This is the list of publications of this laboratory
2014
Proceedings Articles
Martínez-Alvarado, Ricardo; Sánchez-Orta, Anand; Granda-Gutiérrez, E.; Ruiz-Sanchez, Francisco J.
performance evaluation of propeller-engine systems for unmanned aerial vehicles in hovering Proceedings Article
In: performance evaluation of propeller-engine systems for unmanned aerial vehicles in hovering, pp. 131-136, congreso internacional en ingenieria electronica electro 2014, 2014, ISSN: 1405-2172.
@inproceedings{Mart\'{i}nez-Alvarado2014,
title = {performance evaluation of propeller-engine systems for unmanned aerial vehicles in hovering},
author = {Mart\'{i}nez-Alvarado, Ricardo and S\'{a}nchez-Orta, Anand and Granda-Guti\'{e}rrez, E. and Ruiz-Sanchez, Francisco J.},
url = {https://www.researchgate.net/publication/267094930_PERFORMANCE_EVALUATION_OF_PROPELLER-ENGINE_SYSTEMS_FOR_UNMANNED_AERIAL_VEHICLES_IN_HOVERING_MODE},
issn = {1405-2172},
year = {2014},
date = {2014-00-00},
booktitle = {performance evaluation of propeller-engine systems for unmanned aerial vehicles in hovering},
volume = {36},
pages = {131-136},
publisher = {congreso internacional en ingenieria electronica electro 2014},
abstract = {A flexible tool to dimensioning and optimizing the performance of a propeller-engine system for multi-rotor Unmanned Aerial Vehicles (UAVs) is proposed. The study is centered on an experimental platform designed to identify the dynamic behavior of the thruster which operates as main actuator in multi-rotor UAVs. The aim is to optimize the performance of the propulsion system with basis on its dynamic behavior. The dynamic of an UAV changes notably according to the performance of the thruster, which is composed by a propeller coupled to a Brushless Direct Current (BLDC) Motor. The dynamic response of the propulsion system is acquired from the experimental data, including the electric, mechanical and aerodynamic effects of the wing when the propeller is the load of the rotor. The experimental platform allows evaluating the performance of the system and determining the payload for a UAV, but also validates control laws to regulate the thruster action.
PERFORMANCE EVALUATION OF PROPELLER-ENGINE SYSTEMS FOR UNMANNED AERIAL VEHICLES IN HOVERING MODE (PDF Download Available). Available from: https://www.researchgate.net/publication/267094930_PERFORMANCE_EVALUATION_OF_PROPELLER-ENGINE_SYSTEMS_FOR_UNMANNED_AERIAL_VEHICLES_IN_HOVERING_MODE [accessed Jun 16, 2017].},
keywords = {},
pubstate = {published},
tppubtype = {inproceedings}
}
A flexible tool to dimensioning and optimizing the performance of a propeller-engine system for multi-rotor Unmanned Aerial Vehicles (UAVs) is proposed. The study is centered on an experimental platform designed to identify the dynamic behavior of the thruster which operates as main actuator in multi-rotor UAVs. The aim is to optimize the performance of the propulsion system with basis on its dynamic behavior. The dynamic of an UAV changes notably according to the performance of the thruster, which is composed by a propeller coupled to a Brushless Direct Current (BLDC) Motor. The dynamic response of the propulsion system is acquired from the experimental data, including the electric, mechanical and aerodynamic effects of the wing when the propeller is the load of the rotor. The experimental platform allows evaluating the performance of the system and determining the payload for a UAV, but also validates control laws to regulate the thruster action.
PERFORMANCE EVALUATION OF PROPELLER-ENGINE SYSTEMS FOR UNMANNED AERIAL VEHICLES IN HOVERING MODE (PDF Download Available). Available from: https://www.researchgate.net/publication/267094930_PERFORMANCE_EVALUATION_OF_PROPELLER-ENGINE_SYSTEMS_FOR_UNMANNED_AERIAL_VEHICLES_IN_HOVERING_MODE [accessed Jun 16, 2017].