Parameter Identification for Application Within a Fault-Tolerant Flight Control System
Nonlinear Aircraft Model Identification and Validation for a Fault-Tolerant Flight Control System
Identification of Aerodynamic Parameters for a Small UAV from Flight Data
Aerodynamic and Thrust Force Modeling for a Propulsion Assisted Control Aircraft Test Bed
Aerodynamic and Thrust Force Modeling for a Propulsion Assisted Control Aircraft Test Bed
Advanced Research Integrated Avionics (ARIA) System for Fault-Tolerant Flight Research