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Deterministic and Probabilistic Approaches to Model and Update Dynamic Systems
Advances in Aircraft System Identification at NASA Langley Research Center
Practical Aspects of Frequency-Domain Approaches for Aircraft System Identification
Practical Aspects of Real-Time Modeling for the Learn-To-Fly Concept
Flight-Test Techniques for Quantifying Pitch Rate and Angle-of-Attack Rate Dependencies
Vertical Spin Tunnel Testing and Stability Analysis of Multi-Mission Earth Entry Vehicles
Real-Time Onboard Global Nonlinear Aerodynamic Modeling from Flight Data
Nonlinear Aerodynamic Modeling From Flight Data Using Advanced Piloted Maneuvers and Fuzzy Logic
Envelope Protection for In-Flight Ice Contamination
Real-Time Dynamic Modeling - Data Information Requirements and Flight Test Results
Automated Simulation Updates based on Flight Data
Development of a Low-Cost Sub-Scale Aircraft for Flight Research: The FASER Project
Aerodynamic Parameter Estimation for the X-43A (Hyper-X) from Flight Data
Low Order Equivalent System Identification for the Tu-144LL Supersonic Transport Aircraft
Low Order Equivalent System for the Tu-144LL Supersonic Transport Aircraft
Advances in Experiment Design for High Performance Aircraft