Antenna adjustment system and method for an aircraft weather radar system

• US 7,307,583 B1
• Filed: 06/16/2005
• Issued: 12/11/2007
• Est. Priority Date: 06/09/2005
• 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: Koenigs, Gregory J., Dickerson, Charles J., Woodell, Daniel L.
• Primary Examiner(s): Sotomayor, John B
• Application Number:
  US11/153,972
• Time in Patent Office: 908 Days
• Field of Search: 342/26.R, 342/26.A, 342/26.B, 342/26.C, 342/26.D, 342 74- 77, 342/81, 342/173, 342/174
• US Class Current: 342/173
• CPC Class Codes: G01S 13/953 mounted on aircraft
• CPC Class Codes: G01S 7/4026 Antenna boresight
• CPC Class Codes: G01S 7/403 in azimuth, i.e. in the horizontal plane
• CPC Class Codes: G01S 7/4034 in elevation, i.e. in the vertical plane
• CPC Class Codes: G01S 7/4091 during normal radar operation
• 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

A weather radar system or method can be utilized to adjust a position of a weather radar system. The weather radar system can utilize processing electronics coupled to an antenna control system. The processing electronics can determine an error associated with the position of the weather radar antenna and adjust the position of the weather radar antenna in response to data related to returns received by the weather radar antenna and data related to expected returns.

Claims

1. A weather radar system, comprising:

a weather radar antenna;

an antenna control system for adjusting a position of the weather radar antenna; and

processing electronics, coupled to the antenna control system, for determining an error factor or an adjustment factor in response to data related to returns received by the weather radar antenna and data related to expected returns, the processing electronics causing the antenna control system to adjust the position of the weather radar antenna in response to the error factor or the adjustment factor.

2. The weather radar system of claim 1, wherein the processing electronics determines an error representing at least one of a pitch error, an elevation error, and a roll error.

3. The weather radar system of claim 1, wherein the data related to returns is representative of a range derived from a ratio of an upper and lower radar beam.

4. The weather radar display system of claim 1, wherein the data related to expected returns utilizes data from a local terrain data base.

5. The weather radar display system of claim 4, wherein the data related to expected returns utilizes an Earth model.

6. A weather radar system, comprising:

a weather radar antenna;

an antenna control system for adjusting a position of the weather radar antenna;

processing electronics, coupled to the antenna control system, for determining an error associated with the position of the weather radar antenna, wherein the processing electronics determines an error factor or an adjustment factor in response to data related to returns received by the weather radar antenna and data related to expected returns and stores the error factor or adjustment factor, the processing electronics causing the antenna control system to adjust the position of the weather radar antenna in response to the error factor or adjustment factor.

7. The weather radar display of claim 6, wherein the error factor or the adjustment factor is averaged.

8. The weather radar display of claim 7, wherein the error factor or adjustment factor is not averaged when the error factor or adjustment factor is not qualified via a qualification process.

9. The weather radar display system of claim 8, wherein the qualification process utilizes a vector field of overlapping zones, wherein a predetermined number of zones is used to qualify the error factor or adjustment factor.

10. A method of determining an error factor associated with an antenna of an aircraft radar system, the method comprising:

receiving radar returns;

determining a first factor related to the radar returns;

determining a second factor related to a modeled return estimation without using the radar returns associated with the first factor; and

determining the error factor using the first factor and the second factor.

11. The method of claim 10, further comprising adjusting a pitch, roll, or elevation of the antenna in response to the error factor.

12. The method of claim 11, wherein the error factor is determined periodically during a flight of the aircraft.

13. The method of claim 12, further comprising:

adjusting a pitch, roll, or elevation of the antenna in response to a stored factor related to at least one previously determined error factor.

14. The method of claim 11, further comprising:

displaying indicia of the error factor.

15. The method of claim 11, wherein the error factor is determined at least every minute.

16. An apparatus for determining an adjustment to correct at least one position error associated with an antenna of an aircraft radar system, the apparatus comprising:

means for determining a first factor related to a first range from the weather radar returns;

means for determining a second factor related to a second range using altitude information; and

means for determining the adjustment using the first factor and the second factor.

17. The apparatus of claim 16, wherein the means for determining the first factor, the means for determining the second factor, and the means for determining the adjustment are implemented using software.

18. The apparatus of claim 17, wherein the first factor and second factor are calculated using dB values.

19. The apparatus of claim 18, wherein the first factor and the second factor are delta dB values representing an angle to the surface of the Earth.

20. The apparatus of claim 19, wherein the error factor is qualified before being used to determine the adjustment.