Unmanned aerial vehicle

Abstract

The utility model relates to vertical takeoff and landing (VTOL) aircraft. The unmanned aerial vehicle comprises a fuselage housing an onboard electronics unit, a tail-mounted propeller, and side-mounted left and right consoles, each of which supports a left and right boom, each of which in turn supports two lifting propellers. Additionally, left and right tail stabilizers are mounted on the rear of each boom, interconnected at the top. The forward fuselage contains an air pressure receiver in the form of a combined pneumometric tube, secured to a bracket and connected via static, dynamic, and total air pressure lines to an integrated multifunctional avionics unit.A digital magnetic compass and a two-way half-duplex data exchange radio modem are mounted within the aluminum housing at the bottom of the left wing, while a radio altimeter is mounted on the bottom of the fuselage, under the battery. The tail section of the fuselage houses a processing bay housing an integrated multifunctional avionics unit and a brushless electric motor to generate the thrust required for horizontal flight. Additionally, ailerons, navigation lights, and speed controllers are symmetrically located on the trailing edges of each wing. The technical result of using the claimed unmanned aerial vehicle is increased accuracy in automatic flight mode. 1 fig.