| 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 | 44 | 2017 |
| Far and proximity maneuvers of a constellation of service satellites and autonomous pose estimation of customer satellite using machine vision G Arantes Jr, EM Rocco, IM da Fonseca, S Theil Acta Astronautica 66 (9-10), 1493-1505, 2010 | 36 | 2010 |
| 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, ÉJ de Oliveira Acta Astronautica 137, 490-497, 2017 | 29 | 2017 |
| A machine learning strategy for optimal path planning of space robotic manipulator in on-orbit servicing RR Santos, DA Rade, IM da Fonseca Acta Astronautica 191, 41-54, 2022 | 27 | 2022 |
| Structural control interaction for an LSS attitude control system using thrusters and reaction wheels IM Da Fonseca, PM Bainum, AR Da Silva Acta Astronautica 60 (10-11), 865-872, 2007 | 27 | 2007 |
| Integrated structural and control optimization IM Fonseca, PM Bainum Journal of Vibration and Control 10 (10), 1377-1391, 2004 | 18 | 2004 |
| Structural and control optimization of a space structure subjected to the gravity-gradient torque IM Fonseca, PM Bainum, PTM Lourenção Acta Astronautica 51 (10), 673-681, 2002 | 15 | 2002 |
| Inertial measurement unit calibration procedure for a redundant tetrahedral gyro configuration with wavelet denoising ÉJ Oliveira, WC Leite Filho, IM Fonseca Journal of Aerospace Technology and Management 4 (2), 163-168, 2012 | 14 | 2012 |
| SACI-2 attitude control subsystem IM Fonseca, MC Santos INPE 3, 197-209, 2002 | 13 | 2002 |
| Fault Detection and Isolation in Inertial Measurement Units Based on χ2‐CUSUM and Wavelet Packet ÉJ de Oliveira, I Milagre da Fonseca, H Koiti Kuga Mathematical Problems in Engineering 2013 (1), 869293, 2013 | 12 | 2013 |
| CSI due to sloshing motion on LEO LSS IM Da Fonseca, PM Bainum Advances in the Astronautical Sciences 145, 1073-1086, 2012 | 11 | 2012 |
| Large space structure integrated structural and control optimization, using analytical sensitivity analysis IM Fonseca, PM Bainum Journal of Guidance, Control, and Dynamics 24 (5), 978-982, 2001 | 8 | 2001 |
| The Brazilian scientific microsatellite SACI-1 J Neri, WA Dos Santos, S Rabay, IM Fonseca, PN De Souza, ... Acta Astronautica 39 (9-12), 707-709, 1996 | 8 | 1996 |
| SACI-1-A COST-EFFECTIVE MICROSATELLITE BUS FOR MULTIPLE MISSION PAYLOADS J Neri, WA Dos Santos, S Rabay, PN De Souza, OB Oliveira Filho, ... International Conference on Small Satellites: Missions and Technology 9 (13), 1996 | 8 | 1996 |
| Simultaneous structural and control optimization of large space structures IM Fonseca, PM Bainum | 8 | 1995 |
| The Brazilian Satellite Program-A Survey IM Fonseca, PM Bainum Advances in the Astronautical Sciences 122, 505-531, 2006 | 7 | 2006 |
| Modelagem do Movimento Rotacional de um Corpo Rígido Dotado de Um Amortecedor de Nutação Anular Viscoso e Sua Validação Experimental IM Fonseca, PN de Souza Soc. Mech. Sc 12 (1), 89-111, 1990 | 7 | 1990 |
| NanosatC-Br–The First Brazilian Cubesat LL Costa, SL Prochnow, RL Costa, ECD Favera, CE Antunes, NJ Schuch, ... 59th. IAC, Intl. Astronautical Federation, 2008 | 6 | 2008 |
| The Attitude Control Subsystem of the Brazilian Scientific Satellite-SACI-1 IM Fonseca, PN Souza, J Neri, UTV Guedes ICONE’96 Second International Conference on Non-Linear Dynamics, Chaos …, 1996 | 6 | 1996 |
| FDIR for the IMU Component of AOCS Systems MN Pontuschka, IM da Fonseca Mathematical Problems in Engineering 2014 (1), 302716, 2014 | 5 | 2014 |
Élcio Jeronimo de OliveiraIAA - International Academy of Astronautics在 fab.mil.br 的电子邮件经过验证
