UAV Attitude, Heading, and Wind Estimation Using GPS/INS and an Air Data System (AIAA 2013-5201)
Sensitivity Analysis of EKF and UKF in GPS/INS Sensor Fusion
Relaxation of Initial Error and Noise Bounds for Stability of GPS/INS Attitude Estimation
Parameter Identification for Application Within a Fault-Tolerant Flight Control System
On-line Modeling and Calibration of Low-Cost Navigation Sensors
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
Fusion of GPS and Redundant IMU Data for Attitude Estimation
Development of a GPS/INS Sensor Fusion Simulation Environment Using 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
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