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
Optimisation of Composite Sensorcraft Structures for Gust Alleviation
Adaptive Gust Alleviation for a Tilt-Rotor UAV Operating in Turbulent Airwakes
Optimization of a Scaled Sensorcraft Model with Passive Gust Alleviation
Scaling for a Static Nonlinear Response of a Joined-Wing Aircraft