Systems and methods for generating aircraft height data and employing such height data to validate altitude data

• US 8,659,471 B1
• Filed: 07/29/2011
• Issued: 02/25/2014
• Est. Priority Date: 07/29/2011
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: McCusker, Patrick D.
• Primary Examiner(s): Sotomayor, John B
• Assistant Examiner(s): WINDRICH, MARCUS E
• Application Number:
  US13/193,788
• Time in Patent Office: 942 Days
• Field of Search: 342 33- 35, 342/118, 342140-146
• US Class Current: 342/123
• CPC Class Codes: G01S 13/882 for altimeters measuring height using barometric means G01C5/06
• CPC Class Codes: G01S 13/935 for terrain-avoidance
• CPC Class Codes: G01S 7/22 Producing cursor lines and indicia by electronic means

Abstract

Present novel and non-trivial systems and methods for generating aircraft height data are disclosed. A processor is configured to receive both first data comprised of radar-based reflection data of a stationary reference point based upon a horizontal distance between the geographic position of an aircraft and the geographic position of the stationary reference point (e.g., landing threshold point) and second data comprised of internally sourced vertical travel data more frequently than the first data. From the first data and second data, an instant vertical distance above the stationary reference point is determined by updating the first data with the second data. Then, instant height data representative of the instant vertical distance above the stationary reference point is generated. Provided with the instant height data, a presentation system comprised of display unit, aural alert unit and/or a tactile alert unit may present the instant vertical distance to the pilot.

Claims

1. A system for generating aircraft height data, such system comprising:

a source of airborne radar-based reflection data;

at least one source of navigation data; and

a processor configured to

receive at a first rate first data comprised of airborne radar-based reflection data of a conventional, stationary reference point, where

the conventional, stationary reference point is defined by at least a known geographic position,

receive at a second rate second data comprised of internally-sourced vertical travel data provided by at least one source of navigation data, where

the second rate is greater than the first rate,

determine an instant vertical distance above the conventional, stationary reference point by updating the first data with the second data in between each period in which the first data is received, and

generate instant height data representative of the instant vertical distance above the conventional, stationary reference point.

2. The system of claim 1, wherein the conventional, stationary reference point is a landing threshold point of a runway.

3. The system of claim 1, wherein

the airborne radar-based reflection data of the conventional, stationary reference point is representative of

a measured vertical distance above the conventional, stationary reference point, where

the measured vertical distance has been determined as a function of elevation angle and range measurements, or

elevation angle and range measurements from which a measured vertical distance above the conventional, stationary reference point is determined by the processor.

4. The system of claim 1, wherein the internally-sourced vertical travel data is comprised of blended vertical travel data derived by subjecting vertical travel data from at least two sources of navigation data to a blending algorithm.

5. The system of claim 1, wherein

the processor is further configured to

blend the internally-sourced vertical travel data if the internally-sourced vertical travel data is received from at least two sources of navigation data.

6. The system of claim 1, further comprising:

a presentation system configured to

receive the instant height data, where

the processor has been further configured to provide the instant height data to the presentation system, and

present the instant vertical distance above the conventional, stationary reference point represented in the instant height data, whereby

the instant vertical distance is presented

visually on the screen of a display unit,

aurally through an aural alert unit,

tactilely through a tactile alert unit, or

any combination thereof.

7. The system of claim 1, further comprising:

a source of reference point data, such that

the processor is further configured to

receive navigation data comprised of first altitude data representative of a first altitude of the aircraft,

receive reference point data comprised of elevation data representative of the elevation of the conventional, stationary reference point,

determine second altitude data representative of a second altitude of the aircraft as a function of the instant height data and the elevation data,

determine a validity of the first altitude data by comparing the first altitude data with the second altitude data, and

generate validity advisory data responsive to the validity determination, where

the validity advisory data is representative of validity information.

8. The system of claim 7, wherein

the first altitude data is determined to be valid when

a tolerance limit is employed and defined, and

the difference between the first altitude data and the second altitude data is within the tolerance limit.

9. A system for employing aircraft height data to validate aircraft altitude data, such system comprising:

a source of instant height data;

a source of navigation data;

a source of reference point data; and

a processor configured to

receive instant height data representative of an instant vertical distance above a conventional, stationary reference point, where

the conventional, stationary reference point is defined by at least a known geographic position, and

the instant height data is based upon airborne radar-based reflection data that is updated by vertical travel data,

receive navigation data comprised of first altitude data representative of a first altitude of the aircraft,

receive reference point data comprised of elevation data representative of the elevation of the conventional, stationary reference point,

determine second altitude data representative of a second altitude of the aircraft as a function of the instant height data and the elevation data,

determine a validity of the first altitude data by comparing the first altitude data with the second altitude data, and

generate validity advisory data responsive to the validity determination, where the validity advisory data is representative of validity information.

