METHOD AND DEVICE FOR DETERMINING A CONTROL SET POINT OF AN AIRCRAFT, ASSOCIATED COMPUTER PROGRAM AND AIRCRAFT

摘要

A method and device for determining a control set point of an aircraft, an associated computer program and an aircraft are disclosed. In one aspect, the method includes calculating a performance scale in the form of slope values of the aircraft, the performance scale including a slope characteristic value, the slope characteristic value being associated with a corresponding performance characteristic value. The method also includes acquiring a guidance set point and displaying the acquired guidance set point, in the form of a slope value with respect to the performance scale. The method further includes determining a slope characteristic value associated with a guidance set point displayed in the form of a slope value, and calculating an aircraft control set point, the control set point being calculated relative to the performance characteristic value corresponding to the determined slope characteristic value.

主权项

1. A method for determining a control set point of an aircraft, the control set point being configured to be transmitted to at least one avionics system from at least one actuator control system and at least one guidance system, the method being carried out by an electronic device for determining the control set point and comprising:
calculating a performance scale in the form of slope values of the aircraft, the performance scale comprising at least one slope characteristic, each slope characteristic value being associated with a corresponding performance characteristic value from among extreme values of thrust, extreme values of drag, extreme values of ground acceleration, predetermined specific values of thrust, predetermined specific values of drag, predetermined specific values of ground acceleration and characteristic values of guidance set points; acquiring at least one guidance set point; displaying at least one guidance set point among the acquired guidance set point(s), in the form of a slope value with respect to the performance scale; determining at least one slope characteristic value associated with a corresponding guidance set point, displayed in the form of a slope value; and calculating at least one control set point for the aircraft, each control set point being calculated relative to the performance characteristic value corresponding to the associated slope characteristic value for each guidance set point displayed in the form of a slope value.