Apparatus and method for windshear data processing

• US 5,539,409 A
• Filed: 06/30/1994
• Issued: 07/23/1996
• Est. Priority Date: 06/30/1994
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Westinghouse Electric Corporation (Paramount Global (f/k/a ViacomCBS Inc.))
• Inventors: Railey, Guy T., Miller, Fran, Albano, Michael J., Mathews, Bruce D.
• Primary Examiner(s): Sotomayor, John B.
• Application Number:
  US08/269,321
• Time in Patent Office: 754 Days
• Field of Search: 342/26, 342/460, 342/196, 342/91, 342/92, 342/93
• US Class Current: 342/26.00B
• CPC Class Codes: G01S 13/953 mounted on aircraft
• CPC Class Codes: Y02A 90/10 Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Abstract

The present invention improves upon conventional windshear data processing techniques in three mutually exclusive aspects. First, the present invention provides an improved method and system for detecting microburst downdraft candidates. The improvement lies in its capability of detecting multiple candidates in range. Because of the added capability to detect multiple candidates in range, the present invention also provides an improved method and system for azimuthal association of the multiple candidates in range to define an accurate locus of headwind and tailwind pairs. Second, the present invention provides an improvement in that it utilizes a non-circularly symmetric spatial model to compute the vertical component of a total hazard factor. Third, the present invention provides an improvement in the accurate detection of small radii microbursts by correcting bias present in the data from which the small radii microbursts may be detected.

Claims

1. A radar system for determining a vertical component of a total hazard factor of a microburst, comprising:

means for scanning the atmosphere at an upper altitude and identifying said microburst;

means for deriving spatial parameters of a non-circularly symmetric velocity model of said identified microburst;

means for determining an upper horizontal outflow velocity of said identified microburst using said non-circularly symmetric velocity model;

means for scanning the atmosphere at a lower altitude;

means for modifying said spatial parameters of said non-circularly symmetric velocity model to correspond to the shape of said identified microburst at said lower altitude;

means for determining a lower horizontal outflow velocity of said identified microburst using said modified non-circularly symmetric velocity model; and

means for computing said vertical component of said total hazard factor from said upper horizontal outflow velocity, said lower horizontal outflow velocity, said modified spatial parameters of said non-circularly symmetric velocity model.

2. The radar system recited in claim 1, wherein the non-circularly symmetric velocity model is an elliptical velocity model having an elliptical boundary.

3. The radar system recited in claim 2, wherein the elliptical boundary has an oval racetrack shape defined by two separated halves of a circle coupled to each other by two substantially parallel and substantially straight lines.

4. The radar system recited in claim 3, wherein said means for determining an upper horizontal outflow velocity and said means for determining a lower horizontal outflow velocity each includes:

means for calculating, at a plurality of points along the elliptical boundary, a plurality of velocity vectors, said calculating means employing a set of circular geometric compensation rules for the two separated halves of the circle and a set of linear geometric compensation rules for the two substantially parallel and substantially straight lines;

means for calculating a plurality of path lengths between said plurality of points, each of said plurality of path lengths corresponding to the distance along the elliptical boundary between an adjacent pair of said plurality of points;

means for accumulating said plurality of velocity vectors and for accumulating said plurality of path lengths; and

means for normalizing said accumulated velocity vectors and said accumulated path lengths.

5. The radar system recited in claim 4, further comprising means for generating a radar sight line and for measuring a velocity data value along said radar sight line for each of the plurality of points,

wherein the means for calculating the plurality of velocity vectors comprises, for each of the plurality of points, means for determining an angle between said radar sight line and a vector normal to the elliptical boundary, and means for compensating said velocity data value by said angle to obtain the velocity vector.

6. A method for determining a vertical component of a total hazard factor of a microburst, comprising:

radar scanning the atmosphere at an upper altitude and identifying said microburst;

deriving spatial parameters of a non-circularly symmetric velocity model of said identified microburst;

determining an upper horizontal outflow velocity of said identified microburst using said non-circularly symmetric velocity model;

radar scanning the atmosphere at a lower altitude;

modifying said spatial parameters of said non-circularly symmetric velocity model to correspond to the shape of said identified microburst at said lower altitude;

determining a lower horizontal outflow velocity of said identified microburst using said modified non-circularly symmetric velocity model; and

computing said vertical component of said total hazard factor from said upper horizontal outflow velocity, said lower horizontal outflow velocity, and said modified spatial parameters of said non-circularly symmetric velocity model.

7. The method recited in claim 6, wherein the non-circularly symmetric velocity model is an elliptical velocity model having an elliptical boundary.

8. The method recited in claim 7, wherein the elliptical boundary has an oval racetrack shape defined by two separated halves of a circle coupled to each other by two substantially parallel and substantially straight lines.

9. The method recited in claim 8, wherein the step of determining an upper horizontal outflow velocity and the step of determining a lower horizontal outflow velocity each includes the following substeps:

calculating, at a plurality of points along the elliptical boundary, a plurality of velocity vectors, said calculating substep employing a set of circular geometric compensation rules for the two separated halves of the circle and a set of linear geometric compensation rules for the two substantially parallel and substantially straight lines;

calculating a plurality of path lengths between said plurality of points, each of said plurality of path lengths corresponding to the distance along the elliptical boundary between an adjacent pair of said plurality of points;

accumulating said plurality of velocity vectors and said plurality of path lengths; and

normalizing said accumulated velocity vectors and said accumulated path lengths.

