The objective of this project is the implementation of the position control for an ElectroMechanical Actuator (EMA) used to move the rudder of an aircraft. This project is the continuation of EMACON (Electromechanical Actuator Control) project. In the EMACON project the control algorithm was designed and implemented in the DSP TMS320F2812 from Texas Instruments. However, due to delays in that project, all due to reasons outside the scope of the project, the implemented control could not be tested experimentally. Hence, this project has the purpose to finish the work started in the EMACON project.