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System Identification of Aerodynamic Coefficients of F-16XL (ICCAS 2004)

This paper concerns parameter estimation for aerodynamic modeling under unsteady flow effects motivated by early work of Tobak and coworkers [1,2], and continued by Klein and Murphy [3]; therein are described integrodifferential equation models (including the following) which link the angle of attack and pitch rate variables, ) (t α and ) (t q respectively, to a generic aerodynamic coefficient ) (t Ca :