The present invention relates to a visualization method of the attitude of an aircraft, comprising the formation of a pitch scale (E) defining a lower border and an upper border, and including: to visualize the nil pitch angle of the aircraft, a zero graduation on the lower border and the upper border; to visualize the negative pitch angles of the aircraft, straight parallel graduations forming at least two groups converging toward one another with the approach of the zero graduation from the lower border; and to visualize the positive pitch angles of the aircraft, curved graduations, the curvature of which increases moving away from the zero graduation toward the upper border.