Arduino Applicability Model for the Construction of Flight Controller for Drones
Ademir de Cerqueira e Silva dos Santos, João Carlos Silva de Oliveira · International Journal of Advanced Engineering Research and Science · 2019
The aim of this study was to develop a flight developer for an unmanned aeronautical vehicle (UAV) with copyright technology.The project takes into account several aspects of Mechanical Engineering, as well as knowledge of aircraft dynamics, remote control, sensin g and electronics, composing a multidisciplinary work of Electronics, Mechatronics and Aeronautical Engineering.In this project, the UAV is divided into its fundamental components: structure/base , engines, propellers, flight controllers, batteries, sensors and radio, each one being studied and specified for the integration of a full system.Simulation tools and calculation softwares are used to estimate the main features of the final product.We presume that this article serves as a reference for a drone project in general and a guide to the physical production of such a drone, from the initial design with specifications to the selection and integration of components for future work and research projects, becoming a valuable tool of great added value.