IP Library Granted Patent US 11,578,952
Granted Patent B2
US 11,578,952 · App. 17/503,499 · Granted Feb 14, 2023

Directional high-energy radio frequency weapon

Inventor: George G. Fortney (Reston, VA)
Assignee: Science Applications International Corporation
F41H13/0075
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Quick Facts
Patent No.
US 11,578,952
App. No.
17/503,499
Granted
Feb 14, 2023
Kind
B2
Abstract

Systems, methods and apparatus are described for a HERF weapon that may emit high-energy radio waves at a target based on locational information and a frequency associated with the target. The HERF weapon may receive the frequency and locational information from a sensing system. The HERF weapon may emit a high energy pulse toward the target and on the frequency associated with the target to disable or destroy the target without affecting nearby devices. The HERF weapon may allow the user to avoid detection by using a frequency that corresponds to the target's operating frequency.

Claims (67)

1. A method for directing high-intensity beams toward an unmanned aerial vehicle (UAV), the method comprising:

receiving a location of the UAV and a radio frequency (RF) associated with the UAV;

orienting, based on the location, a directional antenna toward the UAV;

adjusting, based on the location, an aperture of the directional antenna; and

emitting, via the directional antenna, an RF signal comprising a frequency based on the RF associated with the UAV, wherein:

the RF signal comprises RF energy at a power configured, along a beam axis of the directional antenna at a range between 1 kilometer and 1.5 kilometers from the directional antenna, to disable the UAV, wherein the RF energy drops off outside a field of view of the directional antenna; and

the frequency is over a spectrum bandwidth of detected transmissions from the UAV; and

determining whether the UAV was disabled by the emitted RF signal.

2. The method of claim 1 , further comprising:

creating, after emitting the RF signal, a log entry comprising an identification of the UAV and a record of the emitted RF signal.

3. The method of claim 1 , wherein the orienting the directional antenna comprises sending control signals to cause movement of a mounting system of the directional antenna.

4. The method of claim 1 , wherein the field of view of the directional antenna is approximately 20 degrees.

5. The method of claim 1 , wherein the directional antenna comprises at least one of a parabolic antenna, a helical antenna, a yagi antenna, a log-periodic antenna, a horn antenna, or a phased array antenna.

6. The method of claim 1 , wherein the spectrum bandwidth is within +/−1% of the radio frequency associated with the UAV.

7. The method of claim 1 , further comprising:

determining, based on the location of the UAV, that a range to the UAV satisfies a threshold, and wherein the emitting the RF signal comprises emitting, based on the determining that the range satisfies the threshold, the RF signal.

8. The method of claim 1 , further comprising:

receiving, after the emitting, an indication that the UAV is still operating; and

emitting, based on the indication that the UAV is still operating, a second RF signal comprising RF energy at a power configured, along the beam axis of the directional antenna at a range between 1 kilometer and 1.5 kilometers from the directional antenna, to disable the UAV.

9. The method of claim 1 , further comprising:

receiving a second location of the UAV relative to a sensing system; and

determining the location by converting the second location relative to the directional antenna, wherein the sensing system and the directional antenna are not co-located.

10. The method of claim 1 , further comprising adjusting a power of the RF signal based on at least one of: a range to the UAV or a perceived threat associated with the UAV.

11. The method of claim 1 , further comprising:

detecting a swarm of UAVs;

orienting, based on the detecting the swarm of UAVs, the directional antenna toward the swarm of UAVs;

adjusting the aperture of the directional antenna to encompass the swarm of UAVs; and

emitting, via the directional antenna, a second RF signal toward the swarm of UAVs.

12. The method of claim 1 , wherein the RF energy comprises at least 30 decibel-milliwatts (dBm) along the beam axis of the directional antenna.

