Optimized two panel AESA for aircraft applications

1. A radar system for an aircraft, the radar system comprising:

a pair of Active Electronically Scanned Array (AESA) panels disposed in a nosecone radome of the aircraft, the pair of AESA panels respectively positioned on two opposing lateral sides of a longitudinal axis of the aircraft, wherein a pointing direction of the first AESA panel is offset by a predetermined angle in a clockwise direction with respect to the longitudinal axis of the aircraft and a pointing direction of the second AESA panel is offset by the predetermined angle in a counterclockwise direction with respect to the longitudinal axis of the aircraft;

a controller in communication with each of the pair of AESA panels, the controller configured for selectively switching between:

the first AESA panel individually for providing a first coverage area in a first direction offset from the longitudinal axis of the aircraft,

the second AESA panel individually for providing a second coverage area in a second direction offset from the longitudinal axis of the aircraft, and

the pair of AESA panels jointly for providing a third coverage area between the first coverage area and the second coverage area.

2. The radar system of claim 1 , wherein the predetermined angle ranges between 30° and 60°.

3. The radar system of claim 1 , wherein the controller is configured for activating the pair of AESA panels jointly for providing a coverage area within plus/minus the predetermined angle along the longitudinal axis of the aircraft.

4. The radar system of claim 3 , wherein the predetermined angle is 35°, and the controller is configured for selectively activating at least one of:

the first AESA panel individually for providing a coverage area between −45° and −60° away from the longitudinal axis of the aircraft;

the second AESA panel individually for providing a coverage area between 45° and 60° away from the longitudinal axis of the aircraft; and

the pair of AESA panels jointly for providing a coverage area within ±45° along the longitudinal axis of the aircraft.

5. The radar system of claim 3 , wherein the predetermined angle is 45°, and the controller is configured for selectively activating at least one of:

the first AESA panel individually for providing a coverage area between −45° and −90° away from the longitudinal axis of the aircraft;

the second AESA panel individually for providing a coverage area between 45° and 90° away from the longitudinal axis of the aircraft; and

the pair of AESA panels jointly for providing a coverage area within ±45° along the longitudinal axis of the aircraft.

6. The radar system of claim 1 , wherein the controller is further configured for activating both the first and the second AESA panels, wherein the first and the second AESA panels operate simultaneously and independently for providing the first and the second converge areas, respectively, and wherein transmitter pulses of the first and the second AESA panels are synchronized to mitigate potential interferences between the first and the second AESA panels.

7. The radar system of claim 1 , wherein the AESA panels are implemented utilizing low off-axis loss radiating elements.

8. A radar system, comprising:

a pair of Active Electronically Scanned Array (AESA) panels, the pair of AESA panels respectively positioned on two opposing sides of a central axis, wherein a pointing direction of the first AESA panel is offset by a predetermined angle in a clockwise direction with respect to the central axis and a pointing direction of the second AESA panel is offset by the predetermined angle in a counterclockwise direction with respect to the central axis;

a controller in communication with each of the pair of AESA panels, the controller configured for selectively switching between:

the first AESA panel individually for providing a first coverage area in a first direction offset from the central axis,

the second AESA panel individually for providing a second coverage area in a second direction offset from the central axis, and

the pair of AESA panels jointly for providing a third coverage area between the first coverage area and the second coverage area.

9. The radar system of claim 8 , wherein the predetermined angle ranges between 30° and 60°.

10. The radar system of claim 8 , wherein the controller is configured for activating the pair of AESA panels jointly for providing a coverage area within plus/minus the predetermined angle along the central axis.

11. The radar system of claim 10 , wherein the predetermined angle is 35°, and the controller is configured for selectively activating at least one of:

the first AESA panel individually for providing a coverage area between −45° and −60° away from the central axis;

the second AESA panel individually for providing a coverage area between 45° and 60° away from the central axis; and

the pair of AESA panels jointly for providing a coverage area within ±45° along the central axis.

12. The radar system of claim 10 , wherein the predetermined angle is 45°, and the controller is configured for selectively activating at least one of:

the first AESA panel individually for providing a coverage area between −45° and −90° away from the central axis;

the second AESA panel individually for providing a coverage area between 45° and 90° away from the central axis; and

the pair of AESA panels jointly for providing a coverage area within ±45° along the central axis.

13. The radar system of claim 8 , wherein the controller is further configured for activating both the first and the second AESA panels, wherein the first and the second AESA panels operate simultaneously and independently for providing the first and the second converge areas, respectively, and wherein transmitter pulses of the first and the second AESA panels are synchronized to mitigate potential interferences between the first and the second AESA panels.

14. The radar system of claim 8 , wherein the AESA panels are implemented utilizing low off-axis loss radiating elements.

15. A method for providing wide azimuth coverage utilizing Active Electronically Scanned Array (AESA) radars, the method comprising:

providing a first AESA panel on a first side of a central axis, wherein a pointing direction of the first AESA panel is offset by a predetermined angle in a clockwise direction with respect to the central axis;

providing a second AESA panel on a second side of the central axis, wherein a pointing direction of the second AESA panel is offset by the predetermined angle in a counterclockwise direction with respect to the central axis; and

switching between:

the first AESA panel for providing a first coverage area in a first direction offset from the central axis,

the second AESA panel for providing a second coverage area in a second direction offset from the central axis, and

the first AESA panel and the second AESA panel jointly for providing a third coverage area between the first coverage area and the second coverage area.

16. The method of claim 15 , wherein the predetermined angle ranges between 30° and 60°.

17. The method of claim 15 , wherein the first AESA panel and the second AESA panel are activated jointly for providing a coverage area within plus/minus the predetermined angle along the central axis.

18. The method of claim 17 , wherein the predetermined angle is 35°, and the method further comprises:

activating the first AESA panel individually for providing a coverage area between −45° and −60° away from the central axis;

activating the second AESA panel individually for providing a coverage area between 45° and 60° away from the central axis; and

activating the first AESA panel and the second AESA panel jointly for providing a coverage area within ±45° along the central axis.

19. The method of claim 17 , wherein the predetermined angle is 45°, and the method further comprises:

activating the first AESA panel individually for providing a coverage area between −45° and −90° away from the central axis;

activating the second AESA panel individually for providing a coverage area between 45° and 90° away from the central axis; and

activating the first AESA panel and the second AESA panel jointly for providing a coverage area within ±45° along the central axis.

20. The method of claim 15 , wherein the switching step further includes: activating both first AESA panel and the second AESA panel, wherein the first and the second AESA panels operate simultaneously and independently for providing the first and the second converge areas, respectively, and wherein transmitter pulses of the first and the second AESA panels are synchronized to mitigate potential interferences between the first and the second AESA panels.