Aircraft System Identification from Multisine Inputs and Frequency Responses
Flight Test Techniques for Quantifying Pitch Rate and Angle of Attack Rate Dependencies
Aeroelastic Modeling of X-56A Stiff-Wing Configuration Flight Test Data
Real-Time Global Nonlinear Aerodynamic Modeling for Learn-To-Fly
Dynamic Modeling from Flight Data with Unknown Time Skews
A Generic Nonlinear Aerodynamic Model for Aircraft
Real-Time Parameter Estimation Using Output Error
Evaluation of Piloted Inputs for Onboard Frequency Response Estimation
Efficient Global Aerodynamic Modeling from Flight Data
Flight Test Maneuvers for Efficient Aerodynamic Modeling
Flight Test Experiment Design for Characterizing Stability and Control of Hypersonic Vehicles
Optimal input design for aircraft instrumentation systematic error estimation
Optimal input design for aircraft parameter estimation using dynamic programming principles