Abstract:We investigate apparent and intrinsic singularities of a flat model of aircrafts, illustrated with numerical simulations using Python and Maple. We consider failure situations and maneuvers for which apparent singularities of the previously known flat outputs may appear, making necessary to use some of the new flat outputs we consider. Basically, the aircraft flat outputs are x, y, z, the coordinates of the gravity center, completed with any function of the sideslip angle β, the angle of attack α, the bank ang… Show more
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