System and method for disrupting radio frequency communications of aircraft

1. A system for disrupting Radio Frequency communication of a plurality of unmanned aircraft, the system comprising:

a directional antenna;

a transmitter to generate a signal waveform for emission by the directional antenna, the signal waveform configured to disrupt Radio Frequency communication of an unmanned aircraft;

a drive system connected to the directional antenna and configured to move the directional antenna about an axis; and

a control system operatively connected to the transmitter and the drive system;

wherein the control system is configured to:

cause the transmitter to generate the signal waveform; and

cause the drive system to rotate the directional antenna about the axis continuously in a same rotational direction such that electromagnetic radiation emitted by the directional antenna irradiates each of the plurality of unmanned aircraft intermittently, wherein each of the plurality of unmanned aircraft is irradiated for a first period of time and not irradiated for a second period of time, and wherein the second period of time is less than or equal to 5 seconds.

2. The system of claim 1 wherein the electromagnetic radiation emitted comprises a GNSS frequency.

3. The system of claim 1 , wherein the electromagnetic radiation emitted comprises an ISM frequency and the second period of time is less than or equal to 0.5 seconds.

4. The system of claim 1 , wherein the drive system is configured to rotate the directional antenna about the axis at a speed of at least 1 rad/s.

5. The system of claim 1 , further comprising:

a detection system configured to detect unmanned aircraft;

wherein the control system is configured to cause the drive system to move a beam emitted by the directional antenna over an area including at least two unmanned aircraft detected by the detection system.

6. The system of claim 5 , wherein control system is configured to vary the speed at which the drive system moves the directional antenna in dependence on detected unmanned aircraft within a beam of electromagnetic radiation emitted by the directional antenna.

7. The system of claim 6 , wherein the control system is configured to cause the drive system to decrease the speed at which the directional antenna moves when an unmanned aircraft is detected within the beam of electromagnetic radiation emitted by the directional antenna.

8. The system of claim 6 , wherein the control system is configured to cause the drive system to increase the speed at which the directional antenna moves when no unmanned aircraft is detected within the beam of electromagnetic radiation emitted by the directional antenna.

9. The system of claim 1 , further comprising:

a tracking system operatively connected to the drive system and the control system, the tracking system for tracking an unmanned aircraft detected by the a detection system;

wherein the control system is configured to:

cause the tracking system to track a single unmanned aircraft, responsive to a single unmanned aircraft being detected by the detection system; and

cause the drive system to move a beam of electromagnetic radiation emitted by the directional antenna across an area including at least two unmanned aircraft, responsive to two or more unmanned aircraft being detected by the detection system.

10. A method of disrupting a radio frequency communication system of one or more unmanned aircraft using a same source of electromagnetic radiation, the method comprising:

irradiating each of the one or more unmanned aircraft with a burst of electromagnetic radiation using the same source of electromagnetic radiation; and

repeating the irradiating each of the one or more unmanned aircraft with a burst of electromagnetic radiation by rotating the source of electromagnetic radiation about an axis continuously in a same rotational direction such that all of the one or more unmanned aircraft are irradiated at least once every 5 seconds.

11. The method of claim 10 , wherein the burst of electromagnetic radiation comprises a GNSS frequency.

12. The method of claim 10 , wherein the burst of electromagnetic radiation comprises an ISM frequency, and the irradiating is repeated such that all of the one or more unmanned aircraft are irradiated at least once every 0.5 seconds.

13. The method of claim 10 , wherein the irradiating and repeating are responsive to detection of one or more unmanned aircraft.

14. A non-transitory computer-readable medium comprising computer-readable instructions for execution by a processor of a system for disrupting radio frequency communication of unmanned aircraft, the system comprising: a directional antenna; a transmitter to generate a signal waveform for emission by the directional antenna; and a drive system connected to the directional antenna and configured to move the directional antenna;

wherein the computing readable instructions, when executed by the processor, cause the processor to:

cause the transmitter to generate the signal waveform, the signal waveform configured to disrupt Radio Frequency communication of an unmanned aircraft; and

cause the drive system to rotate the directional antenna about an axis continuously in a same rotational direction such that electromagnetic radiation emitted by the directional antenna irradiates each of a plurality of unmanned aircraft intermittently, wherein each of the plurality of unmanned aircraft is irradiated for a first period of time and not irradiated for a second period of time, and wherein the second period of time is less than or equal to 5 seconds.

15. The non-transitory computer-readable medium of claim 14 , wherein the computer-readable instructions, when executed by the processor, cause the processor to:

cause the transmitter to generate the signal waveform comprising an ISM frequency; and

cause the drive system to move the directional antenna such that the second period of time is less than or equal to 0.5 seconds.

16. The non-transitory computer-readable medium of claim 14 , wherein the computer-readable instructions, when executed by the processor, cause the processor to:

cause the drive system to vary the speed at which the directional antenna moves in dependence on detected unmanned aircraft within a beam of electromagnetic radiation emitted by the directional antenna.

17. The non-transitory computer-readable medium of claim 16 , wherein the computer-readable instructions, when executed by the processor, cause the processor to:

cause the drive system to move the directional antenna at a first speed when an unmanned aircraft is detected within the beam of electromagnetic radiation emitted by the directional antenna; and

cause the drive system to move the directional antenna at a second speed when no unmanned aircraft is detected within the beam of electromagnetic radiation emitted by the directional antenna, wherein the second speed is faster than the first speed.