Parameter Identification for Application Within a Fault-Tolerant Flight Control System
Nonlinear Aircraft Model Identification and Validation for a Fault-Tolerant Flight Control System
Mobile Ground Control Station Development for Fault Tolerant UAV Research
Identification of Aerodynamic Parameters for a Small UAV from Flight Data
Curvature-Velocity-Orientation Method for UAV Collision Avoidance
Aircraft Attitude, Position, and Velocity Determination Using Sensor Fusion
AIAA-2004-6251 Formation Flight Test Results for UAV Research Aircraft Models
Advanced Research Integrated Avionics (ARIA) System for Fault-Tolerant Flight Research