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