초록 ▼

The method of the invention includes forming a difference between left and right braking commands, by converting the difference into an additional control command for rudder and for a steerable nose gear, and applying the additional control command to the rudder and steerable nose gear according to

The method of the invention includes forming a difference between left and right braking commands, by converting the difference into an additional control command for rudder and for a steerable nose gear, and applying the additional control command to the rudder and steerable nose gear according to both of the following conditions: the difference is greater than a first threshold and the combined control command transmitted to the rudder and steerable nose gear by a rudder bar is less than a second threshold.

대표청구항 ▼

The invention claimed is: 1. A method for driving an aircraft during run over ground, said aircraft including a steerable nose gear and a rudder disposed at a rear of said aircraft, the method comprising:controlling yaw in said aircraft using a rudder bar at a disposal of a pilot of the aircraft, co

The invention claimed is: 1. A method for driving an aircraft during run over ground, said aircraft including a steerable nose gear and a rudder disposed at a rear of said aircraft, the method comprising:controlling yaw in said aircraft using a rudder bar at a disposal of a pilot of the aircraft, configured to address a combined control command to said steerable nose gear and to said rudder;equipping at least two undercarriage legs with brakes, the at least two undercarriage legs symmetric with one another with respect to a longitudinal vertical mid-plane of the aircraft; andproducing a braking command to control the wheel brakes of a corresponding one of the at least two undercarriage legs using two braking control members which are at the disposal of said pilot, respectively, associated with said corresponding one of the at least two undercarriage legs, wherein:a difference between said braking commands is formed;said difference in the braking commands is transformed into an additional control command for said rudder and for said steerable nose gear; andsaid additional control command is applied to said rudder and to said steerable nose gear, on the dual condition that:said difference in the braking commands is greater than a first threshold; andsaid combined control command addressed by said rudder bar to said rudder and to said steerable nose gear is less than a second threshold, and wherein:a maximum travel of each of said braking members lies between a neutral position and a maximum braking position, wherein said first threshold corresponds to a fraction of said maximum travel lying between one third and two-thirds.