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
Relaxation of Initial Error and Noise Bounds for Stability of GPS/INS Attitude Estimation
Fusion of GPS and Redundant IMU Data for Attitude Estimation
Nonlinear Aircraft Model Identification and Validation for a Fault-Tolerant Flight Control System
UAV Attitude, Heading, and Wind Estimation Using GPS/INS and an Air Data System (AIAA 2013-5201)
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
Curvature-Velocity-Orientation Method for UAV Collision Avoidance
Identification of Aerodynamic Parameters for a Small UAV from Flight Data
Sensitivity Analysis of EKF and UKF in GPS/INS Sensor Fusion