Fusion of GPS and Redundant IMU Data for Attitude Estimation
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
2011-6332 On-line Modeling and Calibration of Low-Cost Navigation Sensors
2011-6333 Development of a GPS/INS Sensor Fusion Simulation Environment Using Flight Data
Advanced Research Integrated Avionics (ARIA) System for Fault-Tolerant Flight Research