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
Drag Minimisation Using Adaptive Aeroelastic Structures AIAA Paper 2007-1710 CD-ROM Number 7
Flight Testing an Iced Business Jet for Flight Simulation Model Validation AIAA Paper
Development and Application of New Low Rhodium Three-Way Catalyst Technology
2007-01-1504 Real Time Control of Restraint Systems in Frontal Crashes
Real Time Control of Restraint Systems in Frontal Crashes
Adaptive Gust Alleviation for a Tilt-Rotor UAV Operating in Turbulent Airwakes
Optimisation of Composite Sensorcraft Structures for Gust Alleviation