System for and method of sequential lobing using less than full aperture antenna techniques

• US 8,773,301 B1
• Filed: 05/17/2012
• Issued: 07/08/2014
• Est. Priority Date: 07/02/2008
• 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: Woodell, Daniel L.
• Primary Examiner(s): GREGORY, BERNARR E
• Application Number:
  US13/474,559
• Time in Patent Office: 782 Days
• Field of Search: 342 26 R- 26 D, 342/27, 342/28, 342 61- 65, 342 89-118, 342120-123, 342134-158, 342/175, 342192-197, 342/70, 342/350, 342/368, 342/371, 342/372, 342/385, 342/417, 342/442, 701/1, 701 3- 18, 701/300, 701/301
• US Class Current: 342/65
• CPC Class Codes: G01S 13/935 for terrain-avoidance
• CPC Class Codes: G01S 13/953 mounted on aircraft
• CPC Class Codes: G01S 3/32 derived from different combinations of signals from separate antennas, e.g. comparing sum with difference
• CPC Class Codes: G01S 3/48 the waves arriving at the antennas being continuous or intermittent and the phase difference of signals derived therefrom being measured
• 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 method of determining an angle within the beam to a target using an airborne radar includes receiving first data associated with first returns associated with a first portion of an antenna. The method further includes receiving second data associated with second returns associated with a second portion of an antenna, wherein the first portion is not identical to the second portion. The method further includes determining the angle within the beam to the target using the first and second data.

Claims

1. A method of determining an angle to a target or terrain, the method comprising:

receiving from a receive circuit first data associated with first returns received by a radar system associated with a first area of an antenna, wherein the first data includes a first phase;

receiving from the receive circuit second data associated with second returns received by the radar system associated with a second area of the antenna, wherein the first area is not identical to the second area, wherein the second data includes a second phase; and

calculating in an electronic processor the angle to the target or terrain using the first phase and second phase, wherein the angle is calculated using a difference between the first phase and the second phase associated with a difference in a distance from the first area of the antenna to the terrain or target and a distance from the second area of the antenna to the terrain or target, and wherein the angle is calculated using a Doppler component.

2. The method of claim 1, comprising:

providing third data associated with third returns associated with the first area of the antenna, wherein the Doppler component associated with at least one of the first, second, and third data is cancelled in the calculating step.

3. The method of claim 1 wherein the second returns associated with the second area are associated with a half aperture and the first returns associated with the first area are associated with a full aperture.

4. The method of claim 1, comprising:

providing a first vector to the target or terrain using the first data and a second vector to the target or terrain using the second data.

5. The method of claim 4, wherein a complex conjugate between the first vector and a second vector is used to determine the angle to the target or terrain.

6. The method of claim 1, further comprising:

providing by the radar system a first pulse before sampling the first returns; and

providing by the radar system a second pulse before sampling the second returns.

7. The method of claim 6 further comprising:

providing by the radar system a third pulse before sampling third returns; and

providing by the radar system a fourth pulse before sampling fourth returns.

8. The method of claim 7 wherein the first and third pulses are full aperture pulses.

9. The method of claim 1 further comprising:

receiving third data associated with third returns associated with the first area of the antenna;

receiving fourth data associated with fourth returns associated with the second area of the antenna; and

wherein the angle is determined using an angle within the beam.

10. The method of claim 9 wherein a focusing vector is utilized.

11. A method of determining an angle to a target or terrain, the method comprising:

providing first data associated with first returns received by a radar system associated with a first area of an antenna, the first data representing a first vector to the target or terrain;

providing second data associated with second returns received by the radar system associated with a second area of the antenna, wherein the first area is not identical to the second area, the second data representing a second vector to the target or terrain;

providing third data associated with third returns received by the radar system, the third data representing a third vector to the target or terrain;

removing a Doppler component in the second data and a Doppler component in the third data when calculating the angle to the target or terrain from the first data, the second data, and the third data.

12. The method of claim 11, wherein V1 represents the first vector, V2 represents the second vector, and V3 represents the third vector and the angle to the target or terrain is calculated using an angle within a beam related by:

arctan(VC)/2, where VC=VA times the conjugate of VB and VA=V1 times the conjugate of V2 and VB=V2 times the conjugate of V3.

13. The method of claim 11 wherein the angle to the target or terrain is calculated using conjugate operations.

14. The method of claim 11 wherein the multiple resultant vectors are calculated from successive first, second, and third vectors, the resultant vectors being coherently integrated.

15. A radar system for receiving radar returns, the radar system comprising:

an electronic processor configured to receive electronic data associated with the radar returns received by the radar system, the electronic processor receiving first electronic data associated with a first portion of an antenna and second electronic data associated with a second portion of the antenna, the first portion being within, intersecting with, or being exclusive of the second portion and being not identical to the second portion, the electronic processor calculating an angle to a target or terrain, the angle being calculated using the second electronic data and a lower portion of the first electronic data, the lower portion of the first electronic data being associated with the radar returns received in a first area in the first portion of the antenna below a second area in the first portion of the antenna, an upper portion of the first electronic data being associated with the radar returns received in the second area of the first portion of the antenna, wherein the electronic processor does not use the upper portion of the first electronic data to calculate the angle, thereby reducing weather induced errors associated with the upper portion.

16. The radar system of claim 15 wherein the processor receives third and fourth electronic data, the third electronic data associated with the first portion of the antenna and the fourth electronic data associated with the second portion of the antenna.

17. The radar system of claim 15 wherein the first electronic data is coded data.

18. The radar system of claim 15 wherein the upper portion is defined by an angle constraint, the angle constraint being defined by a power level drop or maximum power.

19. The apparatus of claim 15 wherein the angle constraint is a half beam width.

20. The apparatus of claim 15 wherein the first electronic data and the second electronic data are used to calculate a resultant vector, the resultant vector being in rectangular form and wherein the resultant vector is coherently integrated with other resultant vectors.