Windshear radar system with upper and lower elevation radar scans

• US 5,311,183 A
• Filed: 06/13/1991
• Issued: 05/10/1994
• Est. Priority Date: 06/13/1991
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Westinghouse Electric Company LLC (Brookfield Asset Management Incorporated)
• Inventors: Mountcastle, Paul D., Patterson, Walter W., Mathews, Bruce D.
• Primary Examiner(s): TUBBESING, THEODORE
• Application Number:
  US07/714,133
• Time in Patent Office: 1,062 Days
• Field of Search: 342/26
• 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 is an airborne radar system which scans the flight path of an aircraft with two radar scans, an upper elevation pointing above local level and a lower elevation scan pointing below the glide slope. The radar returns from the upper elevation scan are used to detect the core of the microburst. The core and a model of the windshear which uses the core are used to select angles and range cell candidates, in a lower elevation scan, for hazard detection processing. The candidates in the lower scan, which is pointing at the ground, are used to create a hazard map tested against a predetermined hazard threshold. A threshold violation results in a pilot alert. The hazard map includes a vertical factor determined through model coefficients in the radial outflow as a function of altitude. The invention applies the model to determine the total hazard factor along the glideslope using the vertical hazard of the model and altitude scaling of the horizontal hazard from the lower bar elevation to the glideslope of the aircraft. The present invention also includes a radar scan with two pulse repetition frequencies which allows the elimination of non-correlated returns. The system also includes post detection integration with a sliding azimuth window to enhance the signal to noise ratio. The system also combines velocities within a single range gate to produce a velocity representing the windspeed at that range.

Claims

1. A method of detecting hazardous windshear, comprising:

(a) scanning the atmosphere in an upper radar scan;

(b) determining first hazard candidates in the upper scan;

(c) scanning the atmosphere in a lower radar scan;

(d) determining second hazard candidates in the downward scan responsive to the first hazard candidates; and

(e) characterizing the total hazard responsive to the second hazard candidates.

2. A method as recited in claim 1, wherein the total hazard is scaled to an aircraft glideslope.

3. A method as recited in claim 1, further comprising performing, prior to step (d), constant false alarm rate processing on the lower scan using a non-rectangular window oriented with respect to loci of hazardous windshear.

4. A method as recited in claim 3, where in the constant false alarm rate processing comprises ordering Doppler cells within the window to select a maximum of medians in the Doppler order.

5. A method as recited in claim 3, further comprising, prior to the constant false alarm rate processing, performing post detection integration using a sliding azimuth window.

6. A method as recited in claim 1, wherein step (e) includes determining a microburst profile from a radial outflow determined from the upper scan.

7. A method as recited in claim 1, wherein step (e) includes determining a microburst profile from an upper radial outflow determined by the upper scan and a lower radial outflow determined from the lower scan.

8. A method as recited in claim 1, further comprising performing the upper scan at two pulse repetition frequencies and combining correlated velocity returns on a range gate basis.

9. A method as recited in claim 1, further comprising performing the lower scan at two pulse repetition frequencies and combining correlated returns on a range gate basis.

10. A method as recited in claim 1, wherein step (b) comprises identifying a candidate when a number of adjacent range cells in an azimuthal direction with a wind amplitude above a minimum exceeds a predetermined number.

11. A method as recited in claim 10, further comprising using a maximum tall wind and a maximum head wind in the candidate identify radar ranges to define a diameter of the candidate and radial outflow.

12. A method as recited in claim 10, further comprising using a maximum tall wind and a maximum head wind in the candidate identify radar ranges to define an ellipsoidal, asymmetric candidate.

13. A method recited in claim 1, wherein step (b) includes determining drift and said method further includes adjusting the total hazard response to drift.

14. A method of hazardous windshear detection, comprising:

(a) scanning the atmosphere in an upper radar scan;

(b) scanning the atmosphere in a lower radar scan; and

(c) determining a downdraft core size from the upper and lower scans.

15. An airborne method of detecting hazardous windshear from an aircraft, comprising:

(a) scanning the atmosphere in an upper radar scan at approximately five degrees above local level of the aircraft using two pulse repetition frequencies and receiving upper radar returns;

(b) performing post detection integration of the upper returns using a sliding azimuth window;

(c) performing ordered constant false alarm rate processing on the upper returns using a nonrectangular window oriented with respect to loci of hazardous windshear;

(d) combining correlated upper returns on a range gate basis;

(e) scanning the atmosphere in a lower radar scan approximately down a glideslope of the aircraft using the two repetition frequencies and receiving lower radar returns;

(f) performing steps (b)-(d) on the lower returns;

(g) determining a centroid, an upper diameter and an upper radial outflow of a hazard candidate from the upper returns;

(h) selecting a portion of the lower returns for processing responsive to the hazard candidate;

(i) determining a lower diameter and a lower radial outflow of the candidate from the portion;

(j) vertically profiling the candidate;

(k) determining a total hazard;

(l) scaling the total hazard to the glideslope; and

(m) comparing the scaled total hazard to a threshold and warning the pilot when the threshold is exceeded.

16. An airborne method of detecting hazardous windshear, comprising:

(a) scanning the atmosphere in a radar scan and receiving radar returns;

(b) performing post detection integration of the radar returns using an azimuth sliding window; and

integrated returns.

17. An airborne method of detecting hazardous windshear, comprising:

(a) scanning the atmosphere in a radar scan and receiving radar returns;

(b) performing constant false alarm rate processing on the returns; and

(c) detecting windshear from the processed returns.

18. An airborne method of detecting hazardous windshear, comprising:

(a) scanning the atmosphere in upper and lower radar scans;

(b) profiling the windshear from the upper and lower radar scans using a linear relationship between radial outflow and altitude;

(c) determining the hazard from the profile.