| 主权项 |
1. A method to assist piloting of an aircraft, according to which a trajectory pointer representing a current flight trajectory vector and a pitch pointer indicating a current pitch angle value are shown on a pitch scale of a display screen, including the following steps:
determining a pitch angle limiting value representative of a maximum admissible angle of attack, depending on a set of flight parameters and aircraft configurations, and displaying on the pitch scale of the display screen a maximum angle of attack pointer indicating the pitch angle limiting value, where the maximum angle of attack pointer and trajectory pointer form upper and lower limits, respectively, of a dynamic safety envelope representative of a normal flight of the aircraft.
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