All Stories

  1. Identification of a Flexible Fixed-Wing Aircraft Using Different Artificial Neural Network Structures

    Article • Aerospace, January 2026, MDPI AG

    Prof. Luiz Carlos Sandoval Goes

  2. The Influence of the Operational Altitude Variation on Flight Controller Design on Combat Aircraft Configuration

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Éder Moura, LEONARDO NEPOMUCENO, Prof. Luiz Carlos Sandoval Goes

  3. The Wing Swept Angle Influence on Longitudinal Dynamic Stability in a Combat Aircraft Configuration

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    LEONARDO NEPOMUCENO, Prof. Luiz Carlos Sandoval Goes, Éder Moura, Dr Adson A De Paula

  4. An Augmented Reality Visualization System for Simulated Multirotor Aerial Vehicles

    Article • Anais da Academia Brasileira de Ciências, January 2024, FapUNIFESP (SciELO)

    Prof. Luiz Carlos Sandoval Goes

  5. Optimization of the control of a subscale fighter aircraft.

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Luiz Carlos Sandoval Goes, LEONARDO NEPOMUCENO, Éder Moura

  6. Response and Operational Modal Analysis from Wind Tunnel Test of the EOLO Flexible Aircraft

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    David Fernando Castillo Zúñiga, Prof. Luiz Carlos Sandoval Goes

  7. Investigations on Complex Acoustic Modes of Rocket Engines Combustion Chambers for Damping Allocation

    Article • Journal of Aerospace Technology and Management, January 2021, FapUNIFESP (SciELO)

    Prof. Luiz Carlos Sandoval Goes

  8. Requirement derivation method for a legged robot with series-elastic actuators

    Article • November 2020, Comissao Especial de Informatica na Educacao

    Prof. Luiz Carlos Sandoval Goes

  9. Effects of Distributed Electric Propulsion on the Performance of a General Aviation Aircraft

    Article • August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Luiz Carlos Sandoval Goes

  10. Airship Aerodynamic Coefficients Estimation Based on Computational Method for Preliminary Design

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Mr Jonatas Santos, Prof. Luiz Carlos Sandoval Goes

  11. Sizing Methodology of Airship Fins Taking Into Account a Tethered Flight Condition

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Luiz Carlos Sandoval Goes, Mr Jonatas Santos

  12. Development of an Aeroelastic In-Flight Testing System for a Flexible Wing Unmanned Aerial Vehicle using Acceleration and Strain Sensors

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Luiz Carlos Sandoval Goes, David Fernando Castillo Zúñiga

  13. A Labview/Arduino Measurement System for Shape Memory Alloy Wires

    Article • November 2018, Institute of Electrical & Electronics Engineers (IEEE)

    Prof. Luiz Carlos Sandoval Goes

  14. Use of LMS Amesim® model and a bond graph support to predict behavior impacts of typical failures in an aircraft hydraulic brake system

    Article • Journal of the Brazilian Society of Mechanical Sciences and Engineering, August 2018, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  15. Nonlinear Identification Using Polynomial NARMAX Model and a Stability Analysis of an Aeroelastic System

    Article • July 2018, Springer Science + Business Media

    David Fernando Castillo Zúñiga, Prof. Luiz Carlos Sandoval Goes

  16. Formation control of multirotor aerial vehicles using decentralized MPC

    Article • Journal of the Brazilian Society of Mechanical Sciences and Engineering, May 2018, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  17. Selection And Definition Of Maneuvers For Parameter Identification Of An Unmanned Aerial Vehicle, Vector-P

    Article • IEEE Latin America Transactions, February 2018, Institute of Electrical & Electronics Engineers (IEEE)

    Prof. Luiz Carlos Sandoval Goes

  18. Antagonistic shape memory alloy wire as an actuator in a morphing wing

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Joran Driesen, Prof. Luiz Carlos Sandoval Goes

  19. Tethered Aerostat Stabilization in Turbulent Wind Using Actuated Fins

    Article • Journal of Guidance Control and Dynamics, December 2017, American Institute of Aeronautics and Astronautics (AIAA)

    José Azinheira, Prof. Luiz Carlos Sandoval Goes

  20. HSV and NDVI Color Space Analysis and Sampling Procedure for Counting of Seedlings in Eucalyptus spp Plantations from High Definition Aerial Images

    Article • December 2017, Institute of Electrical & Electronics Engineers (IEEE)

    Prof. Luiz Carlos Sandoval Goes

  21. Experimental measurement of parameters for modeling a differentia drive soccer robot

    Article • November 2017, Institute of Electrical & Electronics Engineers (IEEE)

    Prof. Luiz Carlos Sandoval Goes

  22. Deflection control of an aeroelastic system utilizing an antagonistic shape memory alloy actuator

    Article • Meccanica, October 2017, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  23. Attitude and vibration control of a satellite containing flexible solar arrays by using reaction wheels, and piezoelectric transducers as sensors and actuators

