Obstacle avoidance by a remote or autonomously operated vehicle, such as an unmanned aerial vehicle (UAV), is of critical importance. By utilizing a monocular camera, a UAV may capture an image and select a middle sub-image for processing. If the average depth of the pixels in the middle sub-image is greater than a previously determined threshold, the UAV may proceed forward. However, if the average depth of the pixels is less than the threshold, a turn is required. A left sub-image and a right sub-image are processed and, based on the one having the greatest depth, a turn instruction is provided to the UAV.

There is provided a management apparatus configured to allocate a plurality of zones capable of identifying a three-dimensional space in common among a plurality of mobile communication carrier networks to a flight airspace allowing a plurality of mobile terminals to be flown, the plurality of mobile terminals being configured to respectively perform wireless communication with the plurality of mobile communication carrier networks, and configured to transmit information on allocation of the plurality of zones to a mobile communication network respectively managed by the plurality of mobile communication carriers.

A method is provided for supporting a robot in response to a contingency event. The method includes detecting the contingency event during travel of the robot on a route to a destination. In response, the method includes determining a position of the robot, and accessing information about alternate destinations associated with the route. The method includes selecting an alternate destination from the alternate destinations based on a time to travel from the position of the robot to the alternate destination, and the information. And the method includes outputting an indication of the alternate destination for use in at least one of guidance, navigation or control of the robot to the alternate destination.

A method and assembly for guidance of an aircraft during a low-altitude flight. The guidance assembly comprises a memory forming part of a flight management system, which is configured to store an active flight trajectory and any new flight trajectory, generated by the flight management system, and a memory forming part of a guidance system, which is configured to also store the flight trajectory and any new flight trajectory, which are received from the flight management system, the guidance assembly being configured to periodically transmit from the guidance system to the flight management system identification codes for the flight trajectories recorded in the memory of the guidance system.

The present disclosure is generally directed to a method of generating and displaying a parachute flare drift vector symbol on a navigation display of the aircraft capable of deploying a flare relative to a real-time navigation map. The flare drift vector symbol includes a flare ignition forward/aft distance relative to the aircraft deploying the flare, a flare ignition left/right distance relative to the aircraft deploying the flare, a flare burn vector distance, and a flare burn vector direction. The flare drift vector symbol is generating based on the flare parameters, the wind parameters, the flare drift distance, the flare drift direction and the aircraft parameters.

A device receives a request for a flight path for a UAV from a first location to a second location, credentials for the UAV, and component information for the UAV. The device determines, based on the credentials, whether the UAV is authenticated for utilizing the device and a network, and determines whether the UAV is capable of flight based on the component information and maintenance information. The device calculates, the flight path based on capability information for the UAV and/or other information, and determines whether the UAV is capable of traversing the flight path based on the capability information and/or the other information. The device generates flight path instructions for the flight path, and provides the flight path instructions to the UAV to permit the UAV to travel from the first location to the second location via the flight path.

To provide third parties, such as government and private actors, control over aerial drones and/or the ability to communicate with operators of such drones, a signaling system can provide one or more instructions to drones equipped with situational control systems configured to process and/or use such instruction(s). The instruction(s) can include information presentable to the operators (e.g., via remote control mechanisms associated with the aerial drones), such as one or more options for repositioning and/or landing the drones. The instruction(s) can additionally, or alternatively, include data (e.g., coordinate or control information) usable by the aerial drones to reposition or land.

An aviation flight planning system is used for predicting and warning for intersection of flight paths with transported meteorological disturbances, such as transported turbulence and related phenomena. Sensed data and transmitted data provide real time and forecast data related to meteorological conditions. Data modelling transported meteorological disturbances are applied to the received transmitted data and the sensed data to use the data modelling transported meteorological disturbances to correlate the sensed data and received transmitted data. The correlation is used to identify transported meteorological disturbances source characteristics, and identify predicted transported meteorological disturbances trajectories from source to intersection with flight path in space and time. The correlated data are provided to a visualization system that projects coordinates of a point of interest (POI) in a selected point of view (POV) to displays the flight track and the predicted transported meteorological disturbances warnings for the flight crew.

A method and apparatus of controlling movement of an aircraft. A turn path off of a planned route for an aircraft comprising a turn to direct the aircraft to an intercept point on the planned route is determined. A planned route indicator depicting the planned route, a turn path indicator depicting the turn path, and an aircraft position indicator indicating a position of the aircraft are displayed to an operator of the aircraft at the same time on a turn guidance display. Deviation limit indicators for the planned route, the turn path, or both, may be displayed on the turn guidance display. Indicator characteristics of the deviation limit indicators may be changed in response to aircraft deviations from the planned route or the turn path by more than the deviation limits. The turn guidance display is used to control the movement of the aircraft to follow the turn path.

The DYNAMIC AIRCRAFT THREAT CONTROLLER MANAGER APPARATUSES, METHODS AND SYSTEMS (DATCM) transforms flight profile information, terrain, weather/atmospheric data and flight parameter data via DATCM components into comprehensive hazard avoidance optimized flight plans. Comprehensive hazard avoidance includes synergistic comprehensive turbulence and airfoil-specific icing data. In one implementation, the DATCM comprises a processor and a memory disposed in communication with the processor and storing processor-issuable instructions to receive anticipated flight plan parameter data, obtain weather data based on the flight plan parameter data, obtain atmospheric data based on the flight plan parameter data, and determine a plurality of four-dimensional grid points based on the flight plan parameter data. The DATCM may then determine comprehensive hazards mappings. With (near) real-time comprehensive hazard information and/or predictive turbulence/icing forecast specific to airfoil type and/or profile parameters, the DATCM may allow aircraft to avoid areas where comprehensive hazard is greater than a predetermined threshold and/or avoid areas where turbulence/icing may occur.