A method may include detecting, during a flight of an aircraft system, a conflict with a planned route of the aircraft system, determining one or more alternate routes for the aircraft system to avoid the conflict, wherein each of the one or more alternate routes avoid secondary conflicts with active flight operations, transmitting first data to cause first visual information indicating the conflict and second visual information indicating the one or more alternate routes to be displayed to a user, receiving second data indicating one of the one or more alternate routes being selected by the user, and updating the planned route of the aircraft system to include the alternate route selected by the user.

A drone is provided that includes a controller, a time measurer that measures a present time, a position measurer that obtains a current position of the drone, and a storage that stores a time period for which the flight of the drone is permitted. The controller performs operations including determining a possible flight area of the drone in accordance with a difference between an end of the time period for which flight of the drone is permitted and the present time, and determining whether the drone is located within the possible flight area on the basis of the current position of the drone.

A method for planning flight trajectories for at least two aircraft aiming to subsequently approach a predefined reference point, in particular a predefined destination, wherein each aircraft travels along a flight route according to an individual flight trajectory, such that a first aircraft travels along a first flight route according to a first flight trajectory and a second aircraft travels along a second flight route according to a second flight trajectory, wherein at least the second flight trajectory is set or adjusted such that at least one predetermined minimum separation between the two aircraft approaching the predefined destination according to their respective flight trajectories is ensured and the predetermined minimum separation is ensured throughout the whole flight trajectories by setting or adjusting an adjustable trajectory parameter (θ) of the first or second flight trajectory.

Systems and methods for coordinating with a flight management system (FMS) on-board an aircraft to determine whether a flight plan (FP) change generated by an external device is valid. The method includes generating the FP change, which includes a deviation to the intended FP and a savings parameter associated with a parameter of the intended FP, responsive to weather data and aircraft state data; generating a lateral display showing the intended FP and an alphanumeric window with the FP change; transmitting the FP change to the FMS; receiving, from the FMS, a travel path and a calculated parameter for the travel path, generated by the FMS responsive to the FP change; determining whether the travel path realizes the savings parameter by comparing the calculated parameter to the savings parameter; and, displaying either a selectable graphical user interface (GUI) object to implement the FP change, or a warning based thereon.

Systems and methods for converting voice to text messages in an aircraft. The systems and methods transcribe voice messages between a member of the flight crew and Air Traffic Control (ATC) to provide ATC text messages, transcribe a voice-automatic terminal information service report (voice-ATIS) to provide an ATIS text report, determine flight context data based at least on an analysis of the ATC text messages, determine relevant ATIS data from the ATIS text report using the flight context data, and render a visual User Interface (UI) including at least some of the ATC text messages and at least some of the relevant ATIS data on the same ATC transcription page.

Examples for flight navigation determination are presented herein. An example may involve obtaining a target destination for an aircraft and determining an initial flight path between a current location and the target destination. The flight path may include a series of waypoints for guiding navigation. The example may further involve obtaining terrain information that represents elevations of obstacles along the initial flight path and modifying the initial flight path to generate a revised flight path using the terrain information. The revised flight path may include modifications to the series of waypoints of the initial flight path such that navigation of the revised flight path avoids obstacles positioned along the initial flight path. The obstacles may have an elevation that exceeds an adjustable threshold elevation that depends on the initial flight path. The example may further involve providing the revised flight path to a navigation system of the aircraft.

Certain aspects of the present disclosure provide a method for determining a flight plan for an aircraft, including: determining one or more regions that intersect an initial flight path and comprise at least one terrain feature having an elevation greater than an elevation threshold; for each respective region: determining a flight area based on the initial flight path and an elevation threshold line; determining one or more segments of the initial flight path that comprise one or more terrain features having an elevation greater than the elevation threshold; and determining a modified flight path for each respective segment by: determining a plurality of descent gradients along the respective segment; and moving the respective segment of the initial flight path in the safe descent direction if any of the plurality of descent gradients would collide with any of the one or more terrain features.

A method and system for continuously re-planning a vehicle's path, in the face of stationary and moving obstacles, dynamically calculates a new path in real time which is both efficient and maintains minimum safety clearances relative to obstacles. Repulsion signals emanating from obstacles and propagating through delineated sections of a grid representing a geographic space are summed along with values representing the relative distance of the sections from the vehicle origin and vehicle destination. The grid sections having optimal values according to a predetermined criteria represent an efficient and safe travel path between the vehicle origin and destination.

A method of displaying an electronic report on a GUI that includes receiving a user identifier and an authentication identifier associated with a user gaining access to a first application; displaying, on the GUI, a first window associated with the first application; displaying, via the first window, a listing of monitored flights; receiving, via the first window, a request; accessing, using the first application, a second application and a third application that are different from each other and the first application; updating the displayed listing of monitored flights using information accessed from the second and third applications; wherein a flight has a delay greater than two hours; and receiving, via the first window, a request for the electronic report for the flight; displaying, on the GUI and via a second window, the electronic report for the flight that includes information from each of the second and third applications.

Disclosed are embodiments for employing off board sensors to augment data used by a ground based autonomous vehicle. In some aspects, the off-board sensors may be positioned on another autonomous vehicle, such as an aerial autonomous vehicle (AAV). The disclosed embodiments determine uncertainty scores associated with ground regions. The uncertainty scores indicate a need to reimage the ground regions. An AAV may be tasked to reimage a region having a relatively high uncertainty score, depending on a cost associated with the tasking.