    Article • Acta Astronautica, October 2017, Elsevier

    Prof. Luiz Carlos Sandoval Goes

  24. Attitude dynamics and control of a spacecraft like a robotic manipulator when implementing on-orbit servicing

    Article • Acta Astronautica, August 2017, Elsevier

    Prof. Luiz Carlos Sandoval Goes

  25. Development of Flight Mode Algorithms for Tethered Airships

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Mr Jonatas Santos, DR. Konstantin Kondak, Prof. Luiz Carlos Sandoval Goes

  26. System Identification Approach for a Tethered Airship

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Mr Jonatas Santos, DR. Konstantin Kondak, Prof. Luiz Carlos Sandoval Goes

  27. Distributed Formation Flight Control of Multirotor Helicopters

    Article • Journal of Control Automation and Electrical Systems, April 2017, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  28. A reduced order state space model for aeroelastic analysis in time domain

    Article • Journal of Fluids and Structures, February 2017, Elsevier

    Prof. Luiz Carlos Sandoval Goes

  29. Virtual Environment With AMESim and its Integration With MATLAB-Simulink

    Article • October 2016, ASME International

    Prof. Luiz Carlos Sandoval Goes

  30. Stojan

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Mr Jonatas Santos, DR. Konstantin Kondak, Prof. Luiz Carlos Sandoval Goes

  31. Vibration-based damage detection for a composite helicopter main rotor blade

    Article • Case Studies in Mechanical Systems and Signal Processing, June 2016, Elsevier

    Prof. Luiz Carlos Sandoval Goes

  32. Comparison of in-Flight Measured and Computed Aeroelastic Damping: Modal Identification Procedures and Modeling Approaches

    Article • Journal of Aerospace Technology and Management, May 2016, FapUNIFESP (SciELO)

    Prof. Luiz Carlos Sandoval Goes

  33. Model Based System Testing: Bringing Testing and Simulation Close Together

    Article • January 2016, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  34. Strain-Based Experimental Modal Analysis on Planar Structures: Concepts and Practical Aspects

    Article • January 2016, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  35. An adaptive piezoelectric vibration absorber enhanced by a negative capacitance applied to a shell structure

    Article • Smart Materials and Structures, November 2015, Institute of Physics Publishing

    Prof. Luiz Carlos Sandoval Goes

  36. Analysis of the acoustical behavior of cavities using impedance functions

    Article • Journal of the Brazilian Society of Mechanical Sciences and Engineering, September 2015, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  37. The use of strain gauges in vibration-based damage detection

    Article • Journal of Physics Conference Series, July 2015, Institute of Physics Publishing

    Prof. Luiz Carlos Sandoval Goes

  38. Modeling and Control of Tethered Unmanned Multicopters in Hovering Flight

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Mr Jonatas Santos, Prof. Luiz Carlos Sandoval Goes

  39. Autonomous Airship

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Mr Jonatas Santos, Prof. Luiz Carlos Sandoval Goes

  40. Formation flight control of multirotor helicopters with collision avoidance

    Article • June 2015, Institute of Electrical & Electronics Engineers (IEEE)

    Prof. Luiz Carlos Sandoval Goes

  41. Flutter analysis including structural uncertainties

    Article • Meccanica, March 2015, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  42. Trajectory Tracking Control of an Aerial Robot with Obstacle Avoidance

    Article • IFAC-PapersOnLine, January 2015, Elsevier

    Prof. Luiz Carlos Sandoval Goes

  43. The Use of Fiber Bragg Grating Sensors for Strain Modal Analysis

    Article • January 2015, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  44. Aeroelastic stability analysis considering a continuous flight envelope

    Article • Journal of Fluids and Structures, August 2014, Elsevier

    Prof. Luiz Carlos Sandoval Goes

  45. Control of Limit Cycle Oscillation in a Three Degrees of Freedom Airfoil Section Using Fuzzy Takagi-Sugeno Modeling

    Article • Shock and Vibration, January 2014, Wiley

    Prof. Luiz Carlos Sandoval Goes

  46. Multiphysics NVH Modeling: Simulation of a Switched Reluctance Motor for an Electric Vehicle

    Article • IEEE Industrial Electronics Magazine, January 2014, Institute of Electrical & Electronics Engineers (IEEE)

    Prof. Luiz Carlos Sandoval Goes

  47. Strain-Based Dynamic Measurements and Modal Testing

    Article • January 2014, Springer Science + Business Media

    Prof. Luiz Carlos Sandoval Goes

  48. Modal Strain Energy Based Damage Detection Applied to a Full Scale Composite Helicopter Blade

    Article • Key Engineering Materials, July 2013, Trans Tech Publications

    Prof. Luiz Carlos Sandoval Goes

  49. An integrated hybrid methodology of time series forecast and case-based reasoning for fault prognosis

    Article • June 2013, Institute of Electrical & Electronics Engineers (IEEE)

