Use of LMS Amesim® model and a bond graph support to predict behavior impacts of typical failures in an aircraft hydraulic brake system von Maia Neto, Mário, Góes, Luiz Carlos Sandoval

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Control of Limit Cycle Oscillation in a Three Degrees of Freedom Airfoil Section Using Fuzzy Takagi-Sugeno Modeling von Bueno, Douglas Domingues, Gonçalves, Paulo José Paupitz, Sandoval Góes, Luiz Carlos

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Modal Strain Energy Based Damage Detection Applied to a Full Scale Composite Helicopter Blade von dos Santos, Fabio Luis Marques, van der Auweraer, Herman, Peeters, Bart, Sandoval Góes, Luiz Carlos

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Investigations on Complex Acoustic Modes of Rocket Engines Combustion Chambers for Damping Allocation von Guimarães, Gustavo Paulinelli, Pirk, Rogerio, Souto, Carlos D’Andrade, Góes, Luiz Carlos Sandoval

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Formation control of multirotor aerial vehicles using decentralized MPC von Viana, Ícaro Bezerra, dos Santos, Davi Antônio, Góes, Luiz Carlos Sandoval

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Adaptive Stochastic Filtering for Online Aircraft Flight Path Reconstruction von De Mendonça, Celso Braga, Hemerly, Elder Moreira, Góes, Luiz Carlos Sandoval

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Analysis of the acoustical behavior of cavities using impedance functions von Guimarães, Gustavo Paulinelli, Pirk, Rogério, Souto, Carlos D’Andrade, Góes, Luiz Carlos Sandoval

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System identification in time domain of flexible aircraft using panel methods von Paula, Thiago Rosado de, Sarmento, Andrew Gomes Pereira, Fernandes, Vitor Paixão, Fisher, Clécio, Machado, Raphaela Carvalho, Silva, Roberto Gil Annes da, Sandoval Góes, Luiz Carlos

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Results of Short-Period Helicopter System Identification Using Output-Error and Hybrid Search-Gradient Optimization Algorithm von Cruz, Ronaldo Vieira, Sandoval Góes, Luiz Carlos

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Aeroelastic stability analysis considering a continuous flight envelope von Bueno, Douglas Domingues, José Paupitz Gonçalves, Paulo, Carlos Sandoval Góes, Luiz

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Distributed Formation Flight Control of Multirotor Helicopters von Viana, Ícaro Bezerra, Santos, Davi Antônio dos, Góes, Luiz Carlos Sandoval, Prado, Igor Afonso Acampora

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The Use of Gramian Matrices for Aeroelastic Stability Analysis von Gonçalves, Paulo José Paupitz, Sandoval Góes, Luiz Carlos, Marqui, Clayton Rodrigo, Bueno, Douglas Domingues

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The use of strain gauges in vibration-based damage detection von Marques dos Santos, Fabio Luis, Peeters, Bart, Lau, Jenny, Desmet, Wim, Goes, Luiz Carlos Sandoval

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Flight Path Reconstruction and Parameter Estimation Using Output‐Error Method von de Oliveira Maciel, Benedito Carlos, Sandoval Góes, Luiz Carlos, Hemerly, Elder Moreira, Brasil Neto, Nei Salis

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Liquid rocket combustion chamber acoustic characterization von Pirk, Rogério, Souto, Carlos d'Andrade, Silveira, Dimas Donizeti da, Souza, Cândido Magno de, Góes, Luiz Carlos Sandoval

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Selection And Definition Of Maneuvers For Parameter Identification Of An Unmanned Aerial Vehicle, Vector-P von Fischer, Clecio, Nepomuceno, Leonardo Murilo, Goes, Luiz Carlos Sandoval

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Investigations on Complex Acoustic Modes of Rocket Engines Combustion Chambers for Damping Allocation von Gustavo Paulinelli Guimarães, Rogério Pirk, Carlos D'Andrade Souto, Luiz Carlos Sandoval Góes

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Results of Short-Period Helicopter System Identification Using Output-Error and Hybrid Search-Gradient Optimization Algorithm von Cruz, Ronaldo Vieira, Sandoval Góes, Luiz Carlos

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Aircraft Parameter Estimation Experiment Design Considering Measurement Colored Residuals von Neto, Nei Salis Brasil, Hemerly, Elder Moreira, Góes, Luiz Carlos Sandoval

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Prediction of transients and control reactions in a transonic wind tunnel von Falcão Filho, João Batista Pessoa, Ortega, Marcos Aurélio, Góes, Luiz Carlos Sandoval

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