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
Software Considerations for Subscale Flight Testing of Experimental Control Laws
Flight Test Experiment Design for Characterizing Stability and Control of Hypersonic Vehicles
A Flight Control System Architecture for the NASA AirSTAR Flight Test Infrastructure
Optimal input design for aircraft instrumentation systematic error estimation
Optimal input design for aircraft parameter estimation using dynamic programming principles