10. The method recited in claim 9, further comprising the step of generating a radar sight line and measuring a velocity data value along said radar sight line for each of the plurality of points,

wherein the substep of calculating the plurality of velocity vectors comprises, for each of the plurality of points, the substeps of determining an angle between said radar sight line and a vector normal to the elliptical boundary, and of compensating said velocity data value by said angle to obtain the velocity vector.

11. A radar system for determining a horizontal outflow velocity of a microburst, comprising:

means for identifying said microburst;

means for deriving an elliptical spacial model of said identified microburst, wherein the boundary of the elliptical spacial model is defined by two separated halves of a circle coupled to each other by two substantially parallel and substantially straight lines; and

means for calculating said horizontal outflow velocity from said elliptical spacial model.

12. The radar system recited in claim 11, wherein the calculating means includes means for calculating the horizontal outflow velocity at a plurality of altitudes.

13. A method for determining a horizontal outflow velocity of a microburst, comprising:

identifying said microburst using a radar system;

deriving an elliptical spacial model of said identified microburst, wherein the boundary of the elliptical spacial model is defined by two separated halves of a circle coupled to each other by two substantially parallel and substantially straight lines; and

calculating said horizontal outflow velocity from said elliptical spacial model.

14. The method recited in claim 13, wherein the calculating step includes the substep of calculating the horizontal outflow velocity at a plurality of altitudes.

15. A radar system for forming a microburst candidate, comprising:

means for incrementally scanning the atmosphere in an angular swath having a plurality of angle report points;

means for determining, at each of said plurality of angle report points, a peak headwind and a peak tailwind, each having a range from said radar system and a velocity;

means for detecting a start point of said microburst candidate;

means for detecting a stop point of said microburst candidate by comparing the range and velocity of the peak headwind and peak tailwind determined at a final incremental angle report point with the range and velocity determined at a previous incremental angle report point immediately preceding said final incremental angle report point; and

means for designating the width of said microburst candidate as the distance from said start point to said previous incremental angle report point.

16. The radar system recited in claim 15, further comprising means for restarting the incremental scanning means relative to the stop point.

17. The radar system recited in claim 15, wherein the detecting means includes means for determining whether the range and velocity of the peak headwind and/or peak tailwind determined at a target one of said plurality of angle report points substantially differs from the range and velocity of the angle report point immediately preceding said target report point.

18. A method for forming a microburst candidate using a radar system, comprising:

incrementally radar scanning the atmosphere in an angular swath having a plurality of angle report points using a radar system;

determining, at each of said plurality of angle report points, a peak headwind and a peak tailwind, each having a range from said radar system and a velocity;

detecting a start point of said microburst candidate;

detecting a stop point of said microburst candidate, including comparing the range and velocity of the peak headwind and peak tailwind determined at a final incremental angle report point with the range and velocity determined at a previous incremental angle report point immediately preceding said final incremental angle report point; and

designating the width of said microburst candidate as the distance from said start point to said previous incremental angle report point.

19. The method recited in claim 18, further comprising restarting the incremental radar scanning step relative to the stop point.

20. The method recited in claim 18, wherein the detecting step includes the substep of determining whether the range and velocity of the peak headwind and/or peak tailwind determined at a target one of said plurality of angle report points substantially differs from the range and velocity of the angle report point immediately preceding said target report point.

21. A radar system for forming a data string record representing a plurality of microburst candidates in range and determining whether each of said plurality of microburst candidates is a valid candidate, comprising:

antenna scanning means for incrementally scanning the atmosphere in a plurality of angle slices;

means for identifying a plurality of headwinds or tailwinds or headwinds and tailwinds in one of said plurality of angle slices;

means for writing in said data string record a reference range and a reference velocity for each of said headwind and/or tailwind;

means for updating said data string record for each of said plurality of angle slices;

means for terminating said data string record; and

means for determining whether any of said plurality of microburst candidates represented by said data string record is a valid candidate.

22. The radar system recited in claim 21, wherein the scanning means starts at an initial angle slice and the terminating means stops at a terminating angle slice, said system further comprising:

means for restarting the scanning means at an angle slice immediately following said initial angle slice if none of the plurality of microburst candidates is determined to be a valid candidate; and

means for restarting the scanning means at a final angle slice, said final angle slice immediately following said terminating angle slice, if at least one of the plurality of microburst candidates is determined to be a valid candidate.

23. The radar system recited in claim 22, wherein the updating means is activated if the range and velocity of each of the plurality of headwinds and/or tailwinds determined at an incremented angle slice substantially match a corresponding one of the reference range and the reference velocity;

and

wherein the terminating angle slice represents the last angle slice of said plurality of angle slices at which the updating means is activated.

