AERIAL DRONES / UAV’S NEWEST PATENTS AND APPLICATIONS

[EN] METHOD FOR MANAGING A VEHICLE CONTROLLED REMOTELY VIA A COMMUNICATION NETWORK, CORRESPONDING DEVICE, SYSTEM AND COMPUTER PROGRAM

[EN] The invention relates to a method for managing a position of a remotely-controlled vehicle (UAV, 10), referred to as a drone, relative to a control entity (UAVC, 11), said control entity being configured to control the drone via a stream of control data transmitted indirectly within a communication established between the control entity (11) and the drone (10) via a communication network (RC), said method comprising: – for at least one time instant of the communication, determining (E6) at least one parameter relating to a distance between the drone and the control entity; – when the distance-related parameter does not lie within an interval of authorised values for a given piloting mode, applying (E10) at least one given management rule for the drone.

[EN] BOX FRAME OF AN UNMANNED AERIAL VEHICLE

[MT] Flight vehicle and control method of flight vehicle

[MT] A method of controlling a flight vehicle UAV that autonomously flies based on position information of a flight vehicle UAV that provides a flight vehicle and a method of controlling a flight vehicle that can stably fly even when moving between a GNSS environment and a non-GNSS environment, the flight vehicle UAV having an RTK-GNSS positioning function, a sensor positioning function, a range finding function, An orientation acquisition function and a flight control function for controlling the flight of the flight vehicle on the basis of these information. When the control part C always performs the grasp of the position of the flight vehicle UAV by the RTK-GNSS positioning function and the sensor positioning function, and the RTK-GNSS positioning function obtains a fix solution, The control unit C controls the flight of the flight vehicle on the basis of the positional information of the flight vehicle UAV obtained from the RTK-GNSS positioning function, and when the RTK-GNSS positioning function cannot obtain the fix solution, the control unit C controls the flight of the flight vehicle on the basis of the positional information of the control unit C obtained from the sensor positioning function. Figure 1

[EN] COAXIAL ROTOR MINI UNMANNED AERIAL VEHICLE

[EN] UNMANNED AERIAL VEHICLE CAPABLE OF RESPONDING TO DISTURBANCES

[MT] The unmanned aerial vehicle includes a first sensor module , a second sensor module , a first motor module , a rotor portion , a control module , And a battery module . The rotor unit converts a force received by the first motor module into a positive force . The battery module provides power to at least one of the first sensor module , the second sensor module , the first motor module , and the control module . The unmanned aerial vehicle controls an attitude based on at least one of the first information generated by the first sensor module and the second information generated by the second sensor module , and when the control module determines that the first information is not normal , the attitude based on only the second information generated by the second sensor module . That is , when a disturbance has occurred , the attitude is controlled based on second information ( collected in the radar sensor and the vision sensor ) which is not affected by the disturbance .