Flight Test Techniques for Quantifying Pitch Rate and Angle of Attack Rate Dependencies
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
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
Real-Time Stability and Control Derivative Extraction From F-15 Flight Data
Identification of Low Order Equivalent System Models From Flight Test Data
Optimal input design for aircraft instrumentation systematic error estimation
Optimal input design for aircraft parameter estimation using dynamic programming principles