Luiz Carlos Sandoval Goes
Cited by
Cited by
Multiphysics NVH modeling: Simulation of a switched reluctance motor for an electric vehicle
FLM Dos Santos, J Anthonis, F Naclerio, JJC Gyselinck, ...
IEEE Transactions on Industrial Electronics 61 (1), 469-476, 2013
Vibro-acoustic analysis of the Brazilian vehicle satellite launcher (VLS) fairing
R Pirk, W Desmet, B Pluymers, P Sas, LCS Goes
Proceedings of the International Conference on Noise and Vibrationá…, 2002
Vibration-based damage detection for a composite helicopter main rotor blade
FLM Dos Santos, B Peeters, H Van Der Auweraer, LCS Gˇes, W Desmet
Case Studies in Mechanical Systems and Signal Processing 3, 22-27, 2016
Adaptive stochastic filtering for online aircraft flight path reconstruction
CB De Mendonša, EM Hemerly, LCS Gˇes
Journal of aircraft 44 (5), 1546-1558, 2007
Attitude dynamics and control of a spacecraft like a robotic manipulator when implementing on-orbit servicing
IM Da Fonseca, LCS Goes, N Seito, MK da Silva Duarte, ╔J de Oliveira
Acta Astronautica 137, 490-497, 2017
An adaptive piezoelectric vibration absorber enhanced by a negative capacitance applied to a shell structure
JAB Gripp, LCS Goes, O Heuss, F Scinocca
Smart Materials and Structures 24 (12), 125017, 2015
Cabin temperature control model for commercial aircraft
R Romani, LC de Gˇes
AIAA Modeling and Simulation Technologies Conference, 4637, 2012
Liquid rocket combustion chamber acoustic characterization
R Pirk, CA Souto, DD Silveira, CM Souza, LCS Gˇes
Journal of Aerospace Technology and Management 2 (3), 269-278, 2010
Aircraft parameter estimation using output-error methods
LCS Gˇes, EM Hemerly, BCO Maciel, WR Neto, CB Mendonca, J Hoff
Inverse problems in science and engineering 14 (6), 651-664, 2006
Comparison of in-flight measured and computed aeroelastic damping: modal identification procedures and modeling approaches
RC Follador, CE Souza, AG Marto, RGA Silva, LCS Gˇes
Journal of Aerospace Technology and Management 8 (2), 163-177, 2016
Investigation of oscillatory combustion processes in actively controlled liquid fuel combustor
F Kappei, J Lee, C Johnson, E Lubarsky, Y Neumeier, B Zinn
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 3348, 2000
Attitude and vibration control of a satellite containing flexible solar arrays by using reaction wheels, and piezoelectric transducers as sensors and actuators
IM da Fonseca, DA Rade, LCS Goes, T de Paula Sales
Acta Astronautica 139, 357-366, 2017
Modeling and robust analysis of a liquid rocket engine
A Santana, Jr, F Barbosa, M Niwa, L Goes
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 3160, 2000
Prediction of transients and control reactions in a transonic wind tunnel
JBP FalcŃo Filho, MA Ortega, LCS Gˇes
Journal of the Brazilian Society of Mechanical Sciences 22 (2), 317-339, 2000
The use of strain gauges in vibration-based damage detection
FLM dos Santos, B Peeters, J Lau, W Desmet, LCS Goes
Journal of Physics: Conference Series 628 (1), 012119, 2015
Accumulative learning using multiple ANN for flexible link control
ADA Neto, LCS Goes, CL Nascimento
IEEE Transactions on Aerospace and Electronic Systems 46 (2), 508-524, 2010
Dynamic modelling nonlinear and control system for a turboshaft
FAC Burlamaqui Filho, LCS Goes, ABV Oliveira, RW Bosa, GS Fernandes
12th Pan-American Congress of Applied Mechanics, Port of Spain, Trinidad, 2012
Aircraft longitudinal stability and control derivatives identification by using life cycle and Levenberg–Marquardt optimization algorithms
FA Chegury Viana, BCO Maciel, NSB Neto, MF Oliveira, V Steffen Jr, ...
Inverse Problems in Science and Engineering 17 (1), 17-34, 2009
Control of limit cycle oscillation in a three degrees of freedom airfoil section using fuzzy Takagi-Sugeno modeling
DD Bueno, LC Sandoval Goes, PJP Gonšalves
Shock and Vibration 2014, 2014
Results of short-period helicopter system identification using output-error and hybrid search-gradient optimization algorithm
RV Cruz, LC Sandoval Gˇes
Mathematical Problems in Engineering 2010, 2010
The system can't perform the operation now. Try again later.
Articles 1–20