Abstract: Various arrangements for charging an unmanned aerial vehicle (UAV) may be presented. When flying in the vicinity of the UAV docking station, the UAV may identify the UAV docking station based on image recognition of an alignment graphic on a docking platform of the UAV docking station. The UAV may then determine a landing rotational orientation based on the image recognition. The UAV may rotate to the landing rotational orientation. The UAV may land on the docking platform of the UAV docking station in the landing rotational orientation such that electrical contacts of the UAV electrically connect with electrical contacts of the UAV docking station.

Abstract: A solar powered satellite system is provided. A power control system, for example, of the solar powered satellite system may include, but is not limited to, a first interface configured to receive a power signal from the satellite receiver, a voltage converter electrically coupled to the first interface, the voltage converter configured to reduce a voltage of the power signal received from the satellite receiver to a predetermined voltage, a second interface configured to receive a power signal from the solar panel assembly, a third interface configured to be coupled to at least one power consumer of a satellite antenna system, and a source selection circuit electrically coupled to the voltage converter, the solar panel assembly and the third interface, the source selection circuit configured to output a selected power signal based upon a comparison between the predetermined voltage and a voltage of the power signal from the solar panel assembly.

Abstract: A solar powered satellite system is provided. A power control system, for example, of the solar powered satellite system may include, but is not limited to, a first interface configured to receive a power signal from the satellite receiver, a voltage converter electrically coupled to the first interface, the voltage converter configured to reduce a voltage of the power signal received from the satellite receiver to a predetermined voltage, a second interface configured to receive a power signal from the solar panel assembly, a third interface configured to be coupled to at least one power consumer of a satellite antenna system, and a source selection circuit electrically coupled to the voltage converter, the solar panel assembly and the third interface, the source selection circuit configured to output a selected power signal based upon a comparison between the predetermined voltage and a voltage of the power signal from the solar panel assembly.