A current flight path of an aircraft is defined with respect to a two-dimensional mesh plane including a first plurality of nodes. Each node is associated with a pre-designated location. First, second, and third nodes that are the closest to a current aircraft location are identified. Neighboring aircraft data associated with neighboring aircraft disposed within a pre-defined distance of the aircraft is received. The neighboring aircraft data includes a neighboring aircraft location for each the neighboring aircraft. First, second, and third node weights are allocated to the first, second, and third nodes based in part on the pre-designated locations of the first, second, and third nodes with respect to the neighboring aircraft locations. A modified flight path based at least in part on the first, second, and third node weights is generated for display as a suggested flight path on an onboard display device.

Disclosed are systems and associated methods for calculating and displaying formation flight information, to include aircraft spacing, predicted trajectory data, collision avoidance alerts, time on target details, and chalk-specific information, on an augmented reality display designed to interface with aviation helmets. Two or more networked computing devices, each on a separate aircraft, collect some combination of aircraft altitude, location, and inertial data, preform certain calculations, and then develops a virtual overlay according to aircraft relative position and nearby aircraft trajectories. The virtual overlay is further informed by compass and gyroscopic data from an operatively coupled augmented reality display device. The developed virtual overlay is then transmitted to the display device for viewing by the pilot. The display of relevant formation flight information using augmented reality tools may result in improved formation flight spacing, emergency procedure response, and collision avoidance.

An aerial vehicle includes a communication unit configured to receive a wireless signal from a geo-fencing device, and a flight controller configured to generate one or more control signals that cause the aerial vehicle to operate in accordance with a set of flight regulations generated based on the wireless signal. The geo-fencing device is configured not for landing of the aerial vehicle. The set of flight regulations includes rules for controlling at least one of the aerial vehicle, a carrier carried by the aerial vehicle, or a payload of the aerial vehicle.

A control method includes obtaining sensing data output by an observation sensor of a movable platform when sensing a target object in an environment, determining a position of the target object based on the sensing data, and sending the position of the target object to another movable platform moving in the environment, or to a relay device for the relay device to send the position of the target object to the another movable platform.

An example operation may provide receiving, at a server, one or more communications from a drone, determining the one or more communications identify a drone identifier and a current time, determining whether the one or more communications were received within a time window, assigning a token to the identified drone indicating the drone is active, and storing the token as a transaction in memory.

The invention concerns a suborbital space traffic control system that comprises: a radar system configured to monitor a predetermined suborbital region and detect and track objects in the predetermined suborbital region. The objects include vehicles and space debris; and a suborbital space traffic monitoring system configured to: receive, from the radar system, tracking data related to the objects detected and tracked by the radar system; monitor, on the basis of the tracking data, trajectories of the objects in the predetermined suborbital region using one or more predetermined machine-learning techniques to detect potentially hazardous situations for the vehicles in the predetermined suborbital region; and, if it detects a potentially hazardous situation for one or more given vehicles, transmit corresponding alarm messages to the given vehicle(s).

An object of the present disclosure is to provide a flight management apparatus capable of improving the safety of flying objects. In one example, a flight management apparatus (10) of the present disclosure includes a determination unit (12) configured to determine whether a specific space cell in a space is already reserved based on a reservation state about the specific space cell, when the flight management apparatus receives a request for permission to move to the specific space cell from a flying object; and a permission unit (13) configured to permit the movement to the specific space cell of the flying object when the determination unit determines the specific space cell is not reserved, and not to permit the movement to the specific space cell of the flying object when the determination unit determines the specific space cell is already reserved.

A formation flight assistance system is placed on board a follower aircraft to benefit from an upwards air flow induced by a wake vortex generated by a leader aircraft. The system determines a wake vortex effect experienced by the follower aircraft as being a difference between measurements taken by sensors and modelling in a wake vortex free environment. Using a recursive Bayesian filter, the system determines an estimated position of the wake vortex on the basis of information relating to the leader aircraft and a wake vortex model, and determines an estimation uncertainty, according to which a potential discomfort window is computed for the passengers of the follower aircraft. The system keeps the follower aircraft outside the potential discomfort window. Thus, the comfort of the passengers of the follower aircraft is provided, while benefiting from an upwards air flow induced by the wake vortex.

Aircraft guidance with a multi-vehicle network is disclosed. A disclosed example apparatus to determine a position of an aircraft in a contested area includes a direction and distance calculator to determine a relative position of the aircraft to a mobile platform based on a signal transmitted between the aircraft and the mobile platform. The apparatus further includes a position calculator to calculate the position of the aircraft based on the relative position and a position of the mobile platform.

A system for providing maneuvering behaviors to a vehicle is disclosed. The system may include one or more controllers communicatively coupled to one or more vehicles. The one or more controllers may include one or more processors configured to execute one or more program instructions causing the one or more processors to: initiate one or more maneuver primitives in response to decision engine selection; receive a plurality of input parameters for the one or more maneuver primitives, the plurality of input parameters including one or more initialization definition input parameters, one or more goal definition input parameters, one or more navigation state input parameters, one or more design input parameters, and one or more vehicle performance envelope input parameters; and generate one or more control signals at one or more predetermined intervals of time to maneuver the one or more vehicles based on the decision engine selection.