R. Monti

发表

Semi-Analytical Orbital Parameters Description for Thermal Fatigue Analysis

P. Gasbarri, R. Monti, 2016 .

Vibration control of a flexible space manipulator during on orbit operations

Giovanni B. Palmerini, Paolo Gasbarri, Marco Sabatini, 2012 .

A HYBRID TWO-LEVEL APPROACH USED IN THE OPTIMIZATIONA OF AN AERONAUTICAL COMPOSITE STRUCTURE

Paolo Gasbarri, Leonardo D. Chiwiacowsky, Arthur Tórgo Gómez, 2014 .

A two-level procedure based on genetic algorithms to optimize an aeronautical composite structure

Paolo Gasbarri, Haroldo F. de Campos Velho, Leonardo D. Chiwiacowsky, 2012, SAC '12.

Very large space structures: Non-linear control and robustness to structural uncertainties

Paolo Gasbarri, Marco Sabatini, Riccardo Monti, 2014 .

Effects of uncertainties and flexible dynamic contributions on the control of a spacecraft full-coupled model

Paolo Gasbarri, Marco Sabatini, Riccardo Monti, 2014 .

Control-oriented modelization of a satellite with large flexible appendages and use of worst-case analysis to verify robustness to model uncertainties of attitude control☆

Paolo Gasbarri, Riccardo Monti, Chiara Toglia, 2012 .

A Hybrid FEM-Continuous Approach for Modelling Large Space Structures for Attitude Control Synthesis

P. Gasbarri, R. Monti, 2012 .

Optimisation and thermal control of a multi-layered structure for space electronic devices and thermal shielding of re-entry vehicles

Leonardo D. Chiwiacowsky, Paolo Gasbarri, Renato Barboni, 2012 .