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HUBSCHRAUBER
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keywords:(HUBSCHRAUBER)
Variable rotor speed control for an integrated helicopter/engine system
Nonlinear Analysis of a Coaxial Microhelicopter with a Bell Stabilizer Bar
Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation
Towards consistent hybrid overset mesh methods for rotorcraft CFD
Parallel universal approach to mesh motion and application to rotors in forward flight
Design and implementation of H-inf controller for micro-monocopter
Attitude control of a quadrotor aircraft subject to a class of time-varying disturbances
A multi-body systems approach to simulate helicopter occupant protection systems
On Dynamic State-Space models for fatigue-induced structural degradation
Airfoil pressure measurements during a blade vortex interaction and a comparisonwith theory
Correlated turbulence modelling: An advancing Fourier series method
Surrogate based optimization of helicopter rotor blades for vibration reduction in forward flight
Parallel efficient mesh motion using radial basis functions with application to multi-bladed rotors
Rotorcraft dispatching in large-scale emergencies using sequential linear assignment techniques
Computational fluid dynamics simulations of ship airwake
Modeling helicopter blade sailing: Dynamic formulation in the planar case
Heute schon wie morgen fliegen. Mit dem Flugsimulator AVES Forschung auf Flight Level Zero
Fatigue life reliability based on measured usage, flight loads, and fatigue strength variations
A comparison of main rotor smoothing adjustments using linear and neural network algorithms
A new boundary integral formulation for the prediction of sound radiation
Diagnosis using a first-order stochastic language that learns
Studies of trims, stability, controllability, and some flying qualities of a tandem rotor helicopter
Flight dynamics helicopter model validation based on flight test data
Estimating crack growth in rotorcraft structures subjected to mission load spectrum
Model of multidisciplinary simulation integration in helicopter rotor blade design process
Fuzzy Adaptive Nonsingular Terminal Sliding Mode Control of a Miniature Helicopter
Generating Certification Evidence for Autonomous Aerial Vehicles Decision-Making
Nonlinear modeling and control design of active helicopter blades
Prediction of nonlinear propagation distortion in blade-vortex interaction noise
Autonomous Load Control and Transportation Using Multiple Quadrotors
Modelling and dynamic stability of a hingeless active fibre composite blade
Stable adaptive schemes for state estimation and identification of linear systems
A probability-based approach to helicopter rotor tuning