31th Congress of the International Council of the Aeronautical Sciences

06.1 - Flight Dynamics and Control (Control & Modelling)

RECURSIVE AERODYNAMIC PARAMETER IDENTIFICATION OF A FIGHTER JET FLYING IN TURBULENT AIR

C. Grillo, Universit di Palermo, Italy

Present paper performs the determination of aircraft parameter for very agile aircraft, via EKF, taking into account dynamic damping derivatives. A specific technique has been implemented to minimize the state estimation error. The proposed technique has been tested using flight test data of an European-fighter aircraft jet.


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