| Fuzzy adaptive extended Kalman filter for UAV INS/GPS data fusion AL da Silva, JJ da Cruz Journal of the Brazilian Society of Mechanical Sciences and Engineering 38 …, 2016 | 31 | 2016 |
| The nanosatc-br, cubesat development program–A joint cubesat program developed by ufsm and inpe/mctic–Space geophysics mission payloads and first results NJ Schuch, OSC Durão, MR da Silva, F Mattiello-Francisco, JBS Martins, ... Brazilian Journal of Geophysics 37 (1), 95-103, 2019 | 13 | 2019 |
| Conceptual Flexible Aircraft Model for Modeling, Analysis and Control Studies AL da SILVA, P Paglione, T YONEYAMA AIAA Atmospheric Flight Mechanics Conference, 2010 | 13 | 2010 |
| Attitude control system proposed for SERPENS-2 space mission AGV de Brum, L Baroni, AL da Silva, FSN Coelho, ES Ferreira, ... Computational and Applied Mathematics 37 (4), 4743-4756, 2018 | 11 | 2018 |
| COBEM-2017-2703 MODELLING, SIMULATION AND CONTROL OF FIXED-WING UNMANNED AERIAL VEHICLE (UAV) WR Silva, AL da Silva, HA Gründling | 11* | |
| Sliding mode attitude control using thrusters and pulse modulation for the ASTER mission BV Sarli, AL da Silva, P Paglione Computational and Applied Mathematics 34 (2), 535-556, 2015 | 10 | 2015 |
| Nonlinear Optimum Model Following Control of Flexible Aircraft AL da Silva Instituto Tecnológico de Aeronáutica, 2010 | 8 | 2010 |
| Attitude Determination for Low Cost IMU and Processor Board using the Methods of TRIAD, Kalman Filter and Allan Variance MM Carrasco, AL da Silva REVISTA BRASILEIRA DE INICIAÇÃO CIENTÍFICA 3 (2), 2016 | 6 | 2016 |
| PROCEDIMENTO DE PROJETO DE LEIS DE CONTROLE DE VOO DE AERONAVES UTILIZANDO O CONTROLE A ESTRUTURA VARIÁVEL AL da Silva Instituto Tecnológico de Aeronáutica, 2007 | 6 | 2007 |
| Sistema de Controle de Atitude Proposto para a Missão Espacial SERPENS II AV de Brum, L Baroni, AL da Silva, CF de Melo, E dos Santos Ferreira, ... Proceeding Series of the Brazilian Society of Computational and Applied …, 2016 | 4 | 2016 |
| Preliminary attitude control studies for the aster mission BV Sarli, AL Da Silva, P Paglione Journal of Physics: Conference Series 465 (1), 012004, 2013 | 4 | 2013 |
| CONTROLLABILITY ANALYSIS AND STABILIZATION OF FLEXIBLE AIRCRAFTS AL da Silva, T Yoneyama, P Paglione Congresso Brasileiro de Automática, 2010 | 4 | 2010 |
| Optimized Controller Design For CubeSat Attitude Tracking Control Using Magnetic Actuators FSN Coelho, AL da Silva, JR Pinheiro 2nd IAA Latin American Cubesat Workshop, 2016 | 3 | 2016 |
| The Present & Future of the Brazilian INPE-UFSM NANOSATC-BR, CubeSats Development Program NJ Schuch, RP Marques, OSC Durão, MR da Silva, O Mendes, ... Annales Geophysicae Discussions, 1-16, 2019 | 2 | 2019 |
| Optimal linear quadratic model following with an application to a flexible aircraft AL da Silva, T Yoneyama, P Paglione Journal of Vibration and Control 20 (12), 1796-1815, 2014 | 2 | 2014 |
| Cruising Autopilot for a Flexible Aircraft with Internal Loop of Model Following AL da Silva, P Paglione, T Yoneyama Journal of Aerospace Engineering 27 (2), 202-214, 2012 | 2* | 2012 |
| Flight Mechanics Model of Flexible Aircraft AL da Silva | 2 | 2010 |
| A PROCEDURE TO DESIGN AIRCRAFT FLIGHT CONTROL LAWS TAKING INTO ACCOUNT ROBUSTNESS USING THE VARIABLE STRUCTURE CONTROL AL da Silva, FJT Vargas, P Paglione 26th Congress of the International Council of the Aeronautical Sciences, 2008 | 2 | 2008 |
| Preliminary Study of Launch and Orbit of a CubeSat Using a Modified VSB-30 Launcher Vehicle AG Slongo, AL da Silva, DD Moraes, JF de Araújo Martos, LQ Mantovani, ... Journal of Aerospace Technology and Management 12, 2020 | 1 | 2020 |
| Sizing of anti-lock braking system for Formula SAE vehicles LD Boere, AL da Silva SAE Technical Paper, 2018 | 1 | 2018 |
Fátima Mattiello-FranciscoTecnologista Senior INPE在 inpe.br 的电子邮件经过验证
