Laser scanning for spatial acquisition of a satellite receiver
A laser beam transmission system comprises a laser beam system and a controller that controls the laser beam system. The controller is configured to direct a laser beam at a location nearest to a maximum of an uncertainty area in which a satellite is expected to be located. The controller is configured to move the laser beam from the location to a next location nearest to the maximum of the uncertainty area in response to not receiving a confirmation that the satellite is at the location. The next location becomes a current location for the laser beam. The controller is configured to continue to move the laser beam from the current location to the next location nearest to the maximum of the uncertainty area from the current location in response to not receiving the confirmation that the satellite has received the laser beam.
1 . A laser beam transmission system that comprises:
a laser beam system configured to transmit a laser beam; and
a controller configured to control the laser beam system to:
direct the laser beam at a location nearest to a maximum of an uncertainty area in which a satellite is expected to be located;
move the laser beam from the location to a next location nearest to the maximum of the uncertainty area in response to not receiving a confirmation that the satellite is at the location, wherein the next location becomes a current location for the laser beam; and
continue to move the laser beam from the current location to the next location nearest to the maximum of the uncertainty area from the current location with a dwell time at each location in response to not receiving the confirmation that the satellite has received the laser beam.
2 . The laser beam transmission system of claim 1 , wherein a movement of the laser beam is in a form of a nearest to maximum hexagonal scan.
3 . The laser beam transmission system of claim 1 , wherein the controller is further configured to direct a hybrid scan.
4 . The laser beam transmission system of claim 1 , wherein in continuing to move the laser beam, the controller is configured to:
continue to move the laser beam from the current location to the next location nearest to the maximum of the uncertainty area from the current location with a continuous movement from one location to another location in response to not receiving the confirmation that the satellite has received the laser beam.
5 . The laser beam transmission system of claim 1 , wherein the controller is configured to control the laser beam system to:
move the laser beam to a neighbor location of a nearest neighbor in response to a time for moving the laser beam from the current location to the next location using the location nearest to the maximum of the uncertainty area being greater than a threshold, wherein the next location becomes the current location; and
continue to move the laser beam from the current location to a subsequent neighbor location of the nearest neighbor from the current location in response to the time for moving the laser beam from the current location to the next location using the location nearest to the maximum of the uncertainty area being greater than the threshold and in response to not receiving the confirmation that the satellite has received the laser beam.
6 . The laser beam transmission system of claim 5 , wherein in moving the laser beam to the neighbor location of the nearest neighbor and continuing to move the laser beam from the current location to the subsequent neighbor location of the nearest neighbor from the current location is part of a nearest neighbor scan selected from one of a continuous spiral scan, a step spiral scan, a segmented scan, and a raster scan.
7 . The laser beam transmission system of claim 1 , wherein the controller is configured to:
establish communications with the satellite in response to receiving the confirmation.
8 . The laser beam transmission system of claim 7 , wherein the communications are selected from one of unidirectional communications and bidirectional communications.
9 . The laser beam transmission system of claim 1 , wherein the laser beam is selected from a group comprising a continuous laser beam and a pulsed laser beam.
10 . An electromagnetic beam transmission system that comprises:
an electromagnetic beam system configured to transmit an electromagnetic beam; and
a controller configured to control the electromagnetic beam transmission system to:
direct the electromagnetic beam at a location nearest to a maximum of an uncertainty area in which an object is expected to be located;
move the electromagnetic beam from the location to a next location nearest to the maximum of the uncertainty area in response to not receiving a confirmation that the object is at the location, wherein the next location becomes a current location for the electromagnetic beam;
continue to move the electromagnetic beam from the current location to the next location nearest to the maximum of the uncertainty area from the current location with a dwell time at each location in response to not receiving the confirmation that a satellite has received the laser beam; and
continue to move the electromagnetic beam from the current location to the next location nearest to the maximum of the uncertainty area from the current location in response to not receiving the confirmation that the electromagnetic beam has encountered the object.
11 . The electromagnetic beam transmission system of claim 10 , wherein the object is selected from a group comprising an uncooperative object, a mobile platform, a stationary platform, a land-based structure, an aquatic-based structure, a space-based structure, an aircraft, a commercial aircraft, a rotorcraft, a tilt-rotor aircraft, a tilt wing aircraft, a vertical takeoff and landing aircraft, an electrical vertical takeoff and landing vehicle, a personal air vehicle, a surface ship, a tank, a personnel carrier, a train, a spacecraft, a space station, a satellite, a submarine, an automobile, a power plant, a bridge, a dam, a house, a manufacturing facility, a building, and an electromagnetic beam receiver.
