A flight hindrance display apparatus includes circuitry. The circuitry is configured to acquire surrounding information of an aircraft. The surrounding information is related to a hindrance factor which is a possible flight hindrance to the aircraft. The circuitry is configured to determine a spatial range of the flight hindrance factor on a basis of the acquired surrounding information. The circuitry is configured to determine a flight hindrance cross-section that intersects a plane including a vector of a flight direction of the aircraft and is included in the determined spatial range of the flight hindrance factor. The circuitry is configured to cause a display unit to stereoscopically display an own position of the aircraft, the spatial range of the flight hindrance factor, and the flight hindrance cross-section.

A cargo transport system includes a UAV and a vehicle for sending and receiving the UAV. The UAV has a navigation system for guiding the UAV to fly to transport cargos between the vehicle and a terminal according to first navigation position information of the vehicle and the terminal. The vehicle includes a UAV accommodating device and a UAV receiving controller for guiding the UAV to the vehicle based on wireless signal transmitted directly between them when the UAV flies into a preset range around the vehicle. The UAV receiving controller includes: an identity verification unit for providing information to the UAV in response to a request broadcasted by the UAV to determine whether the vehicle is a target vehicle where the UAV is to land; and a short distance guide unit which provides information for guiding the UAV to land when the vehicle is the target vehicle.

A method, computing system and computer program product are provided to monitor compliance with a non-transgression zone between aircraft approach corridors, thereby facilitating simultaneous instrument approaches. In the context of a method, a predicted path of an aircraft is determined during a flight based upon at least a representation of a roll angle of the aircraft and a cross-track component of the velocity of the aircraft. The method also includes identifying an instance in which the predicted path of the aircraft during the flight intersects a non-transgression zone. The method further includes causing an alert to be issued in the instance in which the predicted path of the aircraft during the flight intersects the non-transgression zone.

Systems and methods are disclosed for acquiring data from avionics servers, flight management systems, or connected flight management system cloud services. In some embodiments, a method for acquiring data from avionics servers, flight management systems, or connected flight management system cloud services may include: receiving a dataset request from an input device; generating a plurality of sub-requests for a plurality of partial datasets from the avionics server; transmitting the plurality of sub-requests to a plurality of instances of the avionics server; generating identifications for each of the plurality of partial datasets; assembling the plurality of partial datasets into a single dataset; and transmitting the single dataset to the input device.

A system for graphical indication of a corridor is disclosed. The system may include a display and a processor. The processor may be configured to receive corridor position data of a corridor and aircraft position data indicative of a position of an aircraft. The processor may also be configured to determine a relative distance of the aircraft in relation to the corridor based on the corridor position data and the aircraft position data. The processor may further be configured to display a corridor graphic associated with the corridor based on the relative distance.

A management system provided with an acquisition unit that acquires machine identification information for identifying an unmanned moving apparatus, operation data indicating positions of the unmanned moving apparatus corresponding to the machine identification information, and action states of the unmanned moving apparatus; a storage control unit that stores the machine identification information in association with the operation data and the action states acquired by the acquisition unit; and an output control unit that outputs, in display forms corresponding to the action states, a path over which the unmanned movement apparatus moved, based on the operation data.

A system and method for management of airspace for unmanned aircraft is disclosed. The system and method comprises administration of the airspace including designation of flyways and zones with reference to features in the region. The system and method comprises administration of aircraft including registration of aircraft and mission. A monitoring system tracks conditions and aircraft traffic in the airspace. Aircraft may be configured to transact with the management system including to obtain rights/priority by license and to operate in the airspace under direction of the system. The system and aircraft may be configured for dynamic transactions (e.g. licensing/routing). The system will set rates for licenses and use/access to the airspace and aircraft will be billed/pay for use/access of the airspace at rates using data from data sources.

This disclosure is directed to techniques for automated transmission of surveillance incident data or other anomalous incident data from an aircraft via a preferred transmission mode. An example method includes detecting, by a processing device onboard an aircraft, an anomalous incident involving the aircraft that qualifies for reporting relative to a set of anomalous incident reporting criteria. The method further includes identifying, by the processing device, data onboard the aircraft relevant to the anomalous incident. The method further includes detecting that the aircraft is in a status that makes available a selected data transmission mode for transmitting the data relevant to the anomalous incident. The method further includes communicating the data relevant to the anomalous incident to a transmission system for transmission from the aircraft via the selected data transmission mode in response to detecting that the aircraft is in the status that makes available the selected data transmission mode.

A collaborative aviation information collection and distribution system includes a plurality of aircraft data transmitters and an aircraft data processing system. Each aircraft data transmitter is configured to selectively transmit aircraft data associated with a subscribing aircraft. The aircraft data processing system is in operable communication with each of the aircraft data transmitters and includes a data receiver, a data transmitter, and a data processor. The data receiver receives aircraft data transmitted from each of the aircraft transmitters. The data transmitter selectively transmits actionable aircraft data to one or more of the subscribing aircraft or subscribing ground-based users. The data processor determines which of, and when, the one or more subscribing aircraft or subscribing ground-based users should receive actionable aircraft data, generates actionable aircraft data from at least a portion of the received aircraft data, and supplies the generated actionable aircraft data to the data transmitter for transmission.

Systems and methods for UAV safety are provided. An authentication system may be used to confirm UAV and/or user identity and provide secured communications between users and UAVs. The UAVs may operate in accordance with a set of flight regulations. The set of flight regulations may be associated with a geo-fencing device in the vicinity of the UAV.