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Advances in Aircraft System Identification at NASA Langley Research Center
Aerodynamic Parameter Estimation Using Reconstructed Turbulence Measurements
Aircraft System Identification from Multisine Inputs and Frequency Responses
Practical Aspects of Frequency-Domain Approaches for Aircraft System Identification
Real-Time Estimation of Bare-Airframe Frequency Responses from Closed-Loop Data and Multisine Inputs
Flight-Test Techniques for Quantifying Pitch Rate and Angle-of-Attack Rate Dependencies
Real-Time Data-Compatibility Analysis Using Output-Error Parameter Estimation