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