    Prof. Luiz Carlos Sandoval Goes

  50. Modal-Based Damage Detection of a Composite Helicopter Main Rotor Blade

    Article • April 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Luiz Carlos Sandoval Goes

  51. The Use of Gramian Matrices for Aeroelastic Stability Analysis

    Article • Mathematical Problems in Engineering, January 2013, Wiley

    Prof. Luiz Carlos Sandoval Goes

  52. Cabin Temperature Control Model for Commercial Aircraft

    Article • August 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Luiz Carlos Sandoval Goes

  53. Notes on vibration control of a micro/macromanipulator mounted on a flexible structure

    Article • Proceedings of the Institution of Mechanical Engineers Part K Journal of Multi-body Dynamics, October 2011, SAGE Publications

    Prof. Luiz Carlos Sandoval Goes

  54. Multivariable Control of Aeronautical Air Conditioning System Based on Thermal Comfort

    Article • October 2011, SAE International

    Prof. Luiz Carlos Sandoval Goes

  55. SOME REMARKS ON BIFURCATION ANALYSIS OF A NONLINEAR VIBRATING SYSTEM EXCITED BY A SHAPE MEMORY ALLOY MATERIAL (SMA)

    Article • International Journal of Bifurcation and Chaos, October 2011, World Scientific Pub Co Pte Lt

    Prof. Luiz Carlos Sandoval Goes

  56. Operating a Network of Balloons Instead of Satellites

    Article • June 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Luiz Carlos Sandoval Goes

  57. A note on the attenuation of the sommerfeld effect of a non-ideal system taking into account a MR damper and the complete model of a DC motor

    Article • Journal of Vibration and Control, November 2010, SAGE Publications

    Prof. Luiz Carlos Sandoval Goes

  58. Landing Gear Free-Fall Simulation and Kinetic Energy Optimization

    Article • October 2010, SAE International

    Prof. Luiz Carlos Sandoval Goes

  59. Accumulative Learning using Multiple ANN for Flexible Link Control

    Article • IEEE Transactions on Aerospace and Electronic Systems, April 2010, Institute of Electrical & Electronics Engineers (IEEE)

    Prof. Luiz Carlos Sandoval Goes

  60. Liquid rocket combustion chamber acoustic characterization

    Article • Journal of Aerospace Technology and Management, January 2010, FapUNIFESP (SciELO)

    Prof. Luiz Carlos Sandoval Goes

  61. Aircraft Parameter Estimation Experiment Design Considering Measurement Colored Residuals

    Article • Journal of Aircraft, November 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Luiz Carlos Sandoval Goes

  62. An Investigations on Local and Global Behavior of a (SMA) Oscillator of 3-DOF Driven by a Limited Power Supply

    Article • January 2009, ASME International

    Prof. Luiz Carlos Sandoval Goes

  63. Aircraft longitudinal stability and control derivatives identification by using life cycle and Levenberg–Marquardt optimization algorithms

    Article • Inverse Problems in Science and Engineering, November 2008, Taylor & Francis

    Prof. Luiz Carlos Sandoval Goes

  64. In-flight Output Only Modal Analysis of Aircraft Structural Dynamics

    Article • March 2008, SAE International

    Prof. Luiz Carlos Sandoval Goes

  65. Adaptive Stochastic Filtering for Online Aircraft Flight Path Reconstruction

    Article • Journal of Aircraft, September 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Luiz Carlos Sandoval Goes

  66. Aircraft parameter estimation using output-error methods

    Article • Inverse Problems in Science and Engineering, September 2006, Taylor & Francis

    Prof. Luiz Carlos Sandoval Goes

  67. Flight Tests Telemetry Link for Small and Medium Aircrafts

    Article • November 2005, SAE International

    Prof. Luiz Carlos Sandoval Goes

  68. Design of an Active Feel System for a Flight Simulator

    Article • December 2000, SAE International

    Prof. Luiz Carlos Sandoval Goes

  69. Dynamic Modeling and Experimental Identification of Flexible Structure Mounted Manipulator System

    Article • February 2000, American Society of Civil Engineers (ASCE)

    Prof. Luiz Carlos Sandoval Goes

  70. Dynamic Modeling And Experimental Identification Of An Electric-Hydraulic Pressure Control Valve

    Article • October 1993, SAE International

    Prof. Luiz Carlos Sandoval Goes

  71. Feedback-error-learning for controlling a flexible link

    Article • Institute of Electrical & Electronics Engineers (IEEE)

    Prof. Luiz Carlos Sandoval Goes