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Flugmechanik
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keywords:("Flugmechanik")
Aeroelastic Effects of Battens on the Flight Dynamics of a MAV
Model Predictive Control of Agile Projectiles
Subcritical Bifurcations in Shimmy Dynamics
Flight Control Development for a Speed-Agile Powered-Lift Transport Aircraft
Ground Contact Model for Mars Science Laboratory Mission Simulations
Feasibility Study of a Novel Method for Real-Time Aerodynamic Coefficient Estimation
Nonlinear Model Reduction for Flexible Aircraft Control Design
Continuous Differentiation of Complex Systems Applied to a Hypersonic Vehicle
Store Separation Equations of Motion
Aerodynamic Parameter Identification for Symmetric Projectiles: An Improved Gradient Based Method
A Two-Stage Method for the Parametric Identification of Scale-Model Helicopter Dynamics
Simulation of Aircraft Encounters with Perturbed Vortices Considering Unsteady Aerodynamic Effects
Modeling and Detection of Ice Particle Accretion in Aircraft Engine Compression Systems
Trim Analysis of a Moving-mass Actuated Airplane
Bifurcation Behaviour of a Flapping Wing MAV in Longitudinal Flight
Advanced UAV aerodynamics, flight stability and control : novel concepts, theory and applications
Guidance algorithms for proximity to target spacecraft
Effects of Articulated Wings on the Stability of Small Unmanned Aircraft
Linear, Parameter Varying Model Reduction for Aeroservoelastic Systems
An Initial Flight Investigation of Formation Flight for Drag Reduction on the C-17 Aircraft
Numerical Continuation Analysis of a Dual-Sidestay Main Landing Gear Mechanism
Using Indirect Turbulence Measurements for Real-Time Parameter Estimation in Turbulent Air
Effects of Freeplay on Aircraft Main Landing Gear Stability
Real-Time Frequency Response Estimation Using Joined-Wing SensorCraft Aeroelastic Wind-Tunnel Data
Investigation of the Prediction Error Identification for Flutter Prediction
Aerodynamic Model Identification of Frauke UAV
Development of a Fundamental Model for Flapping Wing MAVs and Preliminary Validation
Performance Enhancements by Bounding Flight
System Identification of Flexible Aircraft in Time Domain
Aircraft Spin Phenomenon Analysis Using Nonlinearity Index Theory
Towards Industrialisation of Bifurcation Analysis in Rotorcraft Aeroelastic Problems
Design and Experimental Validation of a Control System for a Morphing Wing
The Bifurcation and Continuation Method from an Aerospace Systems Design Point of View
Aircraft Stall Phenomenon Analysis Using Nonlinearity Index Theory
Effect Of Jump Strut Nose Landing Gear In Preliminary Design Of Aircraft
Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System
A Conceptual Study of Airfoil Performance Enhancement Using CFD
Bifurcation Analysis of the Generic Transport Model with a View to Upset Recovery
Method for Analyzing The Influence of Random Factors in Carrier Launching