Tactical engagement simulation (TES) ground-based air defense platform
An aerial vehicle is described that is capable of interacting within a TES environment, and capable of acting as a Ground Based Air Defense (GBAD) platform to represent virtually any type of aircraft in the simulation. The aerial vehicle may include sensors for determining its own location and/or orientation, and may further carry a payload of components that can be assembled modularly to equipped the aerial vehicle with different types of functionality. Such functionality can include enabling the aerial vehicle to gather information regarding its surroundings, engage with other military entities within the TES environment, and/or enable other military entities within the TES environment to engage with it.
1. An aerial vehicle for use in a Tactical Engagement Simulation (TES) environment, the aerial vehicle comprising:
a body configured to lift a payload; and
a communications unit comprising:
a Global Navigation Satellite System (GNSS) receiver,
an inertial measurement unit (IMU), and
a wireless communication interface;
wherein the communications unit is configured to
obtain data from one or more components of the payload, and
wirelessly send simulation information, via the wireless communication interface, to a computer server communicatively coupled with the TES environment, wherein:
the simulation information includes engagement information comprising:
an indication of a simulated engagement by the aerial vehicle with an entity within the TES environment,
an indication of a simulated engagement by an entity within the TES environment with the aerial vehicle, or
both; and
the simulation information is based on:
the data received from the one or more components of the payload,
the data from the GNSS receiver, and
the data from the IMU.
2. The aerial vehicle of claim 1 , wherein the one or more components of the payload comprise:
a laser detector,
a laser transmitter,
a thermal signature unit,
an engagement indicator unit,
a radar reflector,
a camera, or
any combination thereof.
3. The aerial vehicle of claim 2 , wherein the one or more components of the payload comprise the camera, and the communications unit is further configured to include, in the simulation information, a video stream.
4. The aerial vehicle of claim 2 , wherein the one or more components of the payload comprise the laser detector.
5. The aerial vehicle of claim 2 , wherein the one or more components of the payload comprise the laser transmitter.
6. The aerial vehicle of claim 1 , wherein the one or more components of the payload are configured to be modularly engaged with the payload.
7. The aerial vehicle of claim 1 , wherein the communications unit is further configured to receive the data from the one or more components of the payload via the wireless communication interface.
8. The aerial vehicle of claim 1 , wherein the wireless communication interface is configured to send the simulation information via cellular radio frequency (RF) technology.
9. A method of operating an aerial vehicle within a Tactical Engagement Simulation (TES) environment, the method comprising:
obtaining, at the aerial vehicle, data from a GNSS receiver of the aerial vehicle;
obtaining, at the aerial vehicle, data from an inertial measurement unit (IMU) of the aerial vehicle;
obtaining, at the aerial vehicle, data from one or more components of a payload carried by the aerial vehicle; and
wirelessly sending simulation information, via a wireless communication interface of the aerial vehicle, to a computer server communicatively coupled with the TES environment, wherein:
the simulation information includes engagement information comprising:
an indication of a simulated engagement by the aerial vehicle with an entity within the TES environment,
an indication of a simulated engagement by an entity within the TES environment with the aerial vehicle, or
both; and
the simulation information is based on:
the data from the one or more components of the payload,
the data from the GNSS receiver, and
the data from the IMU.
10. The method of claim 9 , wherein the one or more components of the payload comprise:
a laser detector,
a laser transmitter,
a thermal signature unit,
an engagement indicator unit,
a radar reflector,
a camera, or
any combination thereof.
11. The method of claim 10 , wherein the one or more components of the payload comprise the camera, and wherein the method further comprises including, in the simulation information, a video stream.
12. The method of claim 10 , wherein the one or more components of the payload comprise the laser detector.
13. The method of claim 10 , wherein the one or more components of the payload comprise the laser transmitter.
14. The method of claim 9 , wherein the one or more components of the payload are configured to be modularly engaged with the payload.
15. The method of claim 9 , wherein obtaining the data from the one or more components of the payload comprises receiving the data from the one or more components of the payload via the wireless communication interface.
16. The method of claim 9 , wherein the wireless communication interface is configured to send the simulation information via cellular radio frequency (RF) technology.
17. A non-transitory computer-readable medium having instructions embedded thereon for operating an aerial vehicle within a Tactical Engagement Simulation (TES) environment, wherein the instructions, when executed by one or more processing units of the aerial vehicle, cause the one or more processing units to:
obtain, at the aerial vehicle, data from a GNSS receiver of the aerial vehicle;
obtain, at the aerial vehicle, data from an inertial measurement unit (IMU) of the aerial vehicle;
obtain, at the aerial vehicle, data from one or more components of a payload carried by the aerial vehicle; and
wirelessly send simulation information, via a wireless communication interface of the aerial vehicle, to a computer server communicatively coupled with the TES environment, wherein:
the simulation information includes engagement information comprising:
an indication of a simulated engagement by the aerial vehicle with an entity within the TES environment,
an indication of a simulated engagement by an entity within the TES environment with the aerial vehicle, or
both; and
the simulation information is based on:
the data from the one or more components of the payload,
the data from the GNSS receiver, and
the data from the IMU.
18. The non-transitory computer-readable medium of claim 17 , wherein the instructions for causing the one or more processing units to obtain the data from one or more components of the payload carried by the aerial vehicle further comprise instructions for causing the one or more processing units to obtain data from:
a laser detector,
a laser transmitter,
a thermal signature unit,
an engagement indicator unit,
a radar reflector,
a camera, or
any combination thereof.
19. The non-transitory computer-readable of claim 18 , wherein the instructions, when executed by the one or more processing units, further cause the one or more processing units to include, in the simulation information, a video stream.
20. The non-transitory computer-readable of claim 18 , wherein the instructions, when executed by the one or more processing units.