All Stories

  1. An Evaluation of Fault-Tolerant Control Allocation Strategies for eVTOL Aircraft
  2. Baseball Avoidance Multirotor Simulation
  3. Aircraft System Identification Approach for Control Surface Fault Diagnosis
  4. Summary of the Second AIAA Stability and Control Prediction Workshop
  5. System Identification for a Subscale Tiltrotor eVTOL Aircraft from Hover Flight-Test Data
  6. Aero-Propulsive Damping Characterization for eVTOL Aircraft Using Free Motion Wind-Tunnel Testing
  7. Transition Aero-Propulsive Analysis of a Tilt-Wing eVTOL Aircraft Using a Surface-Vorticity Solver
  8. Development and Capabilities of the NASA Flight Dynamics Research Facility
  9. Statistical Wind-Tunnel Experimentation Advancements for eVTOL Aircraft Aero-Propulsive Model Development
  10. Experimental Characterization of an Electric Ducted Fan for the SUSAN 25% Scale Research Vehicle
  11. Development and Evaluation of Multirotor Flight Dynamic Models for Estimation and Control
  12. System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data
  13. Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data
  14. Aero-Propulsive Modeling for eVTOL Aircraft Using Wind Tunnel Testing with Multisine Inputs
  15. Efficient Variable-Pitch Propeller Aerodynamic Model Development for Vectored-Thrust eVTOL Aircraft
  16. Aero-Propulsive Modeling for Tilt-Wing, Distributed Propulsion Aircraft Using Wind Tunnel Data
  17. System Identification for Propellers at High Incidence Angles
  18. Rapid Aero Modeling for Urban Air Mobility Aircraft in Wind-Tunnel Tests
  19. Wind Tunnel-Based Aerodynamic Model Identification for a Tilt-Wing, Distributed Electric Propulsion Aircraft
  20. System Identification for Propellers at High Incidence Angles
  21. Wind Tunnel Testing Techniques for a Tandem Tilt-Wing, Distributed Electric Propulsion VTOL Aircraft
  22. Rapid Aero Modeling for Urban Air Mobility Aircraft in Computational Experiments
  23. Intelligent Contingency Management for Urban Air Mobility
  24. Nonlinear Model Identification Methodology for Small, Fixed-Wing, Unmanned Aircraft