Modeling and Linearization of a 1-GDL Helicopter System for Digital Controller Design: PID and via State Feedback

Authors

  • Isabelle Caroline Sousa Gonçalves Departamento de Engenharia Mecatrônica, Centro Federal de Educação Tecnológica de Minas Gerais, CEFET-MG, Brazil https://orcid.org/0009-0008-5034-0560
  • Micaellen Christie Cecília Carvalho Departamento de Engenharia Mecatrônica, Centro Federal de Educação Tecnológica de Minas Gerais, CEFET-MG, Brazil https://orcid.org/0009-0003-0234-5627
  • Igor Ribeiro Pereira Departamento de Engenharia Mecatrônica, Centro Federal de Educação Tecnológica de Minas Gerais, CEFET-MG, Brazil https://orcid.org/0009-0002-4692-499X
  • Gabriel Lopes dos Santos Departamento de Engenharia Mecatrônica, Centro Federal de Educação Tecnológica de Minas Gerais, CEFET-MG, Brazil
  • Cláudio Henrique Gomes dos Santos Departamento de Engenharia Mecatrônica, Centro Federal de Educação Tecnológica de Minas Gerais, CEFET-MG, Brazil

DOI:

https://doi.org/10.18540/jcecvl10iss2pp17163

Keywords:

Helicopter with 1-GDL, Digital control, PID approach, State feedback, MATLAB

Abstract

This work intent to develop the modeling and linearization of a helicopter system with one degree of freedom (1-GDL), using MATLAB and Simulink software. Then, two digital controllers were designed, using the PID approach and state feedback, to evaluate robustness and rejection of disturbances through performance indices and design specifications. Accordingly with the results obtained, it was found that the compensator via state feedback showed better performance in the angular position stabilization process.

Downloads

Download data is not yet available.

Published

2024-03-24

How to Cite

Gonçalves, I. C. S., Carvalho, M. C. C., Pereira, I. R., Santos, G. L. dos, & Santos, C. H. G. dos. (2024). Modeling and Linearization of a 1-GDL Helicopter System for Digital Controller Design: PID and via State Feedback. The Journal of Engineering and Exact Sciences, 10(2), 17163. https://doi.org/10.18540/jcecvl10iss2pp17163

Issue

Section

General Articles