A package unloading and conveying system including a landing platform and one or more container aligning linear rails. The container aligning linear rails for aligning, on or above the landing platform and a hold of an aerial vehicle placed in front of one of multiple conveyor belts. One or more package extracting tools adapted to push or pull the package out of the aligned hold into a container aligned with one of the multiple conveyor belts. The multiple rail arrangements each adapted to convey the container to one of the multiple building windows from one of the multiple conveyors.

Embodiments relate generally to systems, methods, and processes that use thermal imaging at self-service interaction stations. In particular, embodiments may relate to a self-service station for conducting an interaction process, having a thermal imaging device configured to capture thermal images of an area, a processor configured to process the thermal images captured by the thermal imaging device, determine a temperature condition of a face identified in at least one of the captured thermal images and suspend the interaction process based on the determined temperature condition.

The present technology relates to a transport device, a transport method, a program, and an information processing device that can prevent damage to the content of luggage during transportation.

The transport device includes a luggage characteristic estimation unit that estimates luggage characteristics including at least one of fragility of a content of luggage and packaging quality of the luggage based on at least one of change in center of gravity due to movement of the luggage, vibration characteristics of the luggage, and characteristics of the sound generated from the luggage due to the movement of the luggage. The present technology can be applied to, for example, a robot that transports luggage.

An unmanned aerial vehicle (UAV) system, location and method, for operation with a flight management system, has a controlled access UAV zone for at least one of: UAV landing, UAV loading, and UAV take-off. A sensor can be in communication with a control panel and/or a lock to govern access to the UAV zone. The zone can have a barrier with closure secured by the lock, and controlled by a flight management system. Separate access codes can be provided for departure and destination locations, to enable personnel associated with a delivery request to access those locations, to effect delivery of an article. The codes can be generated and supplied when the flight management system receives a valid delivery request.

This invention is a connecting device for earth grounding aircraft and aerospace equipment. The connector assembly has two parts, an upper and lower. The upper part of the connector provides a receptacle to secure an aerospace chassis ground wire. An internal magnet holds the upper part to the lower part. The lower part is secured in the ground and is flush with the surrounding surface. It is subterraneously connected to a ground rod. Upon disconnection and removal of the upper part, the lower part stays in place and provides a smooth and unencumbered surface.

A charging system for mitigating charging failure for an electric aircraft, the system comprising a charger port located on the electric aircraft and configured to mate with a charging connector, a sensor communicatively connected to the charger port and configured to detect a charging datum, and a controller communicatively connected to the charger port and the sensor. The controller is configured to receive charging datum from the sensor, detect a charging failure as a function of a comparison between the charging datum to a pre-set charging datum threshold, and record the charging failure in a database.

Aspects relate to a charger for an electric aircraft with failure monitoring and method for its use. An exemplary charger for an electric aircraft with failure monitoring includes a charging circuit. Included within the charging circuit is a connector configured to mate with an electric aircraft port of an electric aircraft and at least a current conductor configured to conduct a current. At least a conductor comprises a direct current conductor configured to conduct a direct current. A charger may include a control circuit configured to command the charging circuit of an electric aircraft as a function of charging datum. A charger may also include a failure monitor circuit, the failure monitor circuit configured to initiate a failure mitigation procedure as a function of a failure of the charging circuit.

A method includes conveying baggage through a baggage claim system, receiving a code from a first passenger in a queue, and scanning codes on the baggage in the baggage claim system for a baggage item that matches with the code received from the first passenger. The method includes detecting the bagging item that matches with the code received from the first passenger and diverting the baggage item from the baggage conveyed through the baggage claim system for retrieval by the first passenger. This can be performed without the first passenger touching any of the baggage in the baggage claim system other than the baggage item that matches with the code received from the passenger, and without any other passengers touching the baggage item.

An unmanned aerial vehicle (UAV) navigation system includes a portable, ground-based landing pad comprising having a first antenna configured to transmit a data packet; a UAV comprising a second antenna configured to receive the data packet; and second processing circuitry configured to determine a signal strength between the first antenna and the second antenna; determine, based on the signal strength, an orientation of the vehicle relative to the landing pad; and determine, based on a time of flight of the data packet, a distance between the vehicle and the landing pad.

An unmanned aerial vehicle (UAV) navigation system includes a portable, ground-based landing pad comprising having a first antenna configured to transmit a data packet; a UAV comprising a second antenna configured to receive the data packet; and second processing circuitry configured to determine a signal strength between the first antenna and the second antenna; determine, based on the signal strength, an orientation of the vehicle relative to the landing pad; and determine, based on a time of flight of the data packet, a distance between the vehicle and the landing pad.