06.1 - Flight Dynamics and Control (Control & Modelling)

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

C. Grillo, Università 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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