Stowed Unmanned Air Vehicle Engineering (SUAVE): Deployable Wing Design and Testing
Development of a Novel Low Stored Volume High-Altitude Wing Design
Design Limitations of Deployable Wings for Small Low Altitude UAVS
Design Limitations of Deployable Wings for Small Low Altitude UAVs
Testing of Compact Inflatable Wings for Small Autonomous Aircraft
Aeroelastic Behavior of Inflatable Wings: Wind Tunnel and Flight Testing AIAA Paper
Flight Testing and Simulation of a Mars Aircraft Design Using Inflatable Wings AIAA Paper
Flight Control of a UAV with Inflatable Wings with Wing Warping
AIAA-2006-1697 Development of a Finite Element Model of Warping Inflatable Wings
AIAA-2006-1696 A High-Altitude Test of Inflatable Wings for Low-Density Flight Applications
BIG BLUE II: Mars Aircraft Prototype with Inflatable-Rigidizable Wings
AIAA-2004-1503 Development of UV-Curable Inflatable Wings for Low-Density Flight Applications
Development and Flight Testing of a UAV with Inflatable-Rigidizable Wings
AIAA-2004-6570 Flying on Air: UAV Flight Testing with Inflatable Wing Technology