Methods, systems, and devices for wireless communications are described. A wireless network may receive a message from a wireless device that is coupled with an aerial vehicle. The message may include a network identifier, an aerial identifier, and operational information for the aerial vehicle. The wireless network may send a message to an aerial function management system requesting that the aerial function management system authenticate an identity of the aerial vehicle. The wireless network may also request that the aerial function management system approve a flight path for the aerial vehicle. The wireless network may establish a data session with the wireless device based on an authentication of the aerial vehicle and an approval of the flight path.

Provided are a method and device for setting a flight path reflecting an air space of a drone. The method may include receiving flight data collected by the drone; calculating a path error score indicating an extent of deviation of the drone from a planned flight path by comparing the received flight data with the planned flight path of the drone; adjusting the preset air space of the drone based on the path error score; and generating a new flight path of the drone based on the adjusted air space of the drone and a destination.

The present disclosure relates to an information processing apparatus, an information processing method, a program, and an information processing system capable of more easily realizing route planning.

A route planning unit selects, on the basis of priority information regarding setting of the moving route, a viaport where a moving object stops over from among a plurality of charging ports that charges the moving object, and sets a moving route of a moving object from a departure point to a destination. The technology according to the present disclosure can be applied to, for example, an information processing apparatus that performs automatic piloting of a drone.

A system for incorporating predictive health data into a mission timeline receives a predictive health event, identifies a time frame for the event, and incorporates the event into a mission timeline. The event may define a probability window with weighted probabilities overlaid onto the mission timeline. The event may define an uncorrected outcome. The uncorrected outcome is rendered onto the mission timeline at a point when the uncorrected outcome will likely occur if no remedial action is taken.

A method for controlling secure delivery of a medication package includes receiving a medication delivery request to deliver a medication package to a first delivery location. The method also includes identifying one or more authenticated delivery locations corresponding to a recipient and determining whether the one or more authenticated delivery locations includes the first delivery location and, in response to a determination that the one or more authenticated delivery locations includes the first delivery location, instructing an unmanned aerial vehicle to transport the medication package from a starting location to the first delivery location. The method also includes, in response to the unmanned aerial vehicle communicating authentication data, determining whether the authentication data corresponds to the recipient. The method also includes, in response to a determination that the authentication data corresponds to the recipient, instructing the unmanned aerial vehicle to release the medication package to the recipient.

A method and device for generating an optimum aircraft vertical trajectory, including a unit performing iterative processing to determine, on each iteration, a next state from a computational state, by using an estimated overall cost for next states, each estimated overall cost, which is computed by a cost computation unit, being equal to the sum of a real cost computed up to the next state under consideration by using predetermined constraints and a cost estimated up to the current state of the aircraft. The estimated cost is computed using a deterministic neural network based on performance calculations for the aircraft without using energy constraints, allowing computation of this estimated cost and the estimated overall cost to be performed rapidly. The iterative processing is repeated until the determined state is situated in proximity to the current state of the aircraft, the corresponding trajectory part forming the optimum vertical trajectory.

Disclosed are methods, systems, and non-transitory computer-readable medium for distributed vehicle processing. For instance, the method may include: in response to determining a first trigger condition of a first set of trigger conditions is satisfied, performing a first process corresponding to the first trigger condition on-board a vehicle; in response to determining a second trigger condition of a second set of trigger conditions is satisfied, prompting a second process corresponding to the second trigger condition by transmitting an edge request to an edge node and receiving an edge response from the edge node; and in response to determining a third trigger condition of a third set of trigger conditions is satisfied, prompting a third process corresponding to the third trigger condition by transmitting a cloud request to a cloud node and receiving a cloud response from the cloud node.

Methods of determining for a vehicle a three-dimensional path that extends between an origin and a destination. The paths are determined based on the vehicle having a limited amount of energy that is not resupplied during travel. The paths are further determined based on the vehicle arriving at the destination with a predetermined amount of remaining energy.

An automatic trajectory generation system bringing a flying aircraft from a current position to a destination which: obtains polygons representing obstacles potentially encountered, each polygon associated with an altitude layer; defines two first tangential circles relative to a current direction of the aircraft flight, centered on the right and the left, relative to the aircraft current position; defining two second circles tangential relative to a direction to be followed to destination, centered on the right and the left, relative to the georeferenced destination position; defines a third circle around vertices of the polygons; and searches for a flyable lateral trajectory between the aircraft current position and the destination by bypassing the polygons by the vertices in searching for tangential trajectories between the circles, by observing a pre-established vertical trajectory profile, as well as the lateral margin and a vertical margin with the polygons.

Systems and methods for a helideck approach path tool. One example system includes an electronic processor. The electronic processor is configured to determine a helideck identifier and retrieve, from a database storing data on a plurality of helidecks, helideck data corresponding to the helideck identifier. The helideck data includes a helideck azimuth and at least one obstacle characteristic. The electronic processor is configured to generate a graphical user interface including a helideck approach indicator object, which includes a compass ring, a graphical representation of the helideck aligned to the compass ring based on the helideck azimuth, and an obstacle indicator overlaid on the compass ring based on the at least one obstacle characteristic. The electronic processor is configured to present the graphical user interface on a display within the aircraft.