12 . An electromagnetic beam transmission system that comprises:
an electromagnetic beam system configured to transmit an electromagnetic beam; and
a controller configured to control the electromagnetic beam transmission system to:
direct the electromagnetic beam to a location in an uncertainty area using a scan metric, wherein the uncertainty area is one in which an object is expected to be located;
move the electromagnetic beam from the location to a next location using the scan metric in response to not receiving a confirmation that the object is at the location, wherein;
the controller selects the next location in the uncertainty area from a set of candidate locations that has a highest value for the scan metric, wherein the scan metric is as follows: M=PDF int /t tot where PDF int is a probability density function integrated over an area of interest for a next potential location and t tot is a total time t tot =t slew +t dwell , t slew is a time to slew a line-of-sight from a current location to the next potential location, and td well is a time the line of site dwells at the next potential location; and
the next location becomes a current location for the electromagnetic beam; and
continue to move the electromagnetic beam from the current location to the next location using the scan metric in response to not receiving the confirmation that the electromagnetic beam has encountered the object.
13 . The electromagnetic beam transmission system of claim 12 , wherein the controller is further configured to direct a hybrid scan.
14 . A method for pointing a laser beam, the method comprising:
directing the laser beam at a location nearest to a maximum of an uncertainty area in which a satellite is expected to be located;
moving the laser beam from the location to a next location nearest to the maximum of the uncertainty area in response to not receiving a confirmation that the satellite is at the location, wherein the next location becomes a current location for the laser beam; and
continuing to move the laser beam from the current location to the next location nearest to the maximum of the uncertainty area from the current location with a dwell time at each location in response to not receiving the confirmation that the satellite has received the laser beam.
15 . The method of claim 14 , wherein a movement of the laser beam is in a form of a nearest to maximum hexagonal scan.
16 . The method of claim 14 , wherein a controller is configured to direct a hybrid scan.
17 . The method of claim 14 , wherein continuing to move the laser beam comprises:
continuing to move the laser beam from the current location to the next location nearest to the maximum of the uncertainty area from the current location with a continuous movement from one location to another location in response to not receiving the confirmation that the satellite has received the laser beam.
18 . The method of claim 14 further comprising:
moving the laser beam to a neighbor location of a nearest neighbor in response to a time for moving the laser beam from the current location to the next location using the location nearest to the maximum of the uncertainty area being greater than a threshold, wherein the next location becomes the current location; and
continuing to move the laser beam from the current location to a subsequent neighbor location of the nearest neighbor from the current location in response to the time for moving the laser beam from the current location to the next location using the location nearest to the maximum of the uncertainty area being greater than the threshold and in response to not receiving the confirmation that the satellite has received the laser beam.
19 . The method of claim 18 , wherein moving the laser beam to the neighbor location of the nearest neighbor and continuing to move the laser beam from the current location to the subsequent neighbor location of the nearest neighbor from the current location is part of a nearest neighbor scan selected from one of a continuous spiral scan, a step spiral scan, a segmented scan, and a raster scan.
20 . The method of claim 14 further comprising:
establishing communications with the satellite in response to receiving the confirmation.
21 . The method of claim 20 , wherein the communications are selected from one of unidirectional communications and bidirectional communications.
22 . The method of claim 14 , wherein the laser beam is selected is selected from a group comprising a continuous laser beam and a pulsed laser beam.
23 . A method for pointing an electromagnetic beam, the method comprising:
directing the electromagnetic beam at a location nearest to a maximum of an uncertainty area in which an object is expected to be located;
moving the electromagnetic beam from the location to a next location nearest to the maximum of the uncertainty area in response to not receiving a confirmation that the object is at the location, wherein the next location becomes a current location for the electromagnetic beam;
continue to move the electromagnetic beam from the current location to the next location nearest to the maximum of the uncertainty area from the current location with a dwell time at each location in response to not receiving the confirmation that a satellite has received the laser beam; and
continuing to move the electromagnetic beam from the current location to the next location nearest to the maximum of the uncertainty area from the current location in response to not receiving the confirmation that the electromagnetic beam has encountered the object.