Modelling and control system design for uav tri-rotor

Hernando González, Carlos Arizmendi, César Valencia, Diego Valle, Brayam Bernal, Alhim Vera

Resultado de la investigación: Libro / Capitulo del libro / InformeLibros de Investigaciónrevisión exhaustiva

Resumen

The drones are devices of high technology that work thanks to the rotors that allow them to remain and to be propelled in the air. Their movements are controlled by adjusting the propulsion of each propeller and this is done with a device called a flight controller. The paper presents two control system for a UAV-Tricopter. The control techniques proposed are: proportional derivative and integral controller (PID) and Linear Quadratic Gaussian Controller (LQG). These techniques force the tricopter to follow with precision the given trajectory. The simulink toolbox was used to make the designs of each controller and then see the behavior of each control strategy.

Idioma originalInglés
Título de la publicación alojadaAETA 2019 - Recent Advances in Electrical Engineering and Related Sciences
Subtítulo de la publicación alojadaTheory and Application
EditoresDario Fernando Cortes Tobar, Vo Hoang Duy, Tran Trong Dao
EditorialSpringer
Páginas84-93
Número de páginas10
ISBN (versión impresa)9783030530204
DOI
EstadoPublicada - 2021
Evento6th International Conference on Advanced Engineering Theory and Applications, AETA 2019 - Bogota, Colombia
Duración: 6 nov. 20198 nov. 2019

Serie de la publicación

NombreLecture Notes in Electrical Engineering
Volumen685 LNEE
ISSN (versión impresa)1876-1100
ISSN (versión digital)1876-1119

Conferencia

Conferencia6th International Conference on Advanced Engineering Theory and Applications, AETA 2019
País/TerritorioColombia
CiudadBogota
Período6/11/198/11/19

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