Determinação do Momento de Inércia de Aeronaves não Tripuladas com Métodos Pendulares

Abstract

The moment of inertia of mass is one of the quantities most important used to determine the dynamic stability characteristics of aircrafts. To determine this magnitude there are analytical methods, computational methods and experimental methods, the present research uses the pendular experimental methods to determine the moment of inertia of the VANT LCK 2018 of the Car-Kará Advanced team, as well as to compare it with the values obtained through the analitical method with semi-empirical equations and computational method. It also demonstrates how the bench was designed to perform the experiments and the algorithm for processing the experimental data. In addition, is compared the experimental results with results of the others methods.