Selecting antenna patterns on unmanned aerial vehicles
Described herein are unmanned aerial vehicles (UAVs) and systems and methods for dynamically selecting directional antennas onboard the UAV for wireless transmissions. For example, an embodiment pertains to a UAV that comprises a flight control system in remote communication with a remote receiver via directional antennas onboard the UAV. The flight control system is operatively coupled with a propulsion system to control the flight of the UAV. While in-flight, the flight control system is configured to determine an orientation and position of the UAV. It is further configured to select a subset of directional antennas to transmit from based on the determined orientation and position, among other factors. The flight control system then directs a transmitter to send wireless communications using the selected directional antennas.
1. An unmanned aerial vehicle comprising:
a flight control system configured to communicate with a remote receiver via directional antennas on the unmanned aerial vehicle;
a propulsion system operatively coupled with the flight control system and configured to propel the unmanned aerial vehicle as directed by the flight control system;
wherein the flight control system is configured to at least:
determine an orientation and position of the unmanned aerial vehicle;
select a subset of the directional antennas to transmit a signal to the remote receiver based on factors comprising the determined orientation and position; and
direct a transmitter to transmit the signal using the subset of the directional antennas, wherein to direct the transmitter to transmit the signal using the subset of the directional antennas, the flight control system is configured to direct the transmitter to distribute power to the subset of the directional antennas such that a cumulative gain of the subset of the directional antennas does not exceed a threshold.
2. The unmanned aerial vehicle of claim 1 wherein, to select the subset of the directional antennas based on the factors, the flight control system is configured to determine which one of the directional antennas has a direction that comprises a best fit with a line of sight to the remote receiver.
3. The unmanned aerial vehicle of claim 2 wherein the flight control system is further configured to calculate the line of sight to the remote receiver based at least on the position of the unmanned aerial vehicle and a position of the remote receiver.
4. The unmanned aerial vehicle of claim 3 wherein the flight control system is further configured to determine, for each of the directional antennas, the direction of a given antenna based at least on the orientation of the unmanned aerial vehicle.
5. The unmanned aerial vehicle of claim 4 , wherein the threshold corresponds to an effective isotropic radiated power threshold associated with a regulatory standard.
6. The unmanned aerial vehicle of claim 5 wherein the directional antennas consist of two groups of antennas that each contain a separate half of the directional antennas, and wherein the separate half of the directional antennas consists of at least three directional antennas.
7. The unmanned aerial vehicle of claim 6 wherein the subset of the directional antennas comprises one or more antennas of only one of the two groups of antennas.
8. A method of operating an unmanned aerial vehicle, comprising:
determining an orientation and position of the unmanned aerial vehicle;
selecting a subset of directional antennas on the unmanned aerial vehicle to transmit a signal to a remote receiver based on factors comprising the determined orientation and position of the unmanned aerial vehicle; and
transmitting the signal using the subset of directional antennas, wherein transmitting the signal using the subset of directional antennas comprises distributing power to the subset of the directional antennas such that a cumulative gain of the subset of the directional antennas does not exceed a threshold.
9. The method of claim 8 wherein, selecting the subset of the directional antennas based on the factors further comprises determining which one of the directional antennas has a direction that comprises a best fit with a line of sight to the remote receiver.
10. The method of claim 9 , further comprising calculating the line of sight to the remote receiver based at least on the position of the unmanned aerial vehicle and a position of the remote receiver.
11. The method of claim 10 , further comprising determining, for each of the directional antennas, the direction of a given antenna based at least on the orientation of the unmanned aerial vehicle.
12. The method of claim 11 , wherein the threshold corresponds to an effective isotropic radiated power threshold associated with a regulatory standard.
13. The method of claim 12 wherein the directional antennas consist of two groups of antennas that each contain a separate half of the directional antennas, and wherein the separate half of the directional antennas consists of at least three directional antennas.
14. The method of claim 13 wherein the subset of the directional antennas comprises one or more antennas of only one of the two groups of antennas.
15. A computing apparatus, comprising:
one or more computer-readable storage media; and
program instructions stored on the one or more computer-readable storage media that, based on being read and executed by a processing system, direct an unmanned aerial vehicle to at least:
determine an orientation and position of the unmanned aerial vehicle;
select a subset of directional antennas on the unmanned aerial vehicle to transmit a signal to a remote receiver based on factors comprising the determined orientation and position; and
transmit the signal using the subset of the directional antennas, wherein to transmit the signal, the program instructions direct the unmanned aerial vehicle to distribute power to the subset of the directional antennas such that a cumulative gain of the subset of the directional antennas does not exceed a threshold.
16. The computing apparatus of claim 15 wherein, to select the subset of the directional antennas based on the factors, the program instructions further direct the unmanned aerial vehicle to determine which one of the directional antennas has a direction that comprises a best fit with a line of sight to the remote receiver.
17. The computing apparatus of claim 16 wherein the program instructions further direct the unmanned aerial vehicle to calculate the line of sight to the remote receiver based at least on the position of the unmanned aerial vehicle and a position of the remote receiver.
18. The computing apparatus of claim 17 wherein the program instructions further direct the unmanned aerial vehicle to determine, for each of the directional antennas, the direction of a given antenna based at least on the orientation of the unmanned aerial vehicle.
19. The computing apparatus of claim 18 , wherein the threshold corresponds to an effective isotropic radiated power threshold associated with a regulatory standard.
20. The computing apparatus of claim 19 wherein the directional antennas consist of two groups of antennas that each contain a separate half of the directional antennas, wherein the separate half of the directional antennas consists of at least three directional antennas, and wherein the subset of the directional antennas comprises one or more antennas of only one of the two groups of antennas.