time using prognostic algorithms, the number of conditions, and historical data, wherein the data processing system makes the predictions, wherein the predictions include a rate of growth of a condition on the runway.

2. The method of claim 1 further comprising:

sending the number of conditions to a location remote to the aircraft.

3. The method of claim 2, wherein the aircraft is a first aircraft and the location is selected from one of a second aircraft and an air traffic controller.

4. The method of claim 1, wherein the aircraft is a first aircraft and further comprising:

controlling operation of a second aircraft using the runway after the first aircraft based on the number of conditions.

5. The method of claim 1, wherein the number of sensors being associated with the aircraft further comprises the number of sensors being mounted on an underside of a fuselage of the aircraft.

6. The method of claim 1, wherein the data received from the number of sensors includes at least one of imaging data, radar data, light detection and ranging data, camera data, or infrared data.

7. The method of claim 1, wherein the step of receiving the data about the runway from the number of sensors comprises:

identifying a braking distance for the aircraft braking on the runway;

determining that a condition in the number of conditions is present when the braking distance is greater than specified distance.

8. The method of claim 7 further comprising:

determining whether the condition in the number of conditions is present when a directional vector of the aircraft and a directional vector of a wheel on the aircraft are different.

9. The method of claim 1, wherein the number of conditions are selected from at least one of an inconsistency in the runway, a debris, an indentation, or a plant growth extending onto the runway.

10. The method of claim 2, wherein the location is a surface friction database.

11. The method of claim 1 further comprising:

updating a navigational chart with the number of conditions.

15. The method of claim 1, wherein the data processing system uses situational awareness to determine the number of conditions using the processed data.

16. The method of claim 15, wherein the situational awareness comprises aircraft operational data or weather data.

17. The method of claim 15, wherein the situational awareness comprises a combination of temperature data, weather data, airspeed, weight on wheels of the aircraft, angle of attack of the aircraft, weather forecast data.

18. The method of claim 1 further comprising:

determining whether a condition in the number of conditions is present when a directional vector of the aircraft and a directional vector of a wheel on the aircraft are different.

19. The method of claim 1, wherein processing the data received from the number of sensors comprises:

filtering the data, wherein filtering comprises removing noise from the data, and checking validity of the data; and

extracting features from the data, wherein extracting the features from the data comprises performing a transform on the data.

20. The method of claim 1, wherein processing the data received from the number of sensors results in a numerical representation, and wherein determining a number of conditions are present on the runway using the processed data includes comparing the numeral representation with a predetermined value to determine whether a particular type of data indicates the presence of a type of condition on the runway.

12. An apparatus comprising:

a number of sensors associated with an aircraft, wherein the number of sensors is configured to generate data about a runway while the aircraft performs an operation on the runway;

a computer system in the aircraft, wherein the computer system is configured to receive the data from the number of sensors, process the data received from the number of sensors to produce processed data, determine a number of conditions present on the runway using the processed data, and make predictions about the number of conditions present on the runway or other conditions that may develop on the runway at a future time using prognostic algorithms, the number of conditions, and historical data, wherein the data processing system makes the predictions, wherein the predictions include a rate of growth of a condition on the runway.

13. The apparatus of claim 12, wherein the aircraft is a first aircraft and wherein the computer system is further configured to control operation of a second aircraft using the runway after the first aircraft using the number of conditions.

14. The apparatus of claim 12, wherein the number of sensors being associated with the aircraft further comprises the number of sensors being mounted on an underside of a fuselage of the aircraft.