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Flugmechanik
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Utilizing Flight Data to Update Aeroelastic Stability Estimates
Step Based Experiment Design and System Identification for AeroElastic Dynamic Modeling
Practical Aeroservoelasticity In-Flight Identification and Adaptive Control
Optimal Input and Output Blending for Adaptive Suppression of Adverse Aeroservoelastic Dynamics
Low Order Model Approximation of Aeroelastic/Aeroservoelastic System
Higher Level Aerodynamic Input for Aeroservoelastic control of Flexible Aircraft AIAA Paper
Eigenvalue Constraints for Realization-Based Identification
Covariance Function Realization Algorithms for AeroElastic Dynamic Modeling
Computational Tools for Global Aerodynamic Modeling and Nonlinear Control
Application of Multiple Methods for Aeroelastic Uncertainty Analysis
AIAA-2001-4009 Wavelet-Based Time-Varying Human Operator Models
Aerodynamic and Structural Measurement of the Aerostructures Test Wing for Flutter Testing
Adaptive Feedback Control Algorithm for Flutter Boundary Expansion