10. The system of claim 9, wherein

the first altitude data is determined to be valid when

a tolerance limit is employed and defined, and

the difference between the first altitude data and the second altitude data is within the tolerance limit.

11. The system of claim 9, further comprising:

a presentation system configured to

receive the validity advisory data from the processor, where

the processor has been further configured to provide the validity advisory data to the presentation system, and

present the validity information represented in the validity advisory data, whereby

such validity information is presented

visually on the screen of a display unit,

aurally through an aural alert unit,

tactilely through a tactile alert unit, or

any combination thereof.

12. A method for generating aircraft height data, such method comprising:

Performing the following elements, where such elements are performed by a processor;

receiving at a first rate first data comprised of airborne radar-based reflection data of a conventional, stationary reference point, where

the conventional, stationary reference point is defined by at least a known geographic position;

receiving at a second rate second data comprised of internally-sourced vertical travel data provided by at least one source of navigation data, where

the second rate is greater than the first rate;

determining an instant vertical distance above the conventional, stationary reference point by updating the first data with the second data in between each period in which the first data is received; and

generating instant height data representative of the instant vertical distance above the conventional, stationary reference point.

13. The method of claim 12, wherein the conventional, stationary reference point is a landing threshold point of a runway.

14. The method of claim 12, wherein

the airborne radar-based reflection data of the conventional, stationary reference point is representative of

a measured vertical distance above the conventional, stationary reference point, where

the measured vertical distance has been determined as a function of elevation angle and range measurements, or

elevation angle and range measurements from which a measured vertical distance above the conventional, stationary reference point is determined.

15. The method of claim 12, wherein the internally-sourced vertical travel data is comprised of blended vertical travel data derived by subjecting vertical travel data from at least two sources of navigation data to a blending algorithm.

16. The method of claim 12, further comprising:

blending the internally-sourced vertical travel data if the internally-sourced vertical travel data is received from at least two sources of navigation data.

17. The method of claim 12, further comprising:

providing the instant height data to a presentation system configured to present the instant vertical distance above the conventional, stationary reference point represented in the instant height data, whereby

such instant vertical distance is presented

visually on the screen of a display unit,

aurally through an aural alert unit,

tactilely through a tactile alert unit, or

any combination thereof.

18. The method of claim 12, further comprising:

receiving navigation data comprised of first altitude data representative of a first altitude of the aircraft;

receiving reference point data comprised of elevation data representative of the elevation of the conventional, stationary reference point,

determining second altitude data representative of a second altitude of the aircraft as a function of the instant height data and the elevation data;

determining a validity of the first altitude data by comparing the first altitude data with the second altitude data; and

generating validity advisory data responsive to the validity determination, where

the validity advisory data is representative of validity information.

19. The method of claim 18, wherein

the first altitude data is determined to be valid when

a tolerance limit is employed and defined, and

the difference between the first altitude data and the second altitude data is within the tolerance limit.

20. A method for employing aircraft height data to validate aircraft altitude data, such method comprising:

receiving instant height data representative of an instant vertical distance above a conventional, stationary reference point, where

the conventional, stationary reference point is defined by at least a known geographic position, and

the instant height data is based upon airborne radar-based reflection data that is updated by vertical travel data;

receiving navigation data comprised of first altitude data representative of a first altitude of the aircraft;

receiving reference point data comprised of elevation data representative of the elevation of the conventional, stationary reference point;

determining second altitude data representative of a second altitude of the aircraft as a function of the instant height data and the elevation data;

determining a validity of the first altitude data by comparing the first altitude data with the second altitude data; and

generating validity advisory data responsive to the validity determination, where the validity advisory data is representative of validity information.

21. The method of claim 20, wherein

the first altitude data is determined to be valid when

a tolerance limit is employed and defined, and

the difference between the first altitude data and the second altitude data is within the tolerance limit.

22. The method of claim 20, further comprising:

providing the validity advisory data to a presentation system configured to present the validity information represented in the validity advisory data, whereby

such validity information is presented

visually on the screen of a display unit,

aurally through an aural alert unit,

tactilely through a tactile alert unit, or

any combination thereof.