Patent ID: 8478460

Claim:
A method to assist in adjusting a braking intensity of an aircraft on a landing runway comprising the steps of: recovering data concerning said runway where the aircraft is landing; including points characterizing an end of said runaway, a length of said runway, and exit points of said runway, data concerning a controlled speed corresponding to a speed below which the aircraft can perform any turn maneuver when taxiing, acquiring a position of the aircraft on the runway and a speed of the aircraft in a taxiing phase; calculating a distance that the aircraft will have traveled on said runway when the aircraft has reached a controlled speed, the controlled speed being calculated assuming that the speed of the aircraft decreases according to a predefined time function; displaying to the pilot graphical representation of said runway, said end points and exit points of said runway, said aircraft position on said runway and said calculated distance, a difference between said displayed calculated distance and displayed end and exit points of the runway allowing said braking intensity to be increased or reduced by the pilot.