Satellite Attitude Control Using Control Moment Gyroscopes von Portella, Kenedy Matiasso, Schinestzki, Wilcker Neuwald, Sehnem, Róger Mateus, Luz, Leonardo Barros da, Mantovani, Lorenzzo Quevedo, Sacco, Renan Rathis, Sartori, Tarso Kraemer Sarzi, Paglione, Pedro

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Formulation of the Flight Dynamics of Flexible Aircraft Using General Body Axes von Guimarães Neto, Antônio B, Silva, Roberto G. A, Paglione, Pedro, Silvestre, Flávio J

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Satellite Attitude Control Using Control Moment Gyroscopes von Kenedy Matiasso Portella, Wilcker Neuwald Schinestzki, Róger Mateus Sehnem, Leonardo Barros da Luz, Lorenzzo Quevedo Mantovani, Renan Rathis Sacco, Tarso Kraemer Sarzi Sartori, Pedro Paglione

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Optimal linear quadratic model following with an application to a flexible aircraft von da Silva, André Luís, Yoneyama, Takashi, Paglione, Pedro

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Longitudinal stability and control augmentation with robustness and handling qualities requirements using the two degree of freedom controller von Vargas, Francisco J. Triveno, de Oliveira Moreira, Fernando J., Paglione, Pedro

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Preliminary Attitude Control Studies for the ASTER Mission von Sarli, Bruno Victorino, da Silva, André Luís, Paglione, Pedro

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New Stochastic Algorithm for Design Optimization von de Sousa, Fabiano Luis, Ramos, Fernando Manuel, Paglione, Pedro, Girardi, Roberto M

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Stability of Equilibria for a Satellite Subject to Gravitational and Constant Torques von Sarychev, Vassili A, Paglione, Pedro, Guerman, Anna D

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Design of Robust Static Output Feedback Flight Control Law Using Structured Singular Value Optimization von Siqueira, Daniel, Moreira, Fernando J.O., Paglione, Pedro

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