Assistance with piloting of an aircraft in a stall

A system to assist piloting of an aircraft, including a display screen showing a pitch scale, where a trajectory pointer represents a current flight trajectory vector and a pitch pointer indicating a current pitch angle value, comprising:

• an algorithmic module to determine a pitch angle limiting value representative of a maximum admissible angle of attack, depending on a set of flight parameters and aircraft configurations, and the algorithmic module to display on the said pitch scale of the display screen a maximum angle of attack pointer indicating the said pitch angle limiting value and dynamic safety envelope indicator, wherein the dynamic safety envelope indicator includes a graphical representation such that the maximum angle of attack pointer and trajectory pointer form upper and lower limits, respectively, with two vertical lines, each vertical line extending from an end of the maximum angle of attack pointer toward the trajectory pointer and the dynamic safety envelope being representative of a normal flight of the aircraft;
• wherein the display of one of the maximum angle of attack pointer and the said dynamic safety envelope indicator is shown using different colors, including a first color representing a normal flight situation, a second color representing a situation where a stall is imminent, and a third color representing a stall.