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