Method and flexible apparatus permitting advanced radar signal processing, tracking, and classification/identification design and evaluation using single unmanned air surveillance (UAS) device

Patent metadata

Field	Value
Publication number	US-11987355-B2
Application number	US-202117343175-A
Country	US
Kind code	B2
Filing date	Jun 9, 2021
Priority date	Jun 9, 2021
Publication date	May 21, 2024
Grant date	May 21, 2024

Abstract

An assembly is configured for connection to an unmanned aerial vehicle (UAV) and comprises a plurality of emulator devices each configured for attachment to the UAV and a plurality of first connection tethers each configured to operably couple a respective one of the plurality of emulator devices to the UAV at a respective spacing from the UAV. The emulator devices each comprise an emulation component configured to provide, to a target detection system, a characteristic associated with a respective type of airborne object. The plurality of respective first connection tethers each comprises material that does not substantially reflect RF energy. During flight of the UAV, when the assembly is connected, each respective emulator device maintains the respective spacing from the UAV and emulates the characteristic to the target detection system, such that the assembly emulates, to the target detection system, a plurality of airborne objects.

First claim

What is claimed is:

1. An assembly configured for connection to a single unmanned aerial vehicle (UAV), the assembly comprising:
a plurality of emulator devices each configured for attachment to a single UAV, each respective emulator device comprising a first emulation component, the first emulation component configured to provide, to a target detection system, a detectable feature that represents a first characteristic associated with a respective type of airborne object being emulated, the detectable feature comprising at least one of a scattering pattern of the airborne object and a signal return associated with one or more moving parts at or in the airborne object; and
a plurality of respective first connection tethers each configured to operably couple a respective one of the plurality of emulator devices to the single UAV at a desired respective spacing from the single UAV and configured to allow the single UAV to fly freely when the single UAV is connected to the assembly, each respective first connection tether formed such that at least a portion of each respective connection tether comprises a respective material that is configured so that it does not substantially reflect RF energy;
wherein each of the plurality of respective first connection tethers associated with the plurality of respective emulator devices, is constructed and arranged so that, after coupling the assembly to the single UAV, each of the plurality of respective emulator devices maintains the desired respective spacing from the single UAV when the single UAV is flying freely while towing the assembly and wherein at least one of the plurality of respective first connection tethers is configured to have a respective length that is dynamically adjustable, while the UAV is airborne and flying freely, so as to increase and decrease the desired respective spacing between the single UAV and a corresponding emulator device that is operably coupled to the single UAV via the at least one of the plurality of respective first connection tethers;
wherein the assembly is configured so that, when it is connected to the single UAV, the assembly does not constrain the single UAV from becoming airborne and flying freely while towing the assembly, wherein, during a flight of the single UAV that is connected to the assembly, the single UAV is not physically connected to any entities other than the assembly and wherein the assembly is not physically connected to any entities other than the single UAV; and
wherein the assembly, when connected to the single UAV, is configured so that each respective emulator device emulates the first characteristic to the target detection system, such that, during the flight of the single UAV while towing the assembly, the assembly presents, to the target detection system, a plurality of first characteristics that together emulate a grouping comprising a plurality of airborne objects that are each flying individually; and
wherein the increase and decrease of the desired respective spacing between the single UAV and the corresponding emulator device is configured to simulate a change in one or more detectable features of the grouping of airborne objects.

2. The assembly of claim 1 , wherein the airborne object comprises at least one of a drone, unmanned aerial vehicle (UAV), unmanned aerial system (UAS), unmanned aircraft (UA), remotely piloted aircraft (RPA), remotely piloted aircraft systems (RPAS), remotely piloted vehicles (RPV), balloon, airborne weapon, airborne munition, cluster of airborne reflective materials, bird, insect, and bat.

3. The assembly of claim 1 , wherein the target detection system comprises at least one of a radar system, a heat sensor, a light sensor, an infrared sensor, an optical sensor, a Lidar system, and a camera.

4. The assembly of claim 1 , wherein the first characteristic comprises at least one characteristic selected from a list of characteristics that comprises a radar cross section (RCS), a heat signature, a physical appearance, a shape, a pattern of motion, a proximity to other airborne objects, a reflectivity, a frequency pattern, a sound, an RF transmission pattern, a moving part, and a physical appearance.

5. The assembly of claim 1 , wherein the first emulation component comprises at least one of: an RF scatter source configured to simulate an RF scattering pattern associated with one or more of airborne objects; a passive RF scatterer; an RF calibration source; an RF object surrogate scatterer; a target body surrogate; a source of RF modulation; an RF reflecting element; a visual object surrogate, an RF transmission source; a heat source; and a light source.

6. The assembly of claim 1 , further comprising at least one second connection tether, the second connection tether being distinct from the first connection tether, wherein the second connection tether is configured to connect between two or more of the plurality of emulator devices, wherein the second connection tether is configured to maintain, during flight of the single UAV, an intra-emulator device spacing between at least two or more of the plurality of emulator devices.

7. The assembly of claim 4 , wherein at least a respective one of the plurality of emulator devices further comprises a second emulation component, the second emulation component configured to provide, to the target detection system, a second characteristic associated with the respective type of airborne object, wherein the second emulation component is operably coupled to first emulation component and wherein the second characteristic is selected from the list of characteristics but is different than the first characteristic provided by the first emulation component.

8. A method for simulating, for a target tracking system, a first behavior characteristic associated with one or more of a plurality of airborne objects, the method comprising:
configuring each of a plurality of respective emulator devices, in an assembly, for individual attachment to a single unmanned aerial vehicle (UAV), each respective emulator device comprising a first emulation component configured to provide, to a target detection system, a detectable feature that represents a first characteristic associated with a respective type of airborne object being emulated, the detectable feature comprising at least one of a scattering pattern of the airborne object and a signal return associated with one or more moving parts at or in the airborne object;
coupling, to each of the plurality of respective emulator devices, a plurality of respective first connection tethers, each respective first connection tether configured to operably couple a respective one of the plurality of respective emulator devices to the single UAV at a desired respective spacing from the single UAV, each respective first connection tether configured to allow the single UAV to fly freely when the single UAV is connected to the assembly, each respective first connection tether formed such that at least a portion of each respective first connection tether comprises a first material that is configured so that it does not substantially reflect RF energy;
coupling the plurality of respective emulation devices to the single UAV via the plurality of respective first connection tethers so that each of the plurality of respective emulator devices maintains at least the desired respective spacing from the single UAV when the single UAV is flying freely while towing the assembly, wherein, the assembly is configured so that, when it is coupled to the single UAV, the assembly does not constrain the single UAV from becoming airborne and flying while towing the assembly, wherein, during a flight of the single UAV when connected to the assembly, the single UAV is not physically connected to any enti

Assignees

• Raytheon Co

Inventors

• White Brian W

Classifications

• B64U30/26

  Ducted or shrouded rotors · CPC title

• B64U30/10

  Wings · CPC title

• B64U2101/31

  for surveillance · CPC title

• B64C39/024 Primary

  of the remote controlled vehicle type, i.e. RPV · CPC title

• B64D3/02

  for towing targets · CPC title