Higher Level Aerodynamic Input for Aeroservoelastic control of Flexible Aircraft AIAA Paper
Flight Testing of Mission Adaptive Compliant Wing AIAA Paper 2007-1709 CD-ROM Number 7
Autonomous Flight Control Development on the Active Aeroelastic Wing Aircraft
Unsteady Aerodynamic Observable for Gust Load Alleviation and Flutter Suppression
System Benefits of Active Flutter Suppression for a SensorCraft-Type Vehicle
An Overview of SensorCraft Capabilities and Key Enabling Technologies
Conceptual Design of a Multi-utility Aeroelastic Demonstrator
Development of Wing Structural Weight Equation for Active Aeroelastic Wing Technology
HIGH FIDELITY MDO PROCESS DEVELOPMENT AND APPLICATION TO FIGHTER STRIKE CONCEPTUAL DESIGN
CLOSED-LOOP STALL CONTROL ON A MORPHING AIRFOIL USING HOT-FILM SENSORS AND DBD ACTUATORS