The invention relates to a system to control the deceleration of an aircraft during the taxiing phase on a landing strip, the system comprising: acquisition means (100) of the current position of the aircraft on the strip, acquisition means (100) of the current speed of the aircraft on the strip, calculation means (102), receiving position and speed values from the acquisition means, to define, as a function of the desired final speed of the aircraft at the so-called final position on the strip, a deceleration set-point modification time, after the current time, and a new deceleration set-point to apply from the modification time, to reach the final position at the desired speed.