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HUBSCHRAUBER
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1 million investment in document handling
30 year partnership with Westland Helicopters Ltd
Adaptive Algorithm for Classifying Launch and Recovery of the HH-60H Seahawk
A low-vulnerability helicopter rotor blade
A new method for predicting rotor wake geometries and downwash velocity field
A nonlinear inverse simulation technique applied to coaxial rotor helicopter maneuvers
A TMO-based flight program of an unmanned helicopter
Automated generation of aerofoil characteristics for rotorcraft application
BAE systems seeks helicopter landing breakthrough
BARCO's avionics displays selected by Boeing
Boeing joins Team Cormorant for maritime patrol project
Brookhouse technology behind the scenes in USAF helicopter simulators
BT46 simulator for the German antitank helicopter PAH-1 AI
Canadian helicopter verifies night vision system with Ascension's laserBIRD
Commitment to CAE environment for GKN Westland Helicopters
Configuration design and optimisation study of a compound gyroplane
Constrained predictive control of helicopters
Contract to prove future Lynx is right choice
Control system design and testing for a small-scale autonomous helicopter
Cooperative Transport of a Slung Load Using Load-Leading Control
Correlation of helicopter rotor aeroelastic response with HART-II wind tunnel test data
Crashworthiness of helicopter subfloor structural components
Development of integrated rotorcraft design and virtual manufacturing framework
Direct adaptive fuzzy control for a nonlinear helicopter system
Effect of free play in rotor blades hinges on the non-linear ground resonance of a helicopter
Eigenmode Distortion: A New Perspective on Motion Cueing Fidelity in Flight Simulation
Elements of helicopter supermanoeuvrability at low flight velocities
Equivalent linear damping model of nonlinear hydraulic damper for helicopter rotor
ESDU data item simulates fatigue of helicopter rotor systems
Examination of indirect responses of helicopters using a refined inflow model
FAC roadshow highlights 'challenge and opportunity' at GKN-Westland
First high-velocity machining application in commercial helicopters
Flight Vehicle System Identification: A Time-Domain Methodology
Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: Part I
GKN Westland - exploiting powerful CAE software to gain competitive advantage
H∞ robust controller for autonomous helicopter hovering control