13. A system for directing high-intensity beams toward an unmanned aerial vehicle (UAV), the system comprising:

a directional antenna;

a radio frequency (RF) signal generator and amplifier configured to cause emission, via the directional antenna, of RF signals; and

a control unit comprising one or more processors and memory storing instructions that, when executed by the one or more processors, cause the system to:

receive a location of the UAV and a radio frequency (RF) associated with the UAV;

orient, based on the location, the directional antenna toward the UAV;

adjust, based on the location, an aperture of the directional antenna;

emit, via the directional antenna, an RF signal comprising a frequency based on the RF associated with the UAV, wherein:

the RF signal comprises RF energy at a power configured, along a beam axis of the directional antenna at a range between 1 kilometer and 1.5 kilometers from the directional antenna, to disable the UAV, wherein the RF energy drops off outside a field of view of the directional antenna; and

the frequency is over a spectrum bandwidth of detected transmissions from the UAV; and

determine whether the UAV was disabled by the emitted RF signal.

14. The system of claim 13 , wherein the spectrum bandwidth is within +/−1% of the radio frequency associated with the UAV.

15. The system of claim 13 , wherein the instructions, when executed by the one or more processors, cause the system to:

determine, based on the location of the UAV, that a range to the UAV satisfies a threshold; and

emit, based on the determining that the range satisfies the threshold, the RF signal.

16. The system of claim 13 , wherein the instructions, when executed by the one or more processors, cause the system to:

receive, after the emitting, an indication that the UAV is still operating; and

emit, based on the indication that the UAV is still operating, a second RF signal comprising RF energy at a power configured, along the beam axis of the directional antenna at a range between 1 kilometer and 1.5 kilometers from the directional antenna, to disable the UAV.

17. The system of claim 13 , wherein the instructions, when executed by the one or more processors, cause the system to adjust a power of the RF signal based on at least one of: a range to the UAV or a perceived threat associated with the UAV.

18. The system of claim 13 , wherein the instructions, when executed by the one or more processors, cause the system to:

detect a swarm of UAVs;

orient, based on the detecting the swarm of UAVs, the directional antenna toward the swarm of UAVs;

adjust the aperture of the directional antenna to encompass the swarm of UAVs; and

emit, via the directional antenna, a second RF signal toward the swarm of UAVs.

19. The system of claim 13 , wherein the RF energy comprises at least 30 decibel-milliwatts (dBm) along the beam axis of the directional antenna.

20. A non-transitory computer-readable medium comprising instructions that, when executed, cause a system for directing high-intensity beams toward an unmanned aerial vehicle (UAV) to:

receive a location of the UAV and a radio frequency (RF) associated with the UAV;

orient, based on the location, a directional antenna toward the UAV;

adjust, based on the location, an aperture of the directional antenna;

emit, via the directional antenna, an RF signal comprising a frequency based on the RF associated with the UAV, wherein:

the RF signal comprises RF energy at a power configured, along a beam axis of the directional antenna at a range between 1 kilometer and 1.5 kilometers from the directional antenna, to disable the UAV, wherein the RF energy drops off outside a field of view of the directional antenna; and

the frequency is over a spectrum bandwidth of detected transmissions from the UAV; and

determine whether the UAV was disabled by the emitted RF signal.

21. The non-transitory computer-readable medium of claim 20 , wherein the spectrum bandwidth is within +/−1% of the radio frequency associated with the UAV.

22. The non-transitory computer-readable medium of claim 20 , wherein the instructions, when executed, cause the system for directing high-intensity beams toward an UAV to:

receive, after the emitting, an indication that the UAV is still operating; and

emit, based on the indication that the UAV is still operating, a second RF signal comprising RF energy at a power configured, along the beam axis of the directional antenna at a range between 1 kilometer and 1.5 kilometers from the directional antenna, to disable the UAV.

23. The non-transitory computer-readable medium of claim 20 , wherein the RF energy comprises at least 30 decibel-milliwatts (dBm) along the beam axis of the directional antenna.

Assignments (2)
SECURITY INTEREST Recorded Dec 10, 2025
From: SCIENCE APPLICATIONS INTERNATIONAL CORPORATION
To: CITIBANK, N.A., AS COLLATERAL AGENT
Reel/Frame 073170/0273 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 18, 2021
From: FORTNEY, GEORGE G.
To: SCIENCE APPLICATIONS INTERNATIONAL CORPORATION
Reel/Frame 057816/0490 →
Continuity (2)
Continuation 17024283 · Sep 17, 2020
Related Publication 20220082358A1 · Mar 17, 2022
Cited By (2)
US 12,264,900 US 12,624,923