Integrated control system for an unmanned aerial vehicle, method and device

Abstract

The application relates to a device for controlling an unmanned aircraft. A device for controlling an unmanned aircraft, comprising a base part (1), flight control mechanisms (3), a power source (4), a video camera (6), an analog-to-digital signal conversion device (7), a signal amplification device (8), a computing device (9), an electronic memory (10), a radio transmitter / receiver (12), a signal encryption / decryption device (18), an operator's monitor (19), and an operator's control panel (20). The device further comprises a detachable part (2), in turn comprising a reel with an optical cable (13), a radio transmitter / receiver (14), a device for slowing down the descent rate (15), a power source (16), an analog-to-digital signal conversion device (17), and a signal encryption / decryption device (21).The application also concerns a method of controlling an unmanned aircraft, according to which the image from a video camera and / or other on-board observation devices is transmitted to the operator and displayed on his monitor, and then control instructions are transmitted from the operator in the return direction.