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Optimal Input Design for Aircraft Parameter Estimation using Dynamic Programming Principles
Advances in Experiment Design for High Performance Aircraft
Low Order Equivalent System Identification for the Tu-144LL Supersonic Transport Aircraft
Low Order Equivalent System for the Tu-144LL Supersonic Transport Aircraft
Aerodynamic Parameter Estimation for the X-43A (Hyper-X) from Flight Data
Development of a Low-Cost Sub-Scale Aircraft for Flight Research: The FASER Project
Automated Simulation Updates based on Flight Data
Real-Time Dynamic Modeling - Data Information Requirements and Flight Test Results