Systems and methods for providing UAV-based digital escort drones in visitor management and access control systems are provided. A visitor management and access control system can identify a need for escorting a visitor through the region and transmit a signal to a drone that identifies a starting location and a destination location in the region. Responsive to receiving the signal, the drone can escort the visitor along a path from the starting location to the destination location, and an access privilege device carried by the drone can open a secured door or access a secured area along the path.

This disclosure is generally directed to an Unmanned Aerial Device (UAV) that uses a removable computing device for command and control. The UAV may include an airframe with rotors and an adjustable cradle to attach a computing device. The computing device, such as a smart phone, tablet, MP3 player, or the like, may provide the necessary avionics and computing equipment to control the UAV autonomously. For example, the adjustable cradle may be extended to fit a tablet or other large computing device, or retracted to fit a smart phone or other small computing device. Thus, the adjustable cradle may provide for the attachment and use of a plurality of different computing devices in conjunction with a single airframe. Additionally the UAV may comprise adjustable arms to assist in balancing the load of the different computing devices and/or additional equipment attached to the airframe.

A landing platform for an unmanned aerial vehicle, including a plurality of substantially funnel-shaped centering housings configured to cooperate with a corresponding plurality of projections of the aerial vehicle for reaching a predetermined landing position. The platform can include a mechanism for recharging the battery of the aerial vehicle and/or with an arrangement for serial data transfer.

This disclosure describes an aerial vehicle, such as an unmanned aerial vehicle (“UAV”), which includes a plurality of maneuverability propulsion mechanisms that enable the aerial vehicle to move in any of the six degrees of freedom (surge, sway, heave, pitch, yaw, and roll). The aerial vehicle may also include a lifting propulsion mechanism that operates to generate a force sufficient to maintain the aerial vehicle at an altitude.

This disclosure describes an aerial vehicle, such as an unmanned aerial vehicle (“UAV”), which includes a plurality of maneuverability propulsion mechanisms that enable the aerial vehicle to move in any of the six degrees of freedom (surge, sway, heave, pitch, yaw, and roll). The aerial vehicle may also include a lifting propulsion mechanism that operates to generate a force sufficient to maintain the aerial vehicle at an altitude.

Method and system to ascertain location of drone box for landing and charging drones comprising at least a drone box having a drone platform with a plurality of limiting boundaries, divided into number of sensor zones that are mechanically contiguous and electrically separated by an insulated separator of insulation width, each sensor zone having an identification coordinates, each drone having a plurality of ground interfaces, each having a unique address code, each ground interface has a charging terminal at a far end, each charging terminal having an interlocked switchable electricity polarity. The identification coordinates of the activated sensor zones are communicable to a second drone so that the second drone knows where NOT to land on the drone box, Such communication enables a third and subsequent drone to ascertain whether the identified drone box is suitable and available for landing.

An access management system includes a mobile device with a processor and a memory and a software platform including at least a processor and a memory. The software platform is configured to analyze data obtained from the mobile device and other devices connected to the software platform. Specifically, the software platform is operable to determine if an access key received, read, or captured by a mobile device matches an access key for an authorized account, object, device, or space for the mobile device, and to provide access to the mobile device if the access key received, read, or captured by the mobile device matches the authorized access key.

A system with a safety feature for charging an electric aircraft. The system includes an electric aircraft port of an electric aircraft, a sensor on the electric aircraft, and a computing device communicatively connected to the electric aircraft port and the sensor. The electric aircraft port is configured to mate with a charging connector. The sensor is configured to detect a sensor datum of the charging connector. The computing device is configured to receive the sensor datum, generate a charging instruction set as a function of the sensor datum, transmit the charging instruction set to the electric aircraft port, and enable charging of the electric aircraft, by the charging connector and through the electric aircraft port, as a function of the charging instruction set. The charging instruction set includes a safety lock instruction. A method with a safety feature for charging an electric aircraft is also provided.

A system and method for managing residual energy in a charging component is disclosed herein. Managing residual energy includes detecting an electrical parameter of the charging component and the electrically connected battery pack and generating a residual datum. The residual datum is transmitted to a computing device. The computing device identifies a residual element, generates an alert datum, and executes a security measure.

A system for regulating charging of an electric aircraft includes a charging connector and a controller communicatively connected to the charging connector. The charging connector includes a housing, at least a conductor, and at least a control signal conductor. The housing is configured to mate with an electric aircraft port of an electric aircraft. The at least a conductor is configured to conduct a current. The at least a control signal conductor is configured to conduct a control signal. The controller is configured to receive a voltage datum from the electric aircraft, and regulate a charging voltage, as a function of the voltage datum, to the electric aircraft. Regulation of the charging voltage includes charging at least a battery of the electric aircraft in a plurality of phases including a first charging phase at a constant current and a second charging phase at a constant voltage.