Weather radar detection of objects

1. A radar system, configured to mount on an ownship vehicle, and for interleaving a weather detection mode and a noncooperative unmanned aerial vehicle (UAV) detection mode, the radar system comprising:

an airborne-capable phased-array radar device configured to:

receive weather signals in the weather detection mode,

receive sensing signals in the noncooperative UAV detection mode by at least:

receiving at least one upper elevation beam at a first angle higher than a slope of the ownship vehicle; and

receiving at least one lower elevation beam at a second angle lower than the slope of the ownship vehicle,

interleave the weather detection mode and the noncooperative UAV detection mode at an interleaving rate, the interleaving rate being greater than once per two seconds, and

complete a full cycle through the weather detection mode and the noncooperative UAV detection mode in less than two seconds; and

processing circuitry configured to:

determine weather conditions based on the received weather signals, and

detect a noncooperative UAV based on the received sensing signals, wherein the noncooperative UAV is nonresponsive, and wherein the noncooperative UAV is outside of the system.

2. The radar system of claim 1 ,

wherein the weather detection mode is configured to, while operating in the weather detection mode, operate in a windshear mode that is a sub mode of the weather detection mode, and

wherein the airborne-capable phased-array radar device is further configured to interleave the noncooperative UAV detection mode with the windshear mode.

3. The radar system of claim 1 , wherein the airborne-capable phased-array radar device is configured to transmit and receive the sensing signals at altitudes of less than two thousand feet above a ground surface for aircraft on final approach.

4. The radar system of claim 1 , further comprising a memory device configured to store expected characteristics of UAVs, wherein the processing circuitry is configured to detect noncooperative UAVs based on the received sensing signals by at least comparing actual characteristics of the received sensing signals to the expected characteristics of UAVs.

5. The radar system of claim 1 , wherein the processing circuitry is configured to determine a UAV detection range of the at least one lower elevation beam based on an altitude of the ownship vehicle or a distance from the ownship vehicle to a runway.

6. The radar system of claim 1 ,

wherein the airborne-capable phased-array radar device is configured to transmit a first beam, and

wherein the processing circuitry is configured to steer a plurality of receive beams within an area illuminated by the first beam by applying a phase shift to the received sensing signals.

7. The radar system of claim 1 , wherein the processing circuitry is further configured to determine a size, speed, and direction of travel of the noncooperative UAV based on the received sensing signals.

8. The radar system of claim 1 ,

wherein the first angle is higher than the slope of a direction of travel of the ownship vehicle, and

wherein the second angle is lower than the slope of a direction of travel of the ownship vehicle.

9. A method for interleaving a weather detection mode and a noncooperative unmanned aerial vehicle (UAV) detection mode, the method comprising:

receiving, by an airborne-capable phased-array radar device, weather signals in the weather detection mode;

receiving, by the airborne-capable phased-array radar device, sensing signals in the noncooperative UAV detection mode by at least:

receiving at least one upper elevation beam at a first angle higher than a slope of the ownship vehicle; and

receiving at least one lower elevation beam at a second angle lower than the slope of the ownship vehicle;

interleaving the weather detection mode and the noncooperative UAV detection mode at an interleaving rate, the interleaving rate being greater than once per two seconds;

completing a full cycle through the weather detection mode and the noncooperative UAV detection mode in less than two seconds;

determining, by processing circuitry, weather conditions based on the received weather signals; and

detecting, by the processing circuitry, a noncooperative UAV based on the received sensing signals, wherein the noncooperative UAV is nonresponsive, and wherein the noncooperative UAV is outside of the system.

10. The method of claim 9 ,

wherein the weather detection mode comprises a windshear mode that is a sub mode of the weather detection mode, and

wherein interleaving the weather detection mode and the noncooperative UAV detection mode comprises interleaving the noncooperative UAV detection with the windshear mode.

11. The method of claim 9 , further comprising transmitting, by the airborne-capable phased-array radar device, the sensing signals in the noncooperative UAV detection mode at altitudes of less than two thousand feet above a ground surface,

wherein receiving the sensing signals in the noncooperative UAV detection mode comprises receiving the sensing signals at altitudes of less than two thousand feet above a ground surface for aircraft on final approach.

12. The method of claim 9 , further comprising storing expected characteristics of UAVs, wherein detecting noncooperative UAVs based on the received sensing signals by at least comparing actual characteristics of the received sensing signals to the expected characteristics of UAVs.

13. The method of claim 9 , further comprising:

transmitting a first beam; and

steering a plurality of receive beams within an area illuminated by the first beam by applying a phase shift to the received sensing signals.

14. The method of claim 9 , further comprising determining a size, speed, and direction of travel of the noncooperative UAV based on the received sensing signals.

15. The method of claim 9 , further comprising determining a UAV detection range of the at least one lower elevation beam based on an altitude of the ownship vehicle or a distance from the ownship vehicle to a runway.

16. A device comprising a computer-readable medium having executable instructions stored thereon, configured to be executable by one or more processors for causing the one or more processors to:

cause the airborne-capable phased-array radar device to transmit an azimuth beam;

receive, from an airborne-capable phased-array radar device, weather signals in the weather detection mode;

receive, from the airborne-capable phased-array radar device, sensing signals in a noncooperative unmanned aerial vehicle (UAV) detection mode by at least:

receiving at least one upper elevation beam at a first angle higher than a slope of the ownship vehicle; and

receiving at least one lower elevation beam at a second angle lower than the slope of the ownship vehicle;

interleave a weather detection mode and the noncooperative UAV detection mode at an interleaving rate, the interleaving rate being greater than once per two seconds;

complete a full cycle through the weather detection mode and the noncooperative UAV detection mode in less than two seconds;

determine weather conditions based on the received weather signals; and

detect a noncooperative UAV based on the received sensing signals, wherein the noncooperative UAV is nonresponsive, and wherein the noncooperative UAV is outside of the system.

17. The device of claim 16 ,

wherein the weather detection mode comprises a windshear mode that is a sub mode of the weather detection mode, and

wherein the executable instructions further cause the one or more processors to interleave the noncooperative UAV detection mode with the windshear mode.

18. The device of claim 16 , wherein the executable instructions further cause the one or more processors to:

store expected characteristics of UAVs; and

compare actual characteristics of the received sensing signals to the expected characteristics of UAVs.

19. The device of claim 16 , wherein the executable instructions further cause the one or more processors to steer a plurality of receive beams within an area illuminated by the azimuth first beam by applying a phase shift to the received sensing signals.

20. The device of claim 16 , wherein the executable instructions further cause the one or more processors to cause the airborne-capable phased-array radar device to transmit and receive the sensing signals at altitudes of less than two thousand feet above a ground surface for aircraft on final approach.