A cruising distance calculation device includes a distance calculation unit configured to calculate a cruising distance of an eVTOL which is an electric moving object moving in a horizontal direction and a vertical direction, and an output unit configured to output information related to a calculation result of the distance calculation unit. The distance calculation unit acquires a corrected remaining power amount obtained by correcting a remaining power amount of a battery provided to the eVTOL with a departure and arrival power amount required during departure and/or arrival of the eVTOL, and calculates the cruising distance based on the corrected remaining power amount.

A method includes determining, at a computing system of an aircraft, a target path for an approach to landing based on flight data. The method includes determining an approach phase of approach phases of the approach to landing. The method includes determining a real-time operational region of the aircraft for each monitored condition of monitored conditions based on the real-time aircraft data, the target path, and operational regions for each monitored condition. The method includes accessing notification content for a particular monitored condition for the approach phase. The real-time operational region for the particular monitored condition for the approach phase is outside of a target region of the particular monitored condition for the approach phase. The method also includes sending one or more notification signals based on the notification content from the computing system to one or more output systems.

A method includes determining, at a computing system of an aircraft, a target path for an approach to landing based on flight data. The method includes determining an approach phase of approach phases of the approach to landing. The method includes determining a real-time operational region of the aircraft for each monitored condition of monitored conditions based on the real-time aircraft data, the target path, and operational regions for each monitored condition. The method includes accessing notification content for a particular monitored condition for the approach phase. The real-time operational region for the particular monitored condition for the approach phase is outside of a target region of the particular monitored condition for the approach phase. The method also includes sending one or more notification signals based on the notification content from the computing system to one or more output systems.

A method for controlling a plurality of drones to survey a location, the method comprising, at a computing system: automatically generating preliminary flight plans for a plurality of drones to survey the location based on a 3D model; receiving survey data from the plurality of drones as the plurality of drones are surveying the location based on the preliminary flight plans; updating the 3D model based on the survey data received from the plurality of drones; and automatically updating at least a portion of the flight plans based on the updated 3D model

A method for controlling a plurality of drones to survey a location, the method comprising, at a computing system: automatically generating preliminary flight plans for a plurality of drones to survey the location based on a 3D model; receiving survey data from the plurality of drones as the plurality of drones are surveying the location based on the preliminary flight plans; updating the 3D model based on the survey data received from the plurality of drones; and automatically updating at least a portion of the flight plans based on the updated 3D model

A method performed by a wireless transmit/receive unit (WTRU) implemented in a first unmanned aerial vehicle (UAV1) includes registering detect and avoid (DAA) capability in a registration message transmitted by the first UAV to an unmanned aerial system (UAS) service supplier (USS), detecting a flight path conflict with a second UAV (UAV2), selecting a unicast or broadcast communication mode with the UAV2, transmitting to the UAV2 the DAA capability of the UAV1 and a deconfliction message based on the selected communication mode, and avoiding a collision by executing a trajectory correction.

A method performed by a wireless transmit/receive unit (WTRU) implemented in a first unmanned aerial vehicle (UAV1) includes registering detect and avoid (DAA) capability in a registration message transmitted by the first UAV to an unmanned aerial system (UAS) service supplier (USS), detecting a flight path conflict with a second UAV (UAV2), selecting a unicast or broadcast communication mode with the UAV2, transmitting to the UAV2 the DAA capability of the UAV1 and a deconfliction message based on the selected communication mode, and avoiding a collision by executing a trajectory correction.

A system for navigating an aircraft, comprising a flight planning system configured to prepare a set of at least three different trajectories for a flight from a departure point to a destination point, a flight verification system configured to verify each trajectory of the set of trajectories, an onboard flight management system to be installed at an aircraft and having a storage unit for storing the set of trajectories, wherein the flight management system is configured to select one of the trajectories from the set of trajectories as an active trajectory for a current flight of the aircraft, wherein the flight management system includes a replanning unit configured to change, during the current flight, the active trajectory by selecting a second trajectory from the set of trajectories as the active trajectory for the current flight, such as to continue the current flight based on the second trajectory t.

A system for navigating an aircraft, comprising a flight planning system configured to prepare a set of at least three different trajectories for a flight from a departure point to a destination point, a flight verification system configured to verify each trajectory of the set of trajectories, an onboard flight management system to be installed at an aircraft and having a storage unit for storing the set of trajectories, wherein the flight management system is configured to select one of the trajectories from the set of trajectories as an active trajectory for a current flight of the aircraft, wherein the flight management system includes a replanning unit configured to change, during the current flight, the active trajectory by selecting a second trajectory from the set of trajectories as the active trajectory for the current flight, such as to continue the current flight based on the second trajectory t.

A system for generating navigation instructions for delivery of a cargo is provided. The system is configured to obtain geographic area information relating to a geographic area, determine cargo information relating to the cargo, determine one or more aerial routes for a delivery of the cargo based on the geographic area information and the cargo information, estimate a risk value for navigation of an aerial vehicle across each of the one or more aerial routes, identify an aerial route from the one or more aerial routes having lowest estimated risk value based on the estimated risk values for the one or more aerial routes, and generate the navigation instructions for navigation of the aerial vehicle along the identified aerial route for delivery of the cargo.