Sistema autónomo de control para la ejecución de vuelos programados en aviones de ala fija

Abstract

CONDITION FOR PUBLICATION OF PROJECT. This project aims to overcome the challenges associated with optimal logistics transport in rural areas of Ecuador from the perspective of using an autonomous control system in a fixed-wing unmanned aerial vehicle (UAV). The main focus is to validate an open-architecture experimental platform for programmed flight operations based on the Pixhawk controller and the Reno L250 fuselage. The methodology included the structural assembly of the aircraft, the integration of electronic propulsion and navigation components, and the configuration of flight modes and autonomous missions using Mission Planner software. Static thrust tests and control surface calibration were performed in the laboratory; subsequently, field tests confirmed the dynamic response. The results showed a successful takeoff and consistent flight stability under assisted control. Furthermore, the correct integration of the avionics systems was demonstrated. The functional prototype proves to be a viable and modular technological platform for future research on navigation algorithms and autonomous aerial logistics use cases Keywords: Fixed-Wing UAV, Pixhawk, Autonomous Control, Mission Planner, Reno L250.