Construction, Modeling and Simulation of a Mini-unmanned Aircraft in DELTA Configuration

Abstract

We present the design and construction of a UAV in delta configuration in order to accomplish certain tasks and requirements which are explained along this document. We presented too, after the construction, the dynamic model of the UAV developed, based on its structural characteristics and obtained through the Newton-Euler method. The final dynamic model is restricted to longitudinal motion to simplify the system and make it easy to simulate using a control law which will lead the system to the stabilization of the aircraft along the longitudinal axis. These simulations of the dynamic model included the control law were added to demonstrate the capability of the aircraft designed to be longitudinally stabilized.