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Ronaldo Cruz
Ronaldo Cruz
Professor do Departamento de Projetos, ITA
Verifierad e-postadress på ita.br
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Results of short-period helicopter system identification using output-error and hybrid search-gradient optimization algorithm
RV Cruz, LC Sandoval Góes
Mathematical Problems in Engineering 2010, 2010
102010
Desenvolvimento de um modelo dinâmico para simuladores de helicópteros.
RV Cruz
72009
Results of longitudinal helicopter system identification using output-error and both genetic and Levenberg-Marquardt optimization algorithm
RV Cruz, LCS Góes
Proceedings of the 19th Brazilian Congress of Mechanical Engineering, 2007
62007
Results of lateral-directional helicopter system identification using output-error and both genetic and levenberg-marquardt optimization algorithms
RV Cruz, LCS Góes, D de Andrade
Brazilian Symposium on Aerospace Eng. & Applications, by Agência …, 2009
42009
Preliminary results of longitudinal helicopter system identification using genetic optimization algorithm
RV Cruz, NSB Neto, LCS Góes
Proceedings of the 5th Brazilian Conference on Dynamics, Control and their …, 2006
42006
MPCA for flight dynamics parameters determination
IY Sumida, HF de Campos Velho, EFP Luz, RV Cruz, LCS Góes
Computer Assisted Methods in Engineering and Science 21 (3–4), 257-265, 2017
32017
The influence of the positive pitch-flap coupling (negative δ3) on the flapping response of an articulated tail rotor
JMP Figueira, RV Cruz, D de Andrade
9th Brazilian Conference on Dynamics, Control and their Applications, DINCON 10, 2010
12010
Estabilidade em" flutter" de pás de rotores de helicópteros em vôo pairado-um estudo de caso.
RV Cruz
12002
Development of New Flight Test Techniques for Helicopter Air to Air Refueling Qualification Process
LGL de Paula, AC de Freitas, JMP Figueira, RG da Silva, RV Cruz
AIAA SCITECH 2022 Forum, 0198, 2022
2022
Helicopter stability and control derivatives identification in different flight conditions
LL Menegaldo, SS de Oliveira, RV Cruz
Journal of the Brazilian Society of Mechanical Sciences and Engineering 42, 1-12, 2020
2020
Full calibration for helicopter simulator
IY Sumida, HF Campos Velho, EFP Luz, RV Cruz, LCS Góes
Euro GNC, 2015
2015
Flight dynamics parameter estimation of a rotary wing aircraft using theoutput error minimization with natural and meta heuristic methods
IY Sumida, HF Campos Velho, EFP Luz, RV Cruz, LCS Goés
Pan-American Congress on Computational Mechanics, 1 (PANACM), 2015
2015
STABILITY IN FLUTTER OF HOVERING HELICOPTER BLADE
RV Cruz, D de Andrade
Application of Machine Learning and Multi-Disciplinary/Multi-Objective Optimization Techniques for Conceptual Aircraft Design
BS de Mattos, FA Bortolete, JATG Fregnani, AB Jorge, WM Alves, ...
FLIGHT DYNAMICS PARAMETER ESTIMATION OF A ROTARY WING AIRCRAFT USING THE OUTPUT ERROR MINIMIZATION WITH NATURAL AND META HEURISTIC METHODS
IY Sumida, HF de Campos Velho, EFP Luz, RV Cruz, L Carlos, S Góes
Iterative Estimation for Flight Dynamic Helicopter Simulator
IY Sumida, HF de Campos Velho, EFP da Luz, RV Cruz, L Carlos, S Góes
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Artiklar 1–16