Lightweight laser designator systems and methods
Laser designator systems (laser designator systems) and related techniques are provided to improve the operational flexibility of unmanned aerial vehicles (UAVs). A laser designator system includes an imaging module configured to image a scene according to a first field of view (FOV) of the imaging module; a laser spot tracker configured to detect a plurality of PRF encoded laser spots disposed within the scene and to provide a corresponding plurality of angular positions of the plurality of PRF encoded laser spots within a second FOV of the laser spot tracker; and an optical datum faceplate coupled to and configured to optically align the imaging module and the laser spot tracker to each other and a boresight for the laser designator system defined by the optical datum faceplate.
1 . A laser designator system for an unmanned aerial vehicle (UAV), the laser designator system comprising:
an imaging module configured to image a scene according to a first field of view (FOV) of the imaging module;
a laser target marker configured to generate and project a pulse repetition frequency (PRF) encoded laser beam towards the scene and within the first FOV of the imaging module;
a laser spot tracker configured to detect a PRF encoded laser spot generated by the PRF encoded laser beam within the scene and provide an angular position of the PRF encoded laser spot within a second FOV of the laser spot tracker; and
an optical datum faceplate coupled to and configured to optically align the imaging module, the laser target marker, and the laser spot tracker to each other and to a boresight for the laser designator system defined by the optical datum faceplate.
2 . The laser designator system of claim 1 , further comprising:
a logic device configured to communicate with the imaging module, the laser target marker, and/or the laser spot tracker, wherein the logic device is configured to:
disable the laser spot tracker;
control the laser target marker to initiate the PRF encoded laser beam;
receive a series of laser pulse trigger signals corresponding to each pulse of the PRF encoded laser beam;
determine at least one laser pulse repetition period between adjacent pulses of the PRF encoded laser beam based, at least in part, on the received series of laser pulse trigger signals;
determine at least one predicted laser pulse emission time based, at least in part, on the determined at least one pulse repetition period; and
enable the laser spot tracker at least one hundred light-meters after the predicted laser pulse emission time, a light-meter being an amount of time it takes for light to travel a distance of one meter in vacuum.
3 . The laser designator system of claim 2 , wherein the determining the at least one predicted laser pulse emission time comprises:
determining the at least one predicted laser pulse emission time based, at least in part, on the determined at least one laser pulse repetition period and a PRF encoding of the PRF encoded laser beam.
4 . The laser designator system of claim 1 , further comprising:
a laser rangefinder coupled to the optical datum faceplate and configured to provide laser rangefinder data corresponding to the PRF encoded laser spot detected by the laser spot tracker; and
a logic device configured to communicate with the imaging module, the laser target marker, the laser spot tracker, and/or the laser rangefinder, wherein the logic device is configured to:
convert the angular position of the PRF encoded laser spot into a pixel position within image data generated by the imaging module; and
determine a geolocation of the PRF encoded laser spot based, at least in part, on the laser rangefinder data provided by the laser rangefinder and/or the pixel position within the image data generated by the imaging module.
5 . The laser designator system of claim 4 , further comprising an orientation and/or position sensor (OPS) configured to provide an orientation and/or position associated with the laser designator system, wherein the logic device is configured to:
determine a geolocation of the PRF encoded laser spot based, at least in part, on the laser rangefinder data provided by the laser rangefinder, the pixel position within the image data generated by the imaging module, and/or the orientation and/or position associated with the laser designator system provided by the OPS.
6 . The laser designator system of claim 1 , wherein the imaging module comprises a first infrared imaging module and the first FOV comprises a relatively wide FOV, the system further comprising:
a second infrared imaging module configured to image the scene according to a relatively narrow FOV disposed entirely within the relatively wide FOV of the first infrared imaging module, wherein the second infrared imaging module is coupled to the optical datum faceplate and optically aligned to the boresight of the laser designator system by the optical datum faceplate.
7 . An unmanned aircraft system (UAS) comprising the laser designator system of claim 1 , the UAS further comprising:
the UAV, wherein the laser designator system is coupled to the UAV via an actuated gimbal system; and
a base station associated with the UAV, wherein the base station is configured to:
receive image data generated by the imaging module of the laser designator system and the angular position of the PRF encoded laser spot;
convert the angular position of the PRF encoded laser spot into a pixel position within the image data generated by the imaging module;
determine a geolocation of the PRF encoded laser spot based, at least in part, on the pixel position within the image data generated by the imaging module and/or an orientation and/or position of the UAV; and
render a display view comprising the image data generated by the imaging module and at least one graphical element configured to indicate the geolocation of the PRF encoded laser spot within the scene.
8 . A method of operating the laser designator system of claim 1 , the method comprising:
disabling the laser spot tracker;
controlling the laser target marker to initiate the PRF encoded laser beam;
receiving a series of laser pulse trigger signals corresponding to each pulse of the PRF encoded laser beam;
determining at least one laser pulse repetition period between adjacent pulses of the PRF encoded laser beam based, at least in part, on the received series of laser pulse trigger signals;
determining at least one predicted laser pulse emission time based, at least in part, on the determined at least one pulse repetition period; and
enabling the laser spot tracker after the predicted laser pulse emission time.