24. The radar system recited in claim 21, wherein the scanning means scans over a predetermined scanning range;

and

wherein the identifying means includes means for determining a plurality of local maximum headwinds and/or tailwinds within said predetermined scanning range.

25. The radar system recited in claim 24, wherein the means for determining a plurality of local maximum headwinds and/or tailwinds includes means for establishing a plurality of range domains, each of said plurality of range domains encompassing one of the plurality of headwinds and/or tailwinds and being defined by at least one of a plurality of range gates, each of said plurality of range gates being defined by an incremental distance along a radar line-of-sight from the scanning means.

26. The radar system recited in claim 25, wherein each of the plurality of headwinds and/or tailwinds has either a commencing headwind and a terminating tailwind if a divergent windshear is present, or a commencing tailwind and a terminating headwind if a convergent windshear is present;

and

wherein each of the plurality of range domains begins at a commencing range gate and ends at a terminating range gate, said terminating range gate indicating the location along the radar line-of-sight of said terminating headwind or tailwind.

27. The radar system recited in claim 26, wherein, for each succeeding range domain, the commencing range gate has an offset distance along the radar line-of-sight from the terminating range gate of the preceding range domain.

28. The radar system recited in claim 27, wherein the offset distance is dependent on the incremental distance defining the plurality of range gates and on a determination of the minimum possible range between two microburst candidates.

29. A method for forming a data string record representing a plurality of microburst candidates in range and determining whether each of said plurality of microburst candidates is a valid candidate, comprising:

incrementally scanning the atmosphere in a plurality of angle slices;

identifying a plurality of headwinds or tailwinds or headwinds and tailwinds in one of said plurality of angle slices;

writing in said data string record a reference range and a reference velocity for each of said headwind and/or tailwind;

updating said data string record for each of said plurality of angle slices;

terminating said data string record; and

determining whether any of said plurality of microburst candidates represented by said data string record is a valid candidate.

30. The method recited in claim 29, wherein the scanning step starts at an initial angle slice and the terminating step stops at a terminating angle slice, the method further comprising:

reperforming the scanning step at an angle slice immediately following said initial angle slice if none of the plurality of microburst candidates is determined to be a valid candidate; and

reperforming the scanning step at a final angle slice, said final angle slice immediately following said terminating angle slice, if at least one of the plurality of microburst candidates is determined to be a valid candidate.

31. The method recited in claim 30, wherein the updating step is performed if the range and velocity of each of the plurality of headwinds and/or tailwinds determined at an incremented angle slice substantially match a corresponding one of the reference range and the reference velocity;

and

wherein the terminating angle slice represents the last angle slice of said plurality of angle slices at which the updating step occurs.

32. The method recited in claim 29, wherein the scanning step scans over a predetermined scanning range;

and

wherein the identifying step includes the substep of determining a plurality of local maximum headwinds and tailwinds within said predetermined scanning range.

33. The method recited in claim 32, wherein the step of determining a plurality of local maximum headwinds and tailwinds includes the substep of establishing a plurality of range domains, each of said plurality of range domains encompassing one of the plurality of headwinds and/or tailwinds and being defined by at least one of a plurality of range gates, each of said plurality of range gates being defined by an incremental distance along a radar line-of-sight.

34. The method recited in claim 33, wherein each of the plurality of headwinds and/or tailwinds has either a commencing headwind and a terminating tailwind if a divergent windshear is present, or a commencing tailwind and a terminating headwind if a convergent windshear is present;

and

wherein each of the plurality of range domains begins at a commencing range gate and ends at a terminating range gate, said terminating range gate indicating the location along the radar line-of-sight of said terminating headwind or tailwind.

35. The method recited in claim 34, wherein, for each succeeding range domain, the commencing range gate has an offset distance along the radar line-of-sight from the terminating range gate of the preceding range domain.

36. The method recited in claim 35, wherein the offset distance is dependent on the incremental distance defining the plurality of range gates and on a determination of the minimum possible range between two microburst candidates.

37. The method recited in claim 32, wherein the step of determining a plurality of local maximum headwinds and tailwinds functions independently of the plurality of range domains determined in a preceding one of the plurality of angle slices.

38. A radar system for detecting small outflow radii microbursts, comprising:

means for incrementally scanning the atmosphere in an angular swath having a plurality of angle report points;

means for determining, at each of said plurality of angle report points, the radar radial gradient of wind velocity;

means for determining a horizontal hazard factor map of wind velocities;

means for estimating bias errors in the determined horizontal hazard factor map;

means for correcting bias errors in the determined horizontal hazard factor map; and

means for identifying small radii microbursts based upon a horizontal hazard factor as provided in the corrected horizontal hazard factor map.

39. A method of detecting small outflow radii microbursts, comprising:

incrementally scanning the atmosphere in an angular swath having a plurality of angle report points;

determining, at each of said plurality of angle report points, the radar radial gradient of wind velocity;

determining a horizontal hazard factor map of wind velocities;

estimating bias errors in the determined horizontal hazard factor map;

correcting bias errors in the determined horizontal hazard factor map; and

identifying small radii microbursts based upon a horizontal hazard factor as provided in the corrected horizontal hazard factor map.