A New System Identification Method Using Short Duration Flight Test Inputs
A New System Identification Method Using Short Duration Flight Test Inputs
Flight Test Evaluation of the SAFE-Cue System for Loss of Control Mitigation (AIAA 2014-0447)
Piloted Simulation Evaluation of Pitch Axis Feel System Characteristics
Optimal Input and Output Blending for Adaptive Suppression of Adverse Aeroservoelastic Dynamics
Development of Innovative Transit Services Using Market Research Techniques
The Real-Flight Approach to Assess Flight Simulator Force Cueing Fidelity (AIAA 2013-5161)