All Stories

  1. MODELAGEM DE UM UAS (UNMANNED AERIAL SYSTEM) USANDO MÉTODOS DE SUBESPAÇOS
  2. In-flight modal identification by operational modal analysis
  3. Data Compatibility Check of an UAS With a Flexible Wing
  4. Response and Operational Modal Analysis from Wind Tunnel Test of the EOLO Flexible Aircraft
  5. Flight dynamics modeling of a flexible wing unmanned aerial vehicle
  6. Aeroelastic Vibration Measurement Based on Laser and Computer Vision Technique
  7. Development of an Aeroelastic In-Flight Testing System for a Flexible Wing Unmanned Aerial Vehicle using Acceleration and Strain Sensors
  8. Operational Modal Analysis using Impulsive Input of a Wing Flexible Unmanned Aerial Vehicle
  9. Parameter Identification for a Flexible Unmanned Aerial Vehicle Using Extended Kalman Filtering
  10. SYNTHETIC ESTIMATION OF ANGLE OF ATTACK AND SIDESLIP FOR FLIGHT TESTING OF AN UNMANNED AERIAL VEHICLE
  11. Nonlinear Identification Using Polynomial NARMAX Model and a Stability Analysis of an Aeroelastic System
  12. Influence and Suppression of Harmonic Components in Operational Modal Analysis of an Unmanned Aircraft Vehicle
  13. Identificação de parâmetro da dinâmica longitudinal de uma aeronave flexível usando o método de erro na saída.
  14. Modal Testing of a Flexible Wing UAV
  15. SISTEMA DE AQUISIÇÃO DE DADOS DE VOO DE UM VEÍCULO AÉREO NÃO TRIPULADO, VECTOR-P
  16. Impact Modal Analysis of UAV Vector-P's Wing Using LabVIEW