LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS
PROBABILISTIC TECHNIQUES FOR PILOT-VEHICLE INTERACTION AND HANDLING QUALITIES ANALYSIS
PROBABILISTIC TECHNIQUES FOR PILOT-VEHICLE INTERACTION AND HANDLING QUALITIES ANALYSIS
Frequency-Domain Method for Automated Simulation Updates based on Flight Data
A Sense and Avoid System for Unmanned Aircraft in Formation Flight (AIAA 2014-0967)
Integrated Methods to Model and Update Rotorcraft Simulations with Experimental Data
Investigation of Flight Loads Prediction using Multi-Body Simulation
Rapid Prediction of Worst Case Gust Loads Following Structural Modification
Design of Composite Structures to Improve the Aeroelastic Performance
Satellite Orbit Stabilization Using L~1 Adaptive Control
Receptance Based Active Aeroelastic Control Using Multiple Control Surfaces
Robust Adaptive Disturbance Compensation for Ship-Based Rotorcraft
Efficient Prediction of Aeroelastic Response Including Geometric Non-Linearities
Adaptive Aeroelastic Concept Applied to a Civil Jet Aircraft Model
SMorph - Smart Aircraft Morphing Technologies Project
Data-Driven Simulation-Updates of Tiltrotor Aircraft
On-Line Identification of Ship Airwake Disturbances on Rotorcraft
Adaptive Gust Alleviation for a Tilt-Rotor UAV Operating in Turbulent Airwakes
Optimisation of Composite Sensorcraft Structures for Gust Alleviation
Optimization of a Scaled Sensorcraft Model with Passive Gust Alleviation
Scaling for a Static Nonlinear Response of a Joined-Wing Aircraft
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
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
Seamless Positioning in All Conditions and Environments: SPACE