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David Fernando Castillo Zúñiga
David Fernando Castillo Zúñiga
Researcher Aeronautical and Mechanical Engineering, Instituto Tecnológico de Aeronáutica
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Flight dynamics modeling of a flexible wing unmanned aerial vehicle
DFC Zúñiga, AG Souza, LCS Goes
Mechanical Systems and Signal Processing 145, 106900, 2020
132020
Aeroelastic vibration measurement based on laser and computer vision technique
HV De Figueiredo, DF Castillo-Zúñiga, NC Costa, O Saotome, ...
Experimental Techniques 45, 95-107, 2021
122021
Development of an Aeroelastic In-Flight Testing System for a Flexible Wing Unmanned Aerial Vehicle using Acceleration and Strain Sensors
DF Castillo Zuñiga, A Giacobini Souza, LCS Goes
AIAA Scitech 2019 Forum, 2019
62019
Parameter Identification for a Flexible Unmanned Aerial Vehicle Using Extended Kalman Filtering
AG Souza, DF Castillo Zuñiga, LS Goes, MS Sousa
XVIII International Symposium on Dynamic Problems of Mechanics, 2019
32019
Response and operational modal analysis from wind tunnel test of the EOLO flexible aircraft
DF Castillo Zuñiga, A Giacobini Souza, RG da Silva, LC Sandoval Góes
AIAA Scitech 2021 Forum, 1389, 2021
22021
Aeroelastic Analysis and Comparison with In-Flight Testing of Unmanned aerial Vehicles
DF Castillo Zúñiga
Master thesis (Flight Mechanics and Control)-Instituto Tecnologico de …, 2013
2*2013
Modal Testing of the Vector-P Unmanned Aerial Vehicle
DF Castillo Zúñiga, LCS Góes
Proccedings of the 7th Brazilian Congress of Mechanical Enginnering-CONEM2012, 2012
22012
ANÁLISIS AEROELASTICO DE FLUTTER EN ALAS DE AERONAVES BAJO REGIMEN SUBSONICO
DFC ZÚÑIGA
Universidad del Valle; DE CALI-COLOMBIA, SANTIAGO, 2009
2*2009
SISTEMA DE AQUISIÇÃO DE DADOS DE VOO DE UM VEÍCULO AÉREO NÃO TRIPULADO, VECTOR-P
C Fischer, LCS Góes, DFC Zuñiga
CONEM2016, 2016
12016
Impact Modal Analysis of UAV Vector-P's Wing Using LabVIEW
SM Pedreira, DFC Zuñiga, JF de Lima, WAF de Alencar, CA Martins
SAE Technical Paper, 2013
12013
Comments on System identification of an UAS model using a subspace method
RC Machado, DFC Zúniga, A Souza, V Paixão, T Rosado, JM Balthazar, ...
2024
Modelagem de um sistema massa-mola usando método de subespaços
RC Machado, PMSR Rizol, TM Souza, DFC Zúñiga, A Nabarrete, ...
Proceeding Series of the Brazilian Society of Computational and Applied …, 2023
2023
Aerodynamic Modeling of an Unmanned Aerial Vehicle using Vortex Lattice Method
DF Castillo-Zúñiga, RC Machado, LCS Góes
Proceeding Series of the Brazilian Society of Computational and Applied …, 2023
2023
In-flight modal identification by operational modal analysis
EM Cárdenas, DF Castillo-Zúñiga, LU Medina, LCS Góes
Journal of the Brazilian Society of Mechanical Sciences and Engineering 45 …, 2023
2023
OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM
RC Machado, DFC Zúniga, A de Souza, T Rosado, LCS Góes
33rd Congress of the International Council of the Aeronautical Sciences …, 2022
2022
RESPONSE AND OPERATIONAL MODAL ANALYSIS FROM WIND TUNNEL TEST OF THE EOLO FLEXIBLE AIRCRAFT
DFC Zúñiga, AG Souza, RGA da Silva, LCS Góes
2021
SYNTHETIC ESTIMATION OF ANGLE OF ATTACK AND SIDESLIP FOR FLIGHT TESTING OF AN UNMANNED AERIAL VEHICLE
AGP Sarmento, AG de Souza, DFC Zúñiga, LCS Góes
COBEM 2019, 2019
2019
Nonlinear Identification Using Polynomial NARMAX Model and a Stability Analysis of an Aeroelastic System
RCMG Barbosa, LCS Góes, A Nabarrete, JM Balthazar, DFC Zúñiga
Proceedings of DINAME 2017: Selected Papers of the XVII International …, 2019
2019
Nonlinear Identification Using Polynomial NARMAX Model and a Stability Analysis of an Aeroelastic
RCMG Barbosa, LCS Góes, A Nabarrete, JM Balthazar, DFC Zúñiga
Proceedings of DINAME 2017: Selected Papers of the XVII International …, 2018
2018
AEROELASTIC ANALYSIS AND COMPARISON WITH IN-FLIGHT TESTING OF THE VECTOR-P UNMANNED AERIAL VEHICLE
DFC Zúņiga, LS Góes, AG Marto, RGA da Silva
COBEM 2013, 2013
2013
El sistema no puede realizar la operación en estos momentos. Inténtalo de nuevo más tarde.
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