André Luís da Silva
Title
Cited by
Cited by
Year
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
172016
Conceptual Flexible Aircraft Model for Modeling, Analysis and Control Studies
AL da SILVA, P Paglione, T YONEYAMA
AIAA Atmospheric Flight Mechanics Conference, 2010
122010
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
72019
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
72018
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
72015
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
62007
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
52016
Nonlinear Optimal Model Following Control of Flexible Aircraft
AL da Silva
LAP Lambert Academic Publishing, 2012
52012
Nonlinear Optimum Model Following Control of Flexible Aircraft
AL da Silva
Instituto Tecnológico de Aeronáutica, 2010
52010
Preliminary attitude control studies for the aster mission
BV Sarli, AL Da Silva, P Paglione
Journal of Physics: Conference Series 465 (1), 012004, 2013
42013
CONTROLLABILITY ANALYSIS AND STABILIZATION OF FLEXIBLE AIRCRAFTS
AL da Silva, T Yoneyama, P Paglione
Congresso Brasileiro de Automática, 2010
42010
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
22016
Optimized Controller Design For CubeSat Attitude Tracking Control Using Magnetic Actuators
FSN Coelho, AL da Silva, JR Pinheiro
Proceedings Series of the 2nd IAA Latin American Cubesat Workshop, 2016
22016
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
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
22008
NanosatC-BR2 2 unit CubeSat power analysis solar flux prediction design and 3D printing of the flight model from the UFSM & INPE's NanosatC-BR CubeSat development program
LQ Mantovani, RP Marques, A Müller, EX Barreto, AL da Silva, ...
Proceedings of the 4th IAA Conference on University Satellite Missions and …, 2017
12017
Dinâmica e Controle do Voo de um VANT Quadrirrotor
L de Avellar Frederico, AL da Silva, L Martins-Filho
Proceeding Series of the Brazilian Society of Computational and Applied …, 2016
12016
Periodic control applied to attitude control of the SERPENS II mission
F Coelho, AL da Silva, JR Pinheiro
6th inernational conference on nonlinear science and complexity, Sao Jose …, 2016
12016
Navigation and control of an UAV quadrotor in search and surveillance missions
LA Frederico, LS Martins-Filho, AL Da Silva
Journal of Physics: Conference Series 641 (1), 012031, 2015
12015
Determination of an Attitude Estimation Unit with Inertial Sensors Modeled by Allan Variance
MM Carrasco, AL da Silva
IEEE Latin America Transactions 13 (8), 2500-2505, 2015
12015
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