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Flugmechanik
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keywords:("Flugmechanik")
Ground Vibration Test Identified Structure Model for Flutter Envelope Prediction
Parafoil Control Using Payload Weight Shift
Robust Parafoil Terminal Guidance Using Massively Parallel Processing
Parametric Study of Powered Parafoil Flight Dynamics
Nonlinear Unsteady Aerodynamic Modeling by Volterra Variational Approach
Parameter Estimation of Highly Unstable Aircraft Assuming Linear Errors
Parametric Modeling for Store Separation Aerodynamics Using System Identification
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