公开(公告)号：US20190384326A1

公开(公告)日：2019-12-19

申请号：US16435239

申请日：2019-06-07

Applicant: THALES

Inventor： Romain LAMOUR ,  Frédéric BERGER ,  François COLONNA ,  Marianne CAZES

IPC: G05D1/10 ,  B64C13/18

Abstract: A conversion device for converting a guidance setpoint signal from an aircraft guidance system for at least one control axis, into a control signal for an avionics system such as an aircraft stabilization system, comprising an acquisition module designed to acquire the guidance setpoint signal, and a generation module designed to generate the control signal from the acquired guidance setpoint signal, the control signal comprising at least two command pulses, the generation module being designed to calculate the duration between two consecutive command pulses depending on a corresponding value of the acquired guidance setpoint signal.