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49th European Rotorcraft Forum : September 5-7, 2023, Bückeburg, Germany : proceedings
41st European Rotocraft Forum 2015 : ERF : September 1-4, 2015, Munich, Germany : proceedings
40th European Rotorcraft Forum 2014 : 2-5 September 2014, Southampton, UK
Analysis of the Use of GPS + GLONASS for Aviation Applications
Helicopter flight and landing radar - a new technology developed in the european eurostars program
Helicopter rotor blade monitoring using autonomous wireless sensor network
Measurements of features of the ducted fan as a possible actuator of a multi-copter vehicle
A nonlinear position controller for maritime operations of Rotary-wing UAVs
Design and implementation of fuzzy logic controllers for helicopter elevation and azimuth controls
On-line scheduling and fault detection in NCS with communication constraints in Drone application
Application of combined NDT methods to study the helicopter rotor blades
35th European Rotorcraft Forum : ERF ; September 22 - 25, 2009, Hamburg, Germany ; proceedings
Active cabin vibration reduction for jet-smooth helicopter ride
Comprehensive approach for noise reduction in helicopter cabins
Unsteady effects of the seperated flow at the tail section of a helicopter fuselage
Investigation on rotor blade-wake interaction noise in descent flight conditions
Genetic optimizations of EC-135 noise abatement flight procedures using an aeroacoustic database
The effect of simulator motion on pilot control behaviour for agile and inert helicopter dynamics
Rotor power reduction using multiple spanwise-segmented, optimally-actuated trailing-edge flaps
Advanced optical rotor blade deformation measurements on a flying helicopter
Influence of rotor wakes on helicopter aerodynamic behaviour
Development of EC 135 turbulence models via system identification
Multi sensor data acquisition and fusion to increase situation awareness for a helicopter pilot
Optimal trajectory planning for an autonomous helicopter
High-fidelity optimization framework for helicopter rotors
Structural design and testing of active twist blades - a comparison
Design and drop test simulation of a helicopter skid landing gear with Abaqus/CAE
Benefit studies for rotor with active twist control using weak fluid-structure coupling
Sliding mode velocity-observer-based stabilization of a 3-DOF helicopter prototype
Manufacturing process simulation tools for faster industrialisation of composite parts
Numerical simulation of air flow past a full helicopter configuration
New FRP-reinforced PMI-foams for aircraft and transport applications