System and method for runway selection through scoring

1. A method suitable for use onboard an aircraft, executable by a processor, for selecting a runway for an aircraft, comprising:

receiving, from a runway database, runway data for a first runway and a second runway;

receiving, from a positioning subsystem, an aircraft position;

receiving, from sensors, aircraft data comprising an aircraft heading relative to the first runway and an aircraft heading relative to the second runway;

creating, for the first runway, a first boundary envelope surrounding the first runway, a second boundary envelope surrounding the first boundary envelope, and a third boundary envelope surrounding the second boundary envelope, each envelope having a predetermined number of points;

creating, for the second runway, a fourth boundary envelope surrounding the second runway, a fifth boundary envelope surrounding the fourth boundary envelope, and a sixth boundary envelope surrounding the fifth boundary envelope, each envelope having a predetermined number of points;

scoring the first runway, creating a first runway score, based on a combination of (i) the aircraft position with respect to the first runway, and (ii) a number of points associated with boundary envelopes surrounding the first runway within which the aircraft heading falls;

scoring the second runway, creating a second runway score based on a combination of (i) the aircraft position with respect to the second runway, and (ii) a number of points associated with boundary envelopes surrounding the second runway within which the aircraft heading falls; and

selecting the first or the second runway based on the first runway score and the second runway score.

2. The method of claim 1 , wherein the first, second, and third boundary envelopes are part of a first plurality of boundary envelopes surrounding the first runway, each having a predetermined number of points.

3. The method of claim 2 wherein the first plurality of boundary boxes are concentric.

4. The method of claim 3 wherein a runway boundary serves as an additional boundary envelope.

5. The method of claim 1 , wherein:

the first, second, and third boundary envelopes are part of a plurality of angularly inclusive boundary envelopes, each envelope sharing an origin that coincides with a landing position of the aircraft, and extending plus and minus a predetermined angular distance from a runway centerline of the first runway, and

the fourth, fifth, and sixth boundary envelopes are part of a plurality of angularly inclusive boundary envelopes, each envelope sharing an origin that coincides with the landing position of the aircraft, and extending plus and minus a predetermined angular distance from a runway centerline of the second runway.

6. The method of claim 5 wherein:

the first envelope extends plus and minus substantially five degrees, the second envelope extends substantially plus and minus substantially twelve degrees, and the third envelope extends substantially plus and minus substantially twenty degrees from the first runway centerline; and

the fourth envelope extends plus and minus substantially five degrees, the second envelope extends substantially plus and minus substantially twelve degrees, and the third envelope extends substantially plus and minus substantially twenty degrees from the second runway centerline.

7. The method of claim 6 wherein each of the first, second, and third envelopes each represent a predetermined score.

8. The method of claim 5 , wherein the angle is modulated by a predetermined parameter.

9. The method of claim 8 wherein the predetermined parameter is ground speed.

10. A method, executable by a processor, for selecting a runway, comprising:

retrieving runway feature data for first and second runways;

retrieving aircraft data including aircraft heading with respect to bearing of the first and second runways;

creating, for the first runway, a first plurality of concentric boundary envelopes surrounding the first runway, each envelope having a predetermined number of points;

creating, for the second runway, a second plurality of concentric boundary envelopes surrounding the second runway, each envelope having a predetermined number of points;

scoring the first runway based on a combination of (i) the aircraft position with respect to the first runway, and (ii) a number of the first plurality of boundary envelopes within which the aircraft heading falls;

scoring the second runway based on a combination of (i) the aircraft position with respect to the second runway, and (ii) a number of the second plurality of boundary envelopes within which the aircraft heading falls; and

selecting the first runway or the second runway based on the respective runway score.

11. The method of claim 10 wherein:

the first, second, and third boundary envelopes are part of a plurality of angularly inclusive boundary envelopes, each envelope sharing an origin that coincides with a landing position of the aircraft, and extending plus and minus a predetermined angular distance from a runway centerline of the first runway; and

the fourth, fifth, and sixth boundary envelopes are part of a plurality of angularly inclusive boundary envelopes, each envelope sharing an origin that coincides with the landing position of the aircraft, and extending plus and minus a predetermined angular distance from a runway centerline of the second runway.

12. A system for selecting a runway from first and second runways, comprising:

a runway database, providing runway data for a first runway and a second runway, wherein runway data comprises runway length and width, runway center points, runway center line and endpoints, runway bearing, runway true heading and runway reference point of origin;

a positioning subsystem, providing an aircraft position;

sensors, providing aircraft data comprising an aircraft heading relative to the first runway bearing and second runway bearing, respectively;

a processor coupled to the runway database, positioning subsystem, and sensors and configured to

create, for the first runway, a first boundary envelope surrounding the first runway, a second boundary envelope surrounding the first boundary envelope, and a third boundary envelope surrounding the second boundary envelope, each envelope having a predetermined number of points;

create, for the second runway, a fourth boundary envelope surrounding the second runway, a fifth boundary envelope surrounding the fourth boundary envelope, and a sixth boundary envelope surrounding the fifth boundary envelope, each envelope having a predetermined number of points;

scoring the first runway, creating a first runway score, based on a combination of (i) the aircraft position with respect to the first runway, and (ii) a number of points associated with boundary envelopes surrounding the first runway within which the aircraft heading falls;

scoring the second runway, creating a second runway score based on a combination of (i) the aircraft position with respect to the second runway, and (ii) a number of points associated with boundary envelopes surrounding the second runway within which the aircraft heading falls; and

select the first runway or the second runway based on the respective runway score.

13. The system of claim 12 wherein the processor is further configured to generate,

the first, second, and third boundary envelopes as part of a first plurality of angularly inclusive boundary envelopes, each envelope sharing an origin that coincides with a landing position of the aircraft, and extending plus and minus a predetermined angular distance from a runway centerline of the first runway; and

the fourth, fifth, and sixth boundary envelopes as part of a second plurality of angularly inclusive boundary envelopes, each envelope sharing an origin that coincides with the landing position of the aircraft, and extending plus and minus a predetermined angular distance from a runway centerline of the second runway.