bachelorThesis
Aplicação de princípios de controle aeroespacial com dois graus de liberdade em um protótipo de aeronave de duas hélices
Fecha
2018-06-11Registro en:
OLIVEIRA, Gustavo Felipe de; PAIVA, Marcel Cachova de; SCHWAMBACH, Matias. Aplicação de princípios de controle aeroespacial com dois graus de liberdade em um protótipo de aeronave de duas hélices. 2018. 69 f. Trabalho de Conclusão de Curso (Graduação em Engenharia Elétrica) - Universidade Tecnológica Federal do Paraná, Curitiba, 2018.
Autor
Oliveira, Gustavo Felipe de
Paiva, Marcel Cachova de
Schwambach, Matias
Resumen
This work has the analysis of a Twin Rotor prototype built in the laboratory, the development of its mathematical modeling, the identification of unknown parameters and its control. The control is done through MATLAB, and the PID control is used. The prototype is composed by two rotors, which entail a movement of the prototype in two axes. Works that have in their scope experimental results, such as this one, have challenges that go beyond the mathematical part, as it is also described in the course of the final part of the work. The results are shown in graphs and their analysis is described below.