Abstract: An unmanned aerial vehicle (UAV) controller may have control elements configured to receive inputs from a user. A cover may be coupled to the controller. The cover may be movable between a closed position in which the control elements are covered and an open position in which the control elements are exposed. An antenna may be integrated in the cover. The antenna may be electrically connected to circuitry in the controller for communicating with a UAV. In some implementations, a conductive plane and/or an insulating plane may be integrated in the cover. In some implementations, a heatsink, a fan, and/or a support mechanism may be arranged on an under portion of the controller. In some implementations, a circuit board including a cutout may be arranged inside the controller.

Abstract: A method includes: establishing wireless connection between an unmanned aerial vehicle (UAV) and a user interface; generating, via the user interface, a flight path for the unmanned aerial vehicle; generating, via the user interface, a flight schedule for the unmanned aerial vehicle, the flight schedule being associated with the flight path and include one or more designated times; and initiating, via the user interface, autonomous operation of the unmanned aerial vehicle for the unmanned aerial vehicle to autonomously fly the flight path at the one or more designated times

Abstract: A dock assembly includes a docking station and a stand or mount coupled to the docking station. The dock assembly may be configured for an unmanned aerial vehicle (UAV). The docking station may include a landing surface configured to interface with the UAV, an extended portion coupled to the landing surface and extending from the landing surface, and a fiducial located on the extended portion.

Abstract: A battery configured to power an unmanned aerial vehicle. The battery includes an enclosure configured to house a power module of the battery. The battery also includes one or more conducting contacts located on the enclosure configured to contact one or more pogo pins of a battery charger located on a docking station of the unmanned aerial vehicle.

Abstract: A method of using a base station to charge an unmanned aerial vehicle (UAV) is disclosed. The method includes: docking the UAV with a cradle of the base station; retracting the cradle into an enclosure of the base station via a slide mechanism; and electrically connecting a power source of the UAV to a charging hub connected to the slide mechanism to thereby charge the power source.

Abstract: A base station for an unmanned aerial vehicle (UAV) is disclosed. The base station includes: an enclosure; a slide mechanism that is connected to the enclosure and which is repositionable between a retracted position and an extended position; a cradle that is connected to the slide mechanism and which is configured for docking with the UAV such that the UAV is movable into and out of the enclosure during repositioning of the slide mechanism between the retracted position and the extended position; and a charging hub that is connected to the slide mechanism and which is configured for electrical connection to a power source of the UAV to charge the power source.

Abstract: A base station is disclosed for an unmanned aerial vehicle (UAV). The base station includes: a metallic enclosure; a first electronics module; a second electronics module; and a third electronics module, wherein the first electronics module, the second electronics module, and the third electronics module are each configured for individual removal from the metallic enclosure. The metallic enclosure is configured to receive the UAV and includes a front end having a front door and a rear end having a rear door. The rear door is located adjacent to the first electronics module and includes a metallic panel that is positioned in correspondence with the first electronics module so as to create a Faraday cage for the first electronics module and thereby reduce electromagnetic emissions from the base station.

Abstract: A base station is disclosed for use with an unmanned aerial vehicle (UAV). The base station includes: an enclosure; a cradle that is configured to charge a power source of the UAV during docking with the base station; and a temperature control system that is connected to the cradle and which is configured to vary temperature of the power source of the UAV. The temperature control system includes: a thermoelectric conditioner (TEC); a first air circuit that is thermally connected to the TEC and which is configured to regulate temperature of the TEC; and a second air circuit that is thermally connected to the TEC such that the TEC is located between the first air circuit and the second air circuit. The second air circuit is configured to direct air across the cradle to thereby heat or cool the power source of the UAV when docked with the base station.

Abstract: A base station is disclosed that is configured for use with a UAV. The base station includes: an enclosure with an outer housing that defines a roof section and an inner housing that is connected to the outer housing; one or more heating elements that are supported by the enclosure and which are configured to heat the roof section; one or more fiducials that are supported by the enclosure; an illumination system that is supported by the enclosure and which is configured to illuminate the one or more fiducials; and a visualization system that is supported by the enclosure.

Abstract: An unmanned aerial vehicle (UAV) is disclosed that includes a power source. The power source includes: one or more power cells; one or more thermal transfer members that are thermally connected to the one or more power cells; and a heat exchanger that is thermally connected to the one or more thermal transfer members such that the one or more thermal transfer members and the heat exchanger facilitate a transfer of thermal energy between the power source and ambient air to decrease or increase temperature of the power source.

Abstract: An unmanned aerial vehicle (UAV) controller may have control elements configured to receive inputs from a user. A cover may be coupled to the controller. The cover may be movable between a closed position in which the control elements are covered and an open position in which the control elements are exposed. An antenna may be integrated in the cover. The antenna may be electrically connected to circuitry in the controller for communicating with a UAV. In some implementations, a conductive plane and/or an insulating plane may be integrated in the cover. In some implementations, a heatsink, a fan, and/or a support mechanism may be arranged on an under portion of the controller. In some implementations, a circuit board including a cutout may be arranged inside the controller.

Abstract: The technology described herein relates to autonomous aerial vehicle technology and, more specifically, to environment illumination for autonomous unmanned aerial vehicles. In some embodiments, a UAV includes upward-facing image capture devices, downward-facing image capture devices, one or more illumination sources, and a computer system. The computer system is configured to direct the one or more illumination sources to selectively emit light into a surrounding physical environment while the UAV is in flight, process images captured by any one or more of the plurality of upward-facing image capture devices or the plurality of downward-facing image capture devices to estimate a position and/or orientation of the aerial vehicle, generate a planned trajectory for the aerial vehicle through a physical environment based on the processing of the images, and control a propulsion system and/or flight surface of the aerial vehicle to cause the aerial vehicle to autonomously maneuver along the planned trajectory.