9 . The method of claim 8 , wherein the enabling the laser spot tracker occurs at least one hundred light-meters after the predicted laser pulse emission time, a light-meter being an amount of time it takes for light to travel a distance of one meter in vacuum.
10 . The method of claim 9 , wherein the determining the at least one predicted laser pulse emission time is based, at least in part, on the determined at least one laser pulse repetition period and a PRF encoding of the PRF encoded laser beam.
11 . The method of claim 8 , further comprising:
providing laser rangefinder date corresponding to the PRF encoded laser spot detected by the laser spot tracker, and
converting the angular position of the PRF encoded laser spot into a pixel position within image data generated by the imaging module; and
determining a geolocation of the PRF encoded laser spot based, at least in part, on the laser rangefinder data provided by the laser rangefinder and/or the pixel position within the image data generated by the imaging module.
12 . A laser designator system for an unmanned aerial vehicle (UAV), the laser designator system comprising:
an imaging module configured to image a scene according to a first field of view (FOV) of the imaging module;
a laser spot tracker configured to detect a plurality of pulse repetition frequency (PRF) encoded laser spots disposed within the scene and to provide a corresponding plurality of angular positions of the plurality of PRF encoded laser spots within a second FOV of the laser spot tracker; and
an optical datum faceplate coupled to and configured to optically align the imaging module and the laser spot tracker to each other and a boresight for the laser designator system defined by the optical datum faceplate.
13 . The laser designator system of claim 12 , further comprising:
an orientation and/or position sensor (OPS) configured to provide an orientation and/or position associated with the laser designator system; and
a logic device configured to communicate with the imaging module, the laser spot tracker, and/or the OPS, wherein the logic device is configured to:
convert the plurality of angular positions corresponding to the plurality of PRF encoded laser spots into a corresponding plurality of pixel positions within image data generated by the imaging module; and
determine a plurality of geolocations corresponding to the plurality of PRF encoded laser spots based, at least in part, on the orientation and/or position associated with the laser designator system provided by the OPS and/or the plurality of pixel positions within the image data generated by the imaging module.
14 . The laser designator system of claim 13 , further comprising a laser rangefinder coupled to the optical datum faceplate and configured to provide laser rangefinder data corresponding to at least one of the plurality of PRF encoded laser spots detected by the laser spot tracker, wherein the logic device is configured to:
determine the plurality of geolocations corresponding to the plurality of PRF encoded laser spots based, at least in part, on the laser rangefinder data provided by the laser rangefinder, the plurality of pixel positions within the image data generated by the imaging module, and/or the orientation and/or position associated with the laser designator system provided by the OPS.
15 . A method comprising:
controlling a laser target marker to initiate a pulse repetition frequency (PRF) encoded laser beam;
receiving a series of laser pulse trigger signals corresponding to each pulse of the PRF encoded laser beam;
determining at least one laser pulse repetition period between adjacent pulses of the PRF encoded laser beam based, at least in part, on the received series of laser pulse trigger signals;
determining at least one predicted laser pulse emission time based, at least in part, on the determined at least one laser pulse repetition period;
disabling a laser spot tracker from detecting the PRF encoded laser beam during at least one hundred light-meters after the predicted laser pulse emission time, a light-meter being an amount of time it takes for light to travel a distance of one meter in vacuum; and
enabling the laser spot tracker at least one hundred light-meters after the predicted laser pulse emission time to detect reflections of the PRF encoded laser beam.
16 . The method of claim 15 , wherein the determining the at least one predicted laser pulse emission time is based, at least in part, on the determining at least one laser pulse repetition period and a PRF encoding of the PRF encoded laser beam.
17 . The method of claim 16 , further comprising:
detecting a PRF encoded laser spot generated by the PRF encoded laser beam;
providing laser rangefinder data corresponding to the PRF encoded laser spot;
converting an angular position of the PRF encoded laser spot into a pixel position within image data; and
determining a geolocation of the PRF encoded laser spot based, at least in part, on the laser rangefinder data and/or the pixel position within the image data generated by the imaging module.
18 . An unmanned aircraft system (UAS) configured to perform the method of claim 15 , the UAS further comprising:
an imaging module configured to image a scene according to a first field of view (FOV) of the imaging module;
the laser target marker configured to generate and project the PRF encoded laser beam towards the scene and within the first FOV of the imaging module;
a laser spot tracker configured to detect a PRF encoded laser spot generated by the PRF encoded laser beam within the scene and provide an angular position of the PRF encoded laser spot within a second FOV of the laser spot tracker; and
an optical datum faceplate coupled to and configured to optically align the imaging module, the laser target marker, and the laser spot tracker to each other and to a boresight for the laser designator system defined by the optical datum faceplate.
19 . The method of claim 15 , comprising:
disabling the laser spot tracker from detecting the laser beam during at least two hundred light-meters after the predicted laser pulse emission time; and
enabling the laser spot tracker at least two hundred light-meters after the predicted laser pulse emission time to detect reflections of the PRF encoded laser beam.
20 . The method of claim 15 , comprising:
disabling the laser spot tracker from detecting the laser beam during at least three hundred light-meters after the predicted laser pulse emission time; and
enabling the laser spot tracker at least three hundred light-meters after the predicted laser pulse emission time to detect reflections of the PRF encoded laser beam.