Patent ID: 7397391
Filing Date: 2008-07-08
Classification: G05D

Abstract:
1. A method of aiding the piloting of an aircraft during a maneuver bringing about an increase in the attitude of the aircraft, according to which method the following steps are carried out automatically and repeatedly: a) a first value of attitude of the aircraft is taken into account; b) the current attitude of the aircraft is determined; c) an attitude deviation is determined by subtracting said first value of attitude from said current attitude; and d) at least one horizon line is presented on a display screen of a head-up display device, superimposed with the environment seen in front of the aircraft, wherein: in step d), a first section of indication which indicates said attitude deviation is moreover presented on said display screen, said first value of attitude corresponds to an optimal value of attitude at the end of the maneuver, and said first section of indication is presented on said display screen at a fixed position and said horizon line is presented on said display screen in a moveable manner.