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Flugmechanik
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Higher Level Aerodynamic Input for Aeroservoelastic control of Flexible Aircraft AIAA Paper
Application of Multiple Methods for Aeroelastic Uncertainty Analysis
Low Order Model Approximation of Aeroelastic/Aeroservoelastic System
Step Based Experiment Design and System Identification for AeroElastic Dynamic Modeling
Adaptive Feedback Control Algorithm for Flutter Boundary Expansion
Computational Tools for Global Aerodynamic Modeling and Nonlinear Control
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
Eigenvalue Constraints for Realization-Based Identification