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Flugmechanik
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keywords:("Flugmechanik")
Eigenvalue Constraints for Realization-Based Identification
High-fidelity Modeling and Simulation of Flutter/LCO for All-movable Horizontal Tail with Free-play
Covariance Function Realization Algorithms for AeroElastic Dynamic Modeling
Optimal Input and Output Blending for Adaptive Suppression of Adverse Aeroservoelastic Dynamics
Aerodynamic and Structural Measurement of the Aerostructures Test Wing for Flutter Testing
Practical Aeroservoelasticity In-Flight Identification and Adaptive Control
Step Based Experiment Design and System Identification for AeroElastic Dynamic Modeling
Adaptive Feedback Control Algorithm for Flutter Boundary Expansion
Efficient Aeroelastic Model Updating in Support of Aircraft Flight Testing
Computational Tools for Global Aerodynamic Modeling and Nonlinear Control
Application of Multiple Methods for Aeroelastic Uncertainty Analysis
Low Order Model Approximation of Aeroelastic/Aeroservoelastic System