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Yaw rate control of an air bearing vehicle
The NASA Langley Multidisciplinary Uncertainty Quantification Challenge
The effects of lightning on digital flight control systems
Summary of the First AIAA Stability and Control Prediction Workshop
Stability and Performance Metrics for Adaptive Flight Control
Software Considerations for Subscale Flight Testing of Experimental Control Laws
Significance of the dihedral-effect for a combat aircraft in rapid fuselage-reorientation maneuvers
Self-tuning Generalized Predictive Control applied to terrain following flight
Robust dynamic inversion control laws for aircraft control
Reduced-Order Aerodynamic Modeling Based on CFD Frequency Responses from Multisine Inputs
Quasi-steady flight to quasi-steady flight transition in a windshear - Trajectory guidance
Progress Toward a Format Standard for Flight Dynamics Models
Preliminary assessment of the robustness of dynamic inversion based flight control laws
Predictor-Based Model Reference Adaptive Control
Plans and Example Results for the 2nd AIAA Aeroelastic Prediction Workshop