Design of a two-degree-of-freedom helicopter with disturbances in the tail rotor

The design of a two degrees of freedom with an electromechanical mechanism for the generation of disturbances in the tail rotor is presented. The design focuses on a laboratory platform that replicates the dynamics of a helicopter at Pitch and Yaw angles. This platform allows the analysis of the control schemes in the face of the variation in the incidence in the tail rotor by means of a servomotor. The included files are: *Design plans in PDF. *PDF 3D design file. *CAD design on the 2022 inventor software. *Programming files in the simulink environment. *Videos of the simulation and operation of the mechanism of the disturbance generator in the tail rotor. *Video of the two degree-of-freedom helicopter operation. *Programming and interface files on Matlab Simulink for system operation.