RESULTS OF THE DEMONSTRATION FLIGHT OF THE GAINS PROTOTYPE III BALLOON
Addressing gaps in the availability of travel behaviour data
Development of Smart Spars for Active Aeroelastic Structures
Experimental Investigation of an All-Movable Vertical Tail Model
Delivering Multimedia Content to Automobiles Using Wireless LANs
AIAA-2004-1884 Experimental Validation of Wing Twist Control Using Adaptive Internal Structures
AIAA-2004-1883 Development of an Adaptive Stiffness All-Moving Vertical Tail
Effectiveness of Real Time Control for Active Restraint Systems in Frontal Crashes
Seamless Positioning in All Conditions and Environments: SPACE
The Impact of Standards on Maximo's Integration Capability
AIAA-2006-2131 On the Use of Adaptive Internal Structures to Optimise Wing Lift Distributions
AIAA-2006-2023 Application of Higher-Order Harmonic Balance to Non-Linear Aeroelastic Systems
Improved Implementation of the Harmonic Balance Method AIAA Paper 2007-2359 CD-ROM Number 7
Aeroelastic Flight Control for Subscale UAVs AIAA Paper 2007-1706 CD-